-f $4"
                                               January 1984
                                               600/3  H - all
         REGIONAL ACID DEPOSITION:
       MODELS AND PHYSICAL PROCESSES
 ENVIRONMENTAL SCIENCES  RESEARCH LABORATORY
     OFFICE OF RESEARCH  AND DEVELOPMENT
    U.S. ENVIRONMENTAL PROTECTION AGENCY
RESEARCH TRIANGLE PARK,  NORTH CAROLINA  27711

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          REGIONAL ACID DEPOSITION:
        MODELS AND PHYSICAL PROCESSES
                      By

  The NCAR Acid Deposition Modeling Project
  National  Center for Atmospheric Research
                P. 0. Box 3000
           Boulder, Colorado 80307
               Project Officer

             Kenneth L. Demerjian
             Meteorology Division
  Environmental Sciences Research Laboratory
     Research Triangle Park, N. C. 27711
 ENVIRONMENTAL SCIENCES RESEARCH  LABORATORY
     OFFICE OF RESEARCH AND DEVELOPMENT
    U.S. ENVIRONMENTAL PROTECTION AGENCY
RESEARCH TRIANGLE PARK, NORTH CAROLINA  27711
                           . .lis, Af
                OWHONMENTA. iVEstAW

                t> SVv Ttflv S^lReFT

                          97333

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                                 DISCLAIMER

     This report has been reviewed by the Environmental  Sciences  Research
Laboratory of the U.S. Environmental Protection Agency  (EPA)  and  approved
for publication.  Approval does not signify that  the  contents necessarily
reflect the views and policies of the EPA, nor does mention  of  trade  names
or commercial products constitute endorsement or  recommendation  for use.

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                                  ABSTRACT

     In both the scientific study of  regional  acid  precipitation  and in
devising industrial and governmental  responses  to it,  the  role  of mathe-
matical models is essential.  Acid  deposition  is characterized  by such a
rich variety of physical and chemical phenomena that  only  a  comprehensive
computational model is capable of revealing  the detailed cause-effect rela-
tionships and the interactions among  all  the relevant physical  processes.
From an industrial and governmental point of view,  such a  comprehensive
model is essential in any quantitative  analysis of  the source-receptor re-
lationship.  This report reviews the  physical  and chemical phenomena that
give rise to regional  acidic deposition and  discusses the  current status of
modeling these phenomena.

     The role of models in environmental  assessment is first described.
This is followed by a review of existing  models in  a  chapter designed more
to establish a reference framework  for  the bulk of  the report than to pro-
vide a comprehensive review.  Most, if  not all, of  the principal  concepts
in model construction and evaluation  are  discussed.   Extensive  discussions
of state-of-the-art regional meteorological modeling  and the chemistry of
acid generation in the troposphere  are  presented in Chapters IV  and V.
Chapter VI then focuses on the development of  a new generation  of acid de-
position models.  Based largely on  the  topics  reviewed in  earlier chapters,
the desirable features of a comprehensible model are  described, with em-
phasis on topics needing great improvement or  omitted in present  models.
These include emissions data, detailed  acid  rain chemistry,  cloud pro-
cesses, dry deposition, model validation, and  sensitivity  analysis.

     We conclude that there are fundamental weaknesses in  existing models
of regional acid deposition, particularly in upper-air transport  and dis-
persion, omissions of detailed chemical reactions,  cloud physics, and the
treatment of terrain and surface effects.  Due  to recent advances in meso-
scale meteorology and tropospheric  chemistry,  marked  improvements are now
possible in regional acid deposition  models.   However,  the development of a
comprehensive model requires a clearly  focused, multidisciplinary group
effort under strong scientific leadership.  Among many types of modeling
approaches, the Eulerian framework  is most suitable for representing the
essential physical and chemical processes in regional  acid deposition.  A
framework for a model  system incorporating these findings  is contained in
the companion to this report, Regional Acid Deposition:  Design and Manage-
ment Plan for a Comprehensive Modeling  System.

     This is the first of two reports prepared by the National  Center for
Atmospheric Research (NCAR) for the Environmental Protection Agency (EPA)
under Interagency Agreement No. AD49F2A203 extending  from  July  1, 1982 to
May 31, 1983.
                                      111

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                                  CONTENTS
Abstract	  iii

Acknowl edgments	   xl

EXECUTIVE SUMMARY	    1

  I.  THE ACID RAIN PHENOMENON:  A GENERAL PHYSICAL DESCRIPTION	    8
      Overview and History	    8
      The Physical Picture	    9

 II.  THE ROLE OF MODELS IN ENVIRONMENTAL ASSESSMENT	   11

III.  REVIEW OF EXISTING MODELS	   13
      1.  Air Quality Models	   13
          1.1  Introduction	   13
          1.2  The concepts of Eulerian and Lagrangian models	   14
          1.3  Local and mesoscale air quality models	   16
          1.4  Acid deposition models	   17
               a.  Lagrangian acid deposition models	   18
               b.  Eulerian acid deposition models	   21
          1.5  Verification of acid deposition models	   24
          1.6  Model sensitivities	   29
          1.7  Model limitations	   30
               a.  Emissions	   30
               b.  Chemistry	   30
               c.  Transport	   31
               d.  Deposition	   32
          1.8  Model development needs	   32
      2.  Regional Meteorological Models	   33
          2.1  Introduction	   33
          2.2  Quantitative measures of forecast skill and
               realism of simulations	   40
               a.  Measures of forecast skill	   40
                      S} scores	   40
                      Categorical forecast scores	   43
                      Threat scores	   48
                      Bias scores	   48
                      Probability ellipses	   51
                      RMS errors		   51
                      Correlation coefficients	   51

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                     Characteristics of phenomena	   51
                     Prediction matrix of occurrence
                      vs. nonoccurrence of events	   54
                     Scale separation of errors 	   54
                     Summary of operati onal sk i 11  scores	   54
              b.  Statistical  measures of realism of
                  simul ati ons	   55
                     Correl ati on matri x	   55
                     Structure function	   58
                     Spectra	,	   58
         2.3  Components of regional models	»   58
              a.  Numerical  aspects.	   63
                     Grid structure	   63
                     Numerical methods	   63
                     Lateral boundary conditions	   66
                     Data analysis and initialization	   67
              b.  Physical aspects	   70
                     Surface processes	   72
                     Surface-layer and planetary boundary-layer
                      processes	   73
                     Condensation and evaporation processes	   76
                     Layered clouds and radiative effects	   81
         2.4  Summary and conclusions	   85

IV.  THE MATHEMATICS AND PHYSICS OF METEOROLOGICAL MODELS	   87
     1.  Objective Analysis	   87
         1.1  Introduction	   87
         1.2  Observing systems and the representativeness
              of observations	   88
         1.3  Analysis methods of questionable or unknown
              qual i ty	   89
         1.4  Computationally inexpensive methods of
              rel i abl e qual i ty	   91
              a.  Cressman analysis method	   91
              b.  Barnes analysis method	   93
         1.5  Computationally expensive analysis methods
              of hi gher qual i ty	   95
              a.  Univariate optimum interpolation	   95
              b.  Univariate optimum interpolation,
                  isentropic coordinates	   96
              c.  Multivariate optimum interpolation	   99
         1.6  Analysis methods used by NMC	   103
              a.  Three-dimensional spectral analysis	   103
              b.  Multivariate three-dimensional
                  optimum interpolation	   104
         1.7  Experimental comparisons of objective
              analysi s methods	   106
         1.8  Summary	   109
     2.  I ni ti al i zati on	   Ill
         2.1  Introduction	,	   Ill
         2.2  Damping scheme	   Ill
         2.3  Variational scheme	   112
                                    VI

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        2.4  Static scheme	  112
             a.  Nondivergent initialization	  112
             b.  Divergent initialization	  112
        2.5  Dynamic scheme	  112
        2.6  Nonlinear normal mode scheme	  113
        2.7  Bounded-derivative scheme	  113
        2.8  Summary	  113
    3.  Boundary Conditions	  114
        3.1  Introducti on	  114
        3.2  Sponge boundary scheme	  114
        3.3  Radiation boundary scheme	  115
        3.4  Bounded derivative scheme	  115
        3.5  Summary	  116
    4.  Surface Effects	  116
        4.1  Introduction	  116
        4.2  Surface energy budget	  116
        4.3  Surface moisture budget	  117
        4.4  Summary	,	  118
    5.  Planetary Boundary Layer Effects	  118
        5.1  Introduction	  118
        5.2  Single-layer approach	  119
        5.3  Multi-layer approach	  121
             a.  First-order closure	  121
             b.  Higher-order closure	  122
        5.4  Summary	  123
    6.  Clouds and Precipitation	  123
        6.1  Introduction	  123
        6.2  Grid-resolvable clouds and precipitation	  123
        6.3  Subgrid-scale clouds and precipitation	  124
             a.  Moist convective adjustment scheme	  124
             b.  Moisture convergence scheme	  125
             c.  Convective equilibrium scheme	  125
             d.  Buoyancy energy scheme	  126
             e.  Explicit scheme	  126
        6.4  Summary	  126
    7.  Numerical Methods	  127

V.  THE CHEMISTRY OF ACID GENERATION IN THE TROPOSPHERE	  129
    1.  Gas Phase Reactions	  129
        1.1  Introduction	  129
        1.2  The gas phase tropospheric chemistry of
             S02 and N0/N02 in acid generation	  130
             a.  The gas phase HO-radical oxidation
                 of S02 and N02 in the troposphere	  133
             b.  The oxidation of S02 by products of the
                 alkene-ozone reacti ons	  138
             c.  The 0(3P)-atom oxidation of S02	  142
             d.  The CH302 reaction with S02	  142
        1.3  The gas phase chemistry of the troposphere and
             the mechanism of generation of the reactants for
             S02 and N0/N02	  143
                                  vn

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2.  The Solution Phase and Heterogeneous Processes	  154
    2.1  Aqueous phase (aerosol, fog, cloud, rain water)
         chemistry of S(IV) oxidation to H2SOi,	  154
         a.  Gas-particle and particle-particle
             i n terac t i ons	  154
         b.  The particle sulfate formation mechanism	  166
                Carbonaceous particles and acid
                 generati on	  168
                Aqueous phase reactions leading
                 to acid formation	  169
                   S(IY) oxidation by 02	.-  171
                   S(IY) oxidation by 03	  171
                   S{IV) oxidation by H202	  192
                   S(IV) oxidation by other species	  192
         c.  Comparison of aqueous S(IV) oxidation
             mechani sms	  195
    2.2  Acid generation from nitrogen-containing
         species through gas-particle interactions
         and aqueous chemistry	  203
         a.  Features of heterogeneous N0y chemistry:
             empirical evidence	  203
         b.  Condensed-phase kinetics	  206
         c.  NOy gas-particle interactions	  212
    2.3  Coupling of NOX - SOX aqueous and
         particulate chemistries	  219
         a.  Gas-phase oxidant competition..	  220
         b.  Aqueous oxidant competition....	  220
         c.  Acid inhibition	  220
         d.  S02 oxidation by N0y	  221
         e.  Volatilization of weak and comparatively
             insoluble acids	  221
    2.4  The role of hydrocarbons and organic oxidants
         in heterogeneous atmospheric processes...	  222
         a.  Introduction	  222
         b.  Model treatments and condensed-phase
             chemi stry	  222
    2.5  The possible coupling of chemistry and
         meteorol ogy	  223
    2.6  Summary of the chemical reactions important
         for acid generation in the troposphere	  224
3.  Photodissociative Processes in Chemical Modeling.'.	  225
    3.1  Introduction	  225
    3.2  Flux calculations and photolysis rates...	  227
         a.  Clear sky values:  effects of multiple
             scattering and surface reflection	,	  227
         b.  Aerosol and cloud effects	  236
                Aerosol s	*	*	  236
                Cl ouds	  236
    3,3  Photodissociation calculations in a
         regi onal -seal e model	  240
                              viii

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VI.  DEVELOPMENT OF ACID DEPOSITION MODELS	  244
     Introduction	  244
     1.  Emi ssi ons	  244
         1.1  Introduction	  244
         1.2  Needed data for an emissions inventory	  245
              a.  Chemical species	  245
              b.  Classification of sources	  246
              c.  Spatial scales	  246
              d.  Temporal scales	  246
              e.  Number of inventories	  246
         1.3  Adequacy of existing data	-  247
         1.4  Subgrid issues	  252
     2.  Long-Range Transport of Pollutants	  254
     3.  Acid Rain Chemistry	  257
     4.  Cl ouds	  259
         4.1  The roles of clouds in acid rain	  259
         4.2  Boundary-layer venting and clouds	  261
              a.  Observational evidence that cloud
                  transport is important	  261
              b.  Previous simulations	  262
         4.3  Vertical transport of pollutants
              —a mathematical framework	  266
         4.4  Four time scales associated with cloud	  267
              a.  Residence time below cloud base, TSUb cid	  267
              b.  Transport-to-cloud time scale, rtrans	  268
              c.  Transport times through clouds, T-jnso] and TSO]....  268
         4.5  Four representative cloud types	  270
         4.6  Cloud transport as described by large-scale
              meteorological models	  275
         4.7  Cloud modeling	  276
     5.  Dry Deposition	  279
         5.1  Introduction	  279
         5.2  Available model input	  284
              a.  Aerodynamic resistance	  284
              b.  Surface resistance	  284
         5.3  Suitable models	  286
         5.4  Phases of complexity	  290
     6.  Model Resolution	  290
         6.1  Introduction	  290
              a.  The disparity of spatial scales	  290
              b.  The need for fine resolution	  292
              c.  The advantages of limited-resolution models	  292
         6.2  Observations of the variability of S02 and
              NOX concentrati ons	  293
              a.  Aircraft observations of variability	  293
              b.  Ground-level measurements of pollutant
                  variabil i ty	,	  297
         6.3  Physical laws, averaging, and computer solutions;
              the mathematics of subgrid-scale averaging	  297
                                    IX

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               a.  Averaging and computer simulation	  300
               b.  Why are grid-point simulations often
                   sati sf actory ?	  302
               c.  Limits on the magnitude of subgrid-scale effects...  303
          6.4  Situations in which subgrid effects are important	  304
          6.5  Approximate treatments of subgrid processes	  308
          6.6  Boundary-layer transport and the need for
               fine vertical resolution	  309
      7.  Numerical Methods	  316
          7.1  I ntroducti on	  316
          7.2  Particle-in-cell scheme	.-  316
          7.3  Pseudo-spectral  scheme	  316
          7.4  Finite-element scheme	  317
          7.5  Upstream-correcting scheme	  317
          7.6  Numerical  schemes for chemical systems	  318
      8.  Model  Validation and Sensitivity Analysis	  319
          8.1  I ntroducti on	  320
          8.2  Discussion of validation strategy	  323
          8.3  Synergistic relation of modeling and
               measurement programs	  327
          8.4  Sensitivity analysis	  327

 VII.  SUMMARY AND CONCLUSIONS	  329

VIII.  REFERENCES	  331

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                              ACKNOWLEDGMENTS

     This report is the collective effort of the members of the NCAR Acid
Deposition Modeling Project.  We would like to acknowledge the broad com-
munity of researchers whose work has provided the foundation for this-re-
port.  We would also like to thank Dr. Kenneth L. Demerjian, EPA Project
Officer, whose inspiration and support has made the project possible, and
Dr. Wilmot Hess, Director of NCAR, for his enthusiasm and continued inter-
est in the project.  R. E. Dickinson, T. E. Graedel, P. J. Samson, J. H.
Seinfeld, and M. Oppenheimer kindly reviewed earlier versions of this re-
port, and we found their comments and suggestions very useful in preparing
the final version.  Finally, we are also deeply grateful to Daloris Flam-
ing, the administrative assistant for the project, for her continued dedi-
cation and perseverance in producing this report.


                 The NCAR Acid Deposition Modeling Project

                  John Wyngaard (AAP), Project Coordinator
      Richard Anthes (AAP), Subgroup Leader, Meteorological Processes
          Jack Calvert (ACAD), Subgroup Leader, Chemical Processes
           Julius Chang (Lawrence Livermore National Laboratory),
             Subgroup Leader, Model Development and Integration
                           Robert Chatfield (ASP)
                           Ralph Cicerone (ACAD)
                             Tony Del any (ACAD)
                           Daloris Flaming (AAP)
                           Phil Haagenson (ACAD)
                            Brian Heikes (ACAD)
                            Hsiao-ming Hsu (ASP)
                  Shaw Liu (NOAA/ERL Aeronomy Laboratory)
                          Paulette Middleton (ASP)
                            Bill Stockwell (ASP)
                          Anne Thompson (ASP/ACAD)
                            Stacy Walters (ACAD)
                                     XI

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                             EXECUTIVE  SUMMARY

     This report reviews the physical and  chemical  phenomena  that give rise
to regional  acidic precipitation and  deposition,  from  the  viewpoint that
mathematical modeling of these phenomena is  necessary  and  feasible.  While
the review is not exhaustive and all-encompassing,  it  is lengthy.  Accord-
ingly, this Executive Summary presents  a concise  statement of the contents
and conclusions of the full report.

     The rise of the acid  rain (more  accurately,  acid  deposition) problem
to public awareness in the United States and Canada has  occurred very ra-
pidly and recently.  Both  public and  scientific awareness  and activities in
Europe, especially Scandinavia, preceded those  in North  America.  Indeed,
acid rain is not a new phenomenon; many of the  causes  and  controlling fac-
tors and some of the consequences were  recognized 100  years ago.  Features
of the acid rain problem that are new are  (a) our perception  of the quanti-
tative questions that must be answered  to  gain  a  full  understanding of the
essential chemical and meteorological processes,  and (b) our  ability to in-
vestigate the questions with field- and laboratory-measurement programs and
with mathematical models.  Similarly, from the  point of  view  of those con-
cerned with the effects of acid rain, there  now exist  reasonably logical
and mature formulations of (c) relationships between ecological  systems
(and physical structures)  and acid deposition that can be  investigated
quantitatively.  Also, as  noted above,  public awareness  of the potential
effects and probable causes of acid rain is  new,  as is the understanding
that some kinds of pollution traverse political boundaries.

     In the bulk of the report, we examine the  full  range  of  meteorological
and chemical processes that are involved in  the overall  phenomenon; that
is, the production and deposition of  acidified  rain,  snow,  fog,  mist, and
dry deposition of acid anhydrides over  important  inhabited regions such as
the east central United States and Canada.  We  pay particular attention to
issues in the study of acid rain through mathematical  models.  While the
scientific questions dictate the kinds  of  field measurements, laboratory
experiments, and model development to be undertaken (all of which are
necessary),  we are particularly interested in how to develop  and employ
credible models.  By credible models  we mean those that  are built on basic
physical  and chemical processes and that can test hypotheses  and guide the
design and assessment of field measurement programs with the  eventual goal
of predicting acid deposition rates and source-receptor  relationships and
of providing reliable estimates of the  effects  of emission control strate-
gies.

The Physical Picture

     Understanding and modeling the acid rain phenomenon requires one to
recognize a wide range of  physical and  chemical processes  and their inter-

                                      1

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actions.  Briefly, these are (a) emissions of materials  that  cause  and  reg-
ulate acidity in precipitation and deposition,  (b) meteorological motions
that transport and dilute the emitted substances laterally and  vertically,
(c) the variety of physical and chemical transformations that alter the
physical phase and chemical properties  (e.g., valence or oxidation  state)
of the emitted substances, and (d) the meteorological factors and surface
adhesiveness that lead to deposition of the transformed  substances.  A  less
well-recognized set of questions surrounds those properties of  the  Earth's
surface that control the rate of uptake of dry  materials (e.g.,  gaseous S02
and/or airborne particles).

     Because the principal acids in precipitation are sulfuric  (H^O^)  and
nitric (HN03), we are most concerned with emissions of sulfur and nitro-
gen.  However, the hydrocarbons and their oxidation products  are important
reactants in the chemistry which ultimately leads to HN03 and H2SOtt.  Esti-
mates of anthropogenic emissions of S02 (mostly from coal- and  oil-burning
electrical power plants and metal-smelting plants) and of NOX (mostly NO
and N02 from high temperature combustion processes, including those in  auto
and truck engines and power plants) are reasonably reliable for the world's
industrialized countries.  Much less credible,  but probably less important,
are estimates of natural emissions of organic sulfur gases and  of natural
NOX compounds.  Natural sources of gaseous NH3  and particulate  NHj/, gas-
eous hydrocarbons, airborne mineral dusts, and  lightning-produced NOX
must also be estimated reliably.  Minor contributions to precipitation
acidity from HC1 and organic acids are often negligible.

     Whether the key emissions are anthropogenic or natural,  they are in-
jected into the atmosphere at or near the Earth's surface, usually  within
the planetary boundary layer.  Accordingly, boundary layer meteorology  is
at the core of the acid rain problem.  The physics of turbulence and con-
vection, diurnal variation in surface heating,  terrain geometry, and sur-
face and boundary layer hydrology exert strong  control over the initial
dispersion of the emitted substances.  Further, during the time these sub-
stances spend in the boundary layer, their physical environment (e.g.,  tem-
perature, pressure, humidity, available sunlight) and proximity to  surfaces
and to other pollutants such as aerosol particles control the rate  and  type
of chemical  transformations that occur—and they are markedly different
from those that are favored above the boundary  layer in  the free tropo-
sphere.  There is perhaps only one important acid precursor or  regulator,
NOX from lightning, that does not begin its atmospheric  life  in the
boundary layer, although background tropospheric ozone is central to all
tropospheric chemistry.

     In dirty or clean air, in the boundary layer and above,  chemicals
react with each other.  The precise rates and types of reactions depend
strongly on the local pressure, temperature, available sunlight (both
direct and scattered), the presence of  liquid and vapor  H20,  and on the
local chemical composition (i.e., the spectrum  of available chemical co-
reactants).   In Chapter V, we organize  our discussion into categories of
homogeneous reactions (gaseous and liquid) and  heterogeneous  processes  and
by principal categories of chemical species.  Key considerations include
the exact rates of transformation (oxidation) of S02 and NOX  into I^SO^
and HN03, the major pathways of transformation, and the  essential con-

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trolling agents.

     In an oxidizing atmosphere  such  as  that  of  the  Earth,  the  oxidation of
S02 and NOX to H2SOit and HN03 is  inescapable,  given  enough  time in  the
atmosphere.  Practically, however,  it is  very  important to  know what frac-
tion of all of a region's emissions is oxidized  and  deposited within the
region and what fraction of the  total  is  transported long distances (at
high altitudes, for example) for  eventual  deposition onto territories hun-
dreds or thousands of kilometers  from the sources.   This is to  say  that a
credible description and model of this physical  system  must include quanti-
tative treatment of material transport and transformation above the bound-
ary layer.  Similarly, the factors  that  limit  the  rate  of surface  deposi-
tion and uptake of gases (dry deposition)  must be  treated quantitatively.
These include near-ground turbulence,  the condition  and type of the surface
(e.g., vegetation, soils), and the  chemical stickiness  and  reactivity of
the relevant substances on the surfaces.

Existing Models and Components of Models

     In Chapter III, we define,  describe,  and  compare two distinct  types of
models used for studying long-range transport  of air pollutants:   Eulerian
grid models and Lagrangian trajectory models.  Also,  because of different
goals and problems facing air pollution  meteorologists  and  chemists, it has
been useful to develop and employ distinctly  different  models for  air qual-
ity modeling (AQM) and acid deposition modeling  (ADM).   For ADM, we con-
clude that the three-dimensional  nature  of the problem  and  the  importance
of simulating with adequate generality specific  source  distributions and
eventual control strategies require an Eulerian  framework.

     Existing ADM's have already  contributed  to  our  understanding  of the
acid rain problem, but a number  of  phenomena  have  not been  treated  fully
yet, largely because of the relative  youth of  the  ADM field. Reasonably
well-based treatments of each phenomenon  have  been attempted, but  not in-
side one model; that is, the best available mathematical parameterizations
have not been coupled together.   Individual models tend to  be strong in one
respect, but very weak in others.  A  number of fundamental  weaknesses that
are widespread, or even ubiquitous, can  be mentioned.  For  example, exist-
ing acid deposition models do not allow  for mixing of pollutants above the
boundary layer.  Similarly, no recognition is  given  to  different types of
precipitation (rain, snow, dew,  etc.)  or  to the  temperature and pH  that
characterize precipitation scavenging and acid formation.   No cloud-chem-
ical processes have been considered so far.  Further, fundamental  (or ele-
mentary) chemical reactions have  not  been treated  with  sufficient  detail.
Instead, linear overall transformation rates  have  been  employed (for exam-
ple, the rate of conversion of S02  to sulfate  has  been  set  equal to x% per
hour without regard to mechanisms or  controlling factors, although  seasonal
dependence of x is sometimes permitted).   No  published  model has yet in-
cluded reasonably complete chemical reaction  schemes, and nitrogen  oxides
are usually omitted entirely.  Similarly,  dry  deposition of pollutants has
been simulated with fixed deposition  velocities, and dependences on winds,
surface topography, moisture, and vegetation  types have been ignored.  Sub-
grid-scale inhomogeneities in emissions,  transport,  chemical reaction types
and rates, and deposition have not  been  included.  Consequently, and also

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because of lack of field data, the verification  of  ADM's  has  not progressed
very far.  Few data and the use of nonmechanistic model parameter!zations
have led to more model "tuning" in the past  than  is  desirable in the future.

     Air quality modeling and regional meteorological modeling  are  better
developed fields than acid deposition modeling.  The  former have a  longer
history and a greater data base than the latter.  Fortunately,  techniques
and results from AQM and regional  meteorological modeling  are valuable  for
ADM.  For example, the experience and results of AQM  researchers in dealing
with large numbers of chemical reactions can be  tapped.   Schemes to clas-
sify and to reduce systematically the numbers of  independent  chemical -reac-
tion equations offer help to ADM (see especially Chapter  V).  Also,  methods
of incorporating emissions into AQM's and  the AQM emissions data base  it-
self are largely applicable in ADM.

     The relative maturity and quantitative  nature  of regional  meteorologi-
cal modeling as a field can be of enormous benefit  to those who seek to de-
velop new, more general and realistic acid deposition models.  In Chapter
III, we present an overview of regional meteorological models.   A brief
history of their goals, methods, and capabilities is  outlined and the  prin-
cipal components of these models are identified.  Briefly, these are the
mathematical or numerical aspects and the more physical features.  In  the
former category, we review the essential features of  the  spatial  grids  in
these models, the various numerical methods  employed  to solve the governing
partial differential equations, the lateral  boundary  conditions,  and the
overriding need for adequate data analysis and data  initialization.   In
each consideration, much of the task at hand in  ADM,  namely to  model accur-
ately the dispersion and transport of pollutants, is  closely  related to the
main purposes of regional meteorological modeling.   Thus,  the progress  and
methods in the latter field can be tapped  as future  ADM's  are contemplated
and designed.

     Similarly, the ways in which the physical aspects of regional  meteoro-
logical models have been improved and tested will be  of benefit to  ADM  de-
velopment.  These physical aspects include the transports of  heat,  moisture
and momentum at the Earth's surface, in the  planetary boundary  layer and
free troposphere, and the energy sources and sinks  that govern  the  trans-
ports.  Also included are phase changes of water and  the  interaction of ra-
diation with clouds and the surface.  The  fact that these physical  phenome-
na occur on many disparate spatial scales, including  scales shorter than a
model's grid spacing, necessitates parameterizations—relating  the  cumula-
tive effect of subgrid-scale phenomena on  the fluid flow,  for example,  to
the model-resolvable scales of motion.  Parameter!'zations of  surface pro-
cesses, of planetary boundary layer processes, of condensation  and evapora-
tion processes, and of radiative effects of  layered clouds in current mod-
els are also reviewed, and strong indications of  areas ripe for progress
are identified.  While many of the simpler parameter!'zations  of physical
processes now in use in regional meteorological  modeling  (RMM)  are  attract-
ive in the early stages of acid deposition model  development, it is encour-
aging to note the progress in RMM toward tractable,  improved  parameter!za-
tions.

     Another important consideration in the  field of  RMM  that will  be di-

                                     4

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rectly useful in ADM is that of objective measures  of model  skill,  i.e.,
the accuracy of model predictions.  In Chapter  III, we  review  several
standard quantitative measures of forecast  skill  and also  summarize the
state of the art of RMM's to forecast (precipitation, for  example). Clear-
ly, the ability of acid deposition models to  forecast deposition  patterns
(say, annual totals) or deposition amounts  in distinct  events  must  be  mea-
sured objectively.  The methods used in RMM will  serve  as  good guides  at
first.

     Because of the great potential for transferring methods and  parameter-
izations from RMM to ADM, we have reviewed  components of the former models
in some detail, principally in Chapter IV.  First,  the  need  for objective
analysis is recognized—irregularly-spaced  initial  meteorological data must
be transformed to provide initial conditions  on a model grid.   The  tech-
niques, quality, computational costs, and history of objective analysis
methods are summarized and several case studies are discussed. The related
need for data initialization is discussed in  similar detail.   General  phy-
sical considerations, mathematical analysis,  and  experience with  meteorolo-
gical models can indicate general spectral  and  transient characteristics of
data-caused noise.  In specific applications  (e.g., for a  specific  regional
topography and synoptic situation), there is  both sound theory and  practi-
cal experience to guide the choice of initialization procedure.  According-
ly, unneeded computational costs can be avoided.  Also, as is  true  in  all
methods to solve differential equations, boundary conditions must be spe-
cified.  Principal techniques now in use in RMM's (spatial  damping  (or
sponge) conditions, wave-radiation conditions)  and  bounded derivative
schemes are reviewed with various applications  in mind.  Numerical  methods
and mathematical principles for objective analysis, data initialization,
and boundary conditions are also reviewed in  Chapter IV.   Once again,  the
available general theory plus the experience  of RMM researchers constitute
a well-based foundation for ADM development.

     On a more physical side, the essential RMM components mentioned above,
surface physics and effects, planetary boundary layer physics  and effects,
and the thermodynamic and radiative physics and effects of clouds and  pre-
cipitation are also reviewed.  The methods  and  problems extant in the  field
of RMM are very close to those that will prevail  in ADM.

The Chemistry of Acid Generation in the Troposphere

     As mentioned earlier, the chemical phenomena and reaction sets in ex-
isting acid deposition models are far from  complete.  This is  so  for many
reasons, including the fact that the importance of  long-range  transport of
pollutants has been perceived by the public and its agencies.   Accordingly,
much work in ADM has focused on the meteorological  aspects of  transboundary
transport.  Also, it is true that mechanistic information  on the  actual
chemical processes that transform S02 into  sulfuric acid and NOX  into  ni-
tric acid has appeared very confusing and incomplete until  recently.  Also,
the chemistry of acid generation is more complicated than  that of regional
chemical oxidants; the former involves gas-phase  and aqueous reactions,
while the latter is due to gas-phase reactions  alone.

     Accordingly, our discussions and review  of the chemistry  of  acid

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generation in Chapter V are  focused  at  first  on  the  essential  chemistry
itself rather than the chemistry now  in  the existing  ADM's.  The main cate-
gories of the review are gas-phase reactions,  aqueous-phase  and heterogene-
ous processes, and photodissociative  processes.   In  any  credible ADM, it is
extremely important—in fact, essential—to think  in  terms of  reaction
mechanisms as opposed to depending completely  on  parameterizations of over-
all reaction or transformation  rates.   For example,  it  is  inadequate to
know only the rate at which  substance A  is transformed  to  substance C in a
mixture as complex and variable as a  regionally  polluted atmosphere.  In-
stead of the overall process
we require, instead, knowledge of elementary  reaction  mechanisms  exempli-
fied by

                           A + B _ ^ _ ^ C  + D,

where the rate k is specific to the two  reactants A  and B  and  to  reaction
conditions (pressure, temperature) and the chemical  identities of C and D.
Only in this way can a rigorous mechanistic understanding  be developed
wherein the overall rates of the key transformations and their sensiti-
vities to pollutant and ambient chemical concentrations are predictable.
Without it, we would continue to be prey to unknown  errors and to criticism
of the type that now applies to
                       S02  rate = x% per hour^ 50^=.

For example, this simple and widespread parameterization  is  inherently
linear:  the rate of production of S(\= is  proportional to  the gaseous
S02 concentration.  In reality, the  supply  of  the  chemicals  that actually
oxidizes S02 to SO^ might be  limited in certain locations,  and little or
no SOi^ production could take  place  even when  large  amounts  of S02 are
available there.  Similarly, the S02-to-S01|= conversion rate probably de-
pends on the exact species that is accompanying the  oxidation so that the
rate, x, is not constant but varies  with time.  Obviously,  analogous funda-
mental considerations apply to the conversion  of NOX to nitric acid, to
the production of photochemical oxidants like  ozone  and peroxyacetyl ni-
trate and to the production of S02 from biogenic organic  sul fides, for
example.

     The main goals of the very detailed presentations  in Chapter V are to
identify from available research results the principal elementary reaction
mechanisms and key species in  the gas-phase, aqueous-phase,  and heterogen-
eous reactions that cause and  control acid  generation.  From a complex and
encyclopedic list of chemicals and reactions,  a smaller,  more concise list
of chemical  variables and processes  must be distilled to  develop a tract-
able and useful ADM.  From fundamental principles, laboratory data or pho-
tochemistry and kinetics, laboratory simulations of  complex  systems and
field data, we can explain the essence of acid generation.   These shortened
lists of species and processes (elementary  reactions when possible) will
require further testing, such  as zero-dimensional  sensitivity calcula-
tions.  In some cases, such as gas-phase species (i.e., hydrocarbons),

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the grouping into representative categories  has  been  done  in  AQM  research
previously, so only refinements will be needed for ADM  development.   In
other cases, such as solution-phase chemistry, it  is  not yet  completely
clear how to achieve conciseness in the reaction list while still  simula-
ting the essential features and rates  of  reactions.  This  is  partly  because
the role of in-cloud chemistry in generating acids has  been appreciated
only recently.

     Certain clear indications of how  to  proceed in ADM development  do ap-
pear in the course of our review.  For example,  because all gas-phase pro-
cesses that lead to S02 oxidation are  initiated  by the  gas-phase  OH  radical
(in daylight, of course), it is clear  that the major processes  that  control
OH concentrations must be embodied in  the minimal  reaction  set  for the
ADM.  Similarly, because of its role in NOX  chemistry and  because it is  a
major source of OH, tropospheric 03 must  be  calculated  accurately.  In the
liquid phase, it will be necessary to  simulate behavior of  03,  H202,  OH,
H02, N03, and probably 02~ and N205.   Fortunately, there  is a large  and
talented group of chemists working worldwide on  precisely  the reactions  of
interest and there are several international panels who meet  regularly to
prepare critical reviews of progress in chemical kinetics,  so the funda-
mental data necessary in ADM development  are forthcoming  or are largely
available already.

Acid Deposition Model Development and  Testing

     In Chapters IV, V, and VI, we face many of  the issues  that arise in
the design of a comprehensive model, i.e., one which  includes coupled mete-
orology and chemistry.  The key meteorological and chemical processes that
are identified in the earlier chapters are stated  more  concisely  in  Chapter
VI, and certain other phenomena and practical considerations  are  introduced
into the discussion.  For example, we  discuss the  apparent  importance of
dry deposition of acidic gases and particles, the  available methods  for  its
measurement, the controlling physics and  chemistry, and how an  ADM might
treat dry deposition.  We also introduce  in  Chapter VI  the  questions  and
facts concerning surface emissions of  pollutants and  natural  sources  of
acid precursors and of those species that regulate acid generation.   Other
general features, components, and questions  in ADM development  are also
reviewed and summarized in Chapter VI.  These include model resolution,
subgrid-scale processes and how to begin  to  treat  them, mathematical  and
numerical techniques for large comprehensive models,  special  considerations
for clouds that arise out of the need  to  couple  chemistry  and physics, and
issues in model validation and sensitivity analysis.

     While there are many issues and potential problems involved  in  the
development of a comprehensive acid deposition model  and  its  framework,  it
is clear that this field is ripe for progress.  The two principal  disci-
plines that are involved, meteorology  and atmospheric chemistry,  have made
dramatic if separate progress recently.   Early attempts to  include meteoro-
logical and chemical processes in integrated models have  been useful  al-
ready, and the experience of the contributing scientists  can  be tapped.
Computational facilities and methods are  up  to the task.  With  appropriate
amounts of enthusiasm, realism, resources, and teamwork,  a  new,  greatly
improved generation of acid deposition models can  be  born.

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                                CHAPTER ONE

                         THE ACID RAIN PHENOMENON:
                       A GENERAL PHYSICAL DESCRIPTION
Overview and History

     Although the pH scale to describe and quantify  the  acidity  of  aqueous
solutions was not developed until 1909, the occurrence of  acidic  rainfalls
was recognized at least 250 years ago.  Even the  terminology  "acid  rain"
was in use in 1872, if not earlier.  Further, the  rough  geographical  pat-
terns of acidic rainfalls, their origins  in industrial effluents, and ob-
servations of damage to biological systems and to  physical  structures—all
of these were noted over 100 years ago in Europe.  In the  twentieth cen-
tury, more quantitative analysis, mostly  in Europe,  revealed  the  identity
of the principal acids, anions and cations in precipitation.   In  1948,  the
first network of stations to collect and  analyze  the chemistry of precipi-
tation was established, again in Europe.  By the  mid-19501s,  the  European
(mostly Scandinavian) networks were gathering useful data.  Isolated stud-
ies of precipitation were undertaken in the United States  in  the  late
1950's and 1960's, and one United States  collection  network operated be-
tween 1960 and 1966.  These facts and many other  pieces  of the historical
record can be found in a review by Cowling (1982).

     Thus, it can be seen that acid rain  is not a  newly  recognized  problem,
nor is it a new phenomenon.  What is new, especially in  the United  States,
is the public awareness of the potential  effects  and probable causes of
acid rain.  There are also other new features of  acid rain that  are more
important from a research point of view.  These are:  (a)  our perception  of
the quantitative questions that must be answered  to  gain a full  understand-
ing of the essential chemical and meteorological  processes, and  (b) our
ability to investigate the questions with field-  and laboratory-measurement
programs and with mathematical models.  Similarly, from  the point of view
of those who are concerned with the effects of acid  rain,  there  now exist
reasonably logical and mature formulations of (c)  relationships  between
ecological systems (and physical structures) and  acid rain that  can be
investigated quantitatively.

     In the remainder of this report, we  examine  the full  range  of  meteoro-
logical and chemical processes that are involved  in  the  overall  phenomenon;
that is, the production and deposition of acidified  rain,  snow,  fog, mist,
and dry deposition of acid anhydrides over important inhabited regions such
as the east central United States and Canada.  We  pay particular  attention
to issues in the study of acid rain through mathematical models.  While the
scientific questions must dictate the kinds of field measurements,  labora-
tory experiments, and model development to be undertaken (all  of  which are

                                     8

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necessary), we are particularly interested  in  how  to  develop  and  employ
credible models.  By credible models, we mean  those that  can  pose testable
hypotheses and guide the design and  assessment of  field-measurement pro-
grams, with the eventual goal of predicting acid deposition  rates and
spatial patterns and of providing reliable  estimates  of the  effects of
emission-control strategies.

The Physical Picture

     The Earth's atmosphere, although often perceived as  calm,  benign, and
stable, is far from a static system.  As a  fluid,  it  supports both laminar
and turbulent flows, and each of these  is characterized by a  spectrum of
spatial scales, time constants, and  distinct measures of  repeatability.
Further, physical transformations occur in  the air and at the surfaces of
land, ocean, vegetation, and on airborne surfaces, e.g.,  on  solid-particle
and cloud-droplet surfaces.  Phase transitions are dramatic  and dynamic  oc-
currences that not only modify the form of  material  (e.g. H20)  at the mi-
croscopic level, but also represent  major entries  in  the  atmospheric energy
budget.  Finally, a rich variety of  chemical phenomena occur  in the atmo-
sphere.  Homogeneous chemical reactions, both  gas-phase and  liquid-phase,
take place, as do heterogeneous (mixed-phase)  reactions,  involving gases,
liquids, and solids.  Driven by visible and ultraviolet photons,  internal
chemical energy, and enhanced by surfaces,  these reactions combine to make
the Earth's atmosphere oxidizing.  Thus, gases such as H2S or CH4 released
into the atmosphere are eventually oxidized to S02 and C02,  respectively.
Conversely, gases with sulfur, carbon,  or nitrogen in reduced valence
states, e.g. H2S, CH4, NH3, are not  produced in our atmosphere—they are
only destroyed (oxidized).  Combustion  in air  is such an  oxidation process
in which natural gas, mostly CH^, becomes C02  and  CO, sulfide (organic or
mineral) becomes S02, etc.  Further, S02 in air (with sulfur  in the (+4)
valence state) eventually is converted  (oxidized)  to  the  (+6) valence
state, sulfate.  The strong tendency for oxidation of substances  to occur
is due fundamentally to thermodynamic equilibria states for  gas mixtures
such as air with 21% 02.  Specific kinetic  limitations dictate  the speed  at
which equilibria are approached.

     Understanding and modeling the  acid rain  phenomenon  requires one to
recognize a wide range of physical and  chemical processes and their inter-
actions.  Briefly, these are (a) emissions  of  materials that  cause and reg-
ulate acidity in precipitation and deposition,  (b) meteorological motions
that transport and dilute the emitted substances laterally and vertically,
(c) the variety of physical and chemical transformations  that alter the
physical phase and chemical properties  (e.g. valence  or oxidation state)  of
the emitted substances, and (d) the  meteorological factors that lead to
transport and deposition of the transformed substances.   A less well  recog-
nized set of questions surrounds those  properties  of  the  Earth's  surface
that control the rate of uptake of downward depositing dry materials, e.g.
gaseous S02 and HN03 and/or airborne particles.

     Because the principal acids in  precipitation  are sulfuric  (H2SOif) and
nitric (HN03), we are most concerned with emissions of sulfur and nitro-
gen.  Estimates of anthropogenic emissions  of  S02  (mostly from  coal- and
oil-burning electrical power plants  and metal-smelting plants)  and of NOX

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(mostly NO and N02 from high-temperature combustion processes  including
auto and truck engines) are reasonably reliable for the world's  industri-
alized countries.  Much less credible, but probably less  important,  are
estimates of natural emissions of organic sulfur gases and  of  natural  NOX
compounds.  Natural sources of gaseous NH3 and particulate  NH^"1",  gaseous
hydrocarbons, airborne mineral dusts, and lightning-produced NOX  must
also be estimated reliably.  Minor contributions to precipitation acidity
from HC1  and organic acids are often, but not always, negligible.

     Whether the key emissions are anthropogenic or natural, they are  in-
jected into the atmosphere at or near the Earth's surface,  certainly within
the planetary boundary layer.  Accordingly, boundary layer  meteorology is
at the core of the acid rain problem.  The physics of turbulence  and con-
vection,  diurnal variation in surface heating, terrain geometry,  and sur-
face and boundary layer hydrology exert strong control over the  initial
dispersion of the emitted substances.  Further, during the  time  these  sub-
stances spend in the boundary layer, their physical environment,  e.g., tem-
perature, pressure, humidity, available sunlight, and proximity  to surfaces
and to other pollutants such as aerosol particles, controls the  rate and
type of chemical transformations that occur—and they are markedly differ-
ent from those that are favored above the boundary layer  in the  free tropo-
sphere.  There is perhaps only one important acid precursor or regulator,
NOX from lightning, that does not begin its atmospheric life in  the
boundary layer, although sporadic subsidence of stratospheric  ozone is
occasionally of interest.

     In dirty or clean air, in the boundary layer and above, chemicals
react with each other.  The precise  rates and types of reactions  depend
strongly on the local  pressure, temperature, available sunlight  (both
direct and scattered), the presence  of liquid and vapor H20, and  on the
local chemical composition, i.e., the spectrum of available chemical co-
reactants.  In the later sections of this report, we attempt to  organize
our discussion into categories of homogeneous reactions,  gaseous  and li-
quid, and heterogeneous processes and by principal categories  of  chemical
species.  Key considerations include the exact rates of transformation
(oxidation) of S02 and NOX into r^SO^ and HN03, the major pathways of
transformation and the essential controlling agents.

     As noted earlier, the oxidation of S02 and NOX to H^SO^. and  HN03  is
inescapable, given enough time in the atmosphere.  Practically,  however,  it
is very important to know whether all of a region's emissions  are so trans-
formed or whether the oxidation processes are interrupted by deposition  of
the materials to ground level before complete acidification or whether the
materials are transported very long  distances, for example, at high alti-
tudes for eventual deposition into the Atlantic Ocean or  even  to  Europe.
This is to say that a credible description and model of this physical  sys-
tem must include quantitative treatment of material transport  and transfor-
mation above the boundary layer.  Similarly, the factors  that  limit the
rate of surface deposition and uptake of gases (dry deposition) must be
treated quantitatively.  These include near-ground turbulence, the condi-
tion and type of the surface (e.g.,  vegetation, soils), and the  chemical
stickiness and reactivity of the relevant substances on the surfaces.
                                     10

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                                CHAPTER TWO

               THE ROLE OF MODELS IN ENVIRONMENTAL ASSESSMENT
     All  decision-making processes in society  require  the  gathering  of
quantitative data to minimize the chances of unforeseen  risks  and to ad-
dress cost-benefit analysis properly.  In most of the  physical  and natural
sciences, direct experimentation on alternative concepts or  procedures pro-
vides the most reliable quantitative data for  such purposes.   In  the envi-
ronmental sciences, however, direct experimentation  is highly  perturbing  to
some segments of society and hence is not often feasible.

    The only recourse is through carefully-developed systems of indirect
probes, culminating in an integrated theoretical system  which  describes the
coupling and feedback processes among many relevant  and  quantifiable physi-
cal phenomena.  This theoretical system is most conveniently expressed as a
set of mathematical equations.  These equations and  the  associated input
data necessary for the construction of their solutions then  constitute the
"model."  The model by itself is not the ultimate goal;  rather, the  model
is a tool to facilitate integration of scientific information  and to pro-
vide a systematic procedure for studying causal relations.  A  well-devel-
oped model supported at all stages of its development  and  subsequent appli-
cations by quality experimental data is the most non-intrusive and economi-
cal tool  for any environmental assessment program.   A  model  can represent
the best judgment and best available information.  Society should not be
unduly apologetic for using such a tool in assessment  studies,  as long as
proper emphasis has been placed upon any analyzable  uncertainties it con-
tains.

     In both the scientific study of regional  acid precipitation  and in
devising industrial and governmental responses to it,  the  role of mathe-
matical models is central.  From an industrial and governmental point of
view, one looks toward predictive and/or simulation  models for guidance in
assessing the effects of man's activities—for example,  in predicting how
altered pollutant emissions and meteorological conditions  change  the depo-
sition of acids and other substances regionally.  In the overall  task of
determining the causes of acidic precipitation, assessing  the  severity of
its effects, and devising control strategies,  we need  models  (and the the-
ories they embody) that are technically sound, testable, and as broadly ap-
plicable as possible.  From a purely scientific point  of view,  models first
synthesize the best available theories and data and  then calculate the val-
ues of measurable quantities in space and time.  Empirical comparisons with
physical  data and new ideas or hypotheses are  then employed  to refine or
reformulate the model.  The more real features that  can  be simulated or
predicted successfully by a model, the more confidence we  develop in its
ability to predict results of perturbations to the system—perturbations

                                     11

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for which there are no experimental  results,  e.g.,  a hypothetical  IB% in-
crease in S02 emissions in a given  region.  Models  are  also used to guide
field and laboratory measurements.

     The acid rain problem has  important  societal and economic ramifica-
tions.  Scientifically, it is characterized by  a  rich variety  of physical
and chemical phenomena.  Therefore,  it  is  essential  for any serious mathe-
matical  modeling effort in this field to  recognize  that all  possible scien-
tific completeness and rigor must be sought,  and  that practical  applica-
tions of the model will ensue.  In  the  design of  any useful  comprehensive
model, one must take great care to  ensure  that  each component  of the model
will be defensible, i.e., scientifically  sound.   For example,  the  input
data and each step of the sequence  of chemical  and  physical  phenomena must
be logical and as realistic as  possible.

     A well-constructed acid deposition model should,  in its maturity,  em-
body all relevant physical and  chemical phenomena and thus serve to inte-
grate results from the full spectrum of acid  rain research.  The model
should be highly modular, enabling  relatively easy  changes in  data input
and in physical and chemical parameterization.  Although initially such a
model will probably be designed for a particular  geographical  region such
as the northeastern United States and southeastern  Canada and  for  a speci-
fic resolution, a modular structure would  allow easy adaption  to other re-
gions and other resolutions.  The model could then  serve as a  primary as-
sessment tool in the identification of  future mitigation studies by defin-
ing source-receptor relationships on a  regional scale.
                                      12

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                                CHAPTER III

                         REVIEW OF EXISTING MODELS
1.  AIR QUALITY MODELS

1.1  Introduction

     Historically, the development of air quality models focused  on  the
urban scale (about 50 km), where the ozone and nitrogen oxides  problem was
thought to originate and reside.  Recent field measurements  indicate  that
03 and its precursors {nitrogen oxides and hydrocarbons) are  often trans-
ported over hundreds of kilometers (regional or mesoscale).   Furthermore,
the European OECD program on the Long Range Transport of Air  Pollutants
(LRTAP) has demonstrated that transport and deposition of  sulfur  compounds
occur over the continental scale (over 1000 km).  Therefore,  models  ranging
from urban scale to continental scale have been developed  to  study the
transport, transformation, and deposition of air pollutants.

     Acid deposition models which deal with long-range transport  of  sulfur
and nitrogen species are continental-scale air quality models.  Current
acid deposition models contain highly simplified parameterizations of chem-
istry and transport processes because of limited manpower  and computer re-
sources.  Local and mesoscale air quality models, because  of  their smaller
sizes, consider these processes in various degrees of detail.

     According to the chemistry involved, air quality models  can  be  divided
into two groups:  reactive models and nonreactive models (Demerjian,
1978).  Reactive models are developed primarily to address the  problem of
atmospheric oxidants.  Pollutants typically considered in  these models are
hydrocarbons (HC), S02, nitrogen oxides (NO and N02), and  03.   Models that
consider only  inert pollutants such as particulates  or CO  (inert  within  the
model) are concerned primarily with the dispersion or transport of these
pollutants.

     Models can also be distinguished by their treatment of  the transport
of atmospheric pollutants.  There are two basic types of models used  for
studying long-range transport of pollutants—the  Eulerian grid model and
the Lagrangian trajectory model (Seinfeld, 1975; Liu and Seinfeld, 1975;
Eliassen, 1980).  A variant of the latter type is also known  as a Gaussian
plume model.  A third type of model has also been identified—namely, the
statistical trajectory model (Johnson, 1981; Venkatram et  a!.,  1982), al-
though conceptually this is simply a time-and-space-averaged  Lagrangian
trajectory model with extensive use of climatological data on an  Eulerian
grid (Small and Sarnson, 1983).
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1.2  The concepts of Eulerian and Lagrangian models

     The designation and classification of model types  has  evolved during
the past two decades or more.  Today, many models are "hybrids"   which  in-
clude essential characteristics of both basic types of  models.   For exam-
ple, an Eulerian grid model may include subgrid-scale plumes  or  "tracer
particles" to enhance resolution, and current Lagrangian  trajectory models
usually include an Eulerian grid to map the pollutant concentrations re-
presented by the moving Gaussian plumes onto the geographical  area under
study.
                                               are constructed  with  speci-
                                               (technical  or  financial).
                                               mathematical equations  re-
                                               of  interest within  some con-
     An extensive critique of these types of models would  necessarily  in-
volve many model-specific details, but for our purposes  this  is  not the
most constructive approach.  Individual models
fie objectives and under different constraints
All models are basically no more than a set of
presenting the physical and chemical processes
ceptual framework and associated data.  This underlying  conceptual  frame-
work actually determines the type of model, and  there  are  only  two  major
elements in the conceptual frameworks distinguishing all existing models
(and most likely all models)--namely, reference  systems  and  discrete mathe-
matical representations.  The choice of reference  systems  determines how
all relevant physical processes must be modeled, and the choice  of  discrete
mathematical representations determines how the  model  may  be  analyzed and
interpreted.

     In the Eulerian approach, the observer adopts a fixed frame of refer-
ence, usually the surface of the earth.  In the  Lagrangian approach, the
observer adopts a moving frame of reference, usually fixed to the  bulk mo-
tions of the fluid or materials under consideration.   From a  purely theore-
tical viewpoint, these two approaches are equivalent,  and  any formal mathe-
matical description in one frame of reference can  always be  rigorously
transformed to the other.  However, this is no longer  true after specific
models of the physical processes involved are combined into  the  overall
model (Seinfeld, 1975; Richtmyer and Morton, 1967; Liu and Seinfeld, 1975;
McRae et al., 1982).  For example, let us consider the one-dimensional
Eulerian conservation equation for material c,
                         at
                                !£
                                ax
                                          ax
                                                                         (1)
where c is the local concentration of the material,  v  is  the  mean velocity,
D is the diffusivity, and S  is the local source/sink function for c.   If v
is constant, Equation (1) can be transformed  to  the  Lagrangian  reference
frame with the new coordinates (x',t'), where  x'  = x - vt and t1  = t,
                           ac
                           "at1
                                                                         (2)
D' and S1 are to be determined with  respect  to  the  moving  reference frame.
Equations (1) and (2) illustrate the  fundamental  differences  between Euler-
ian and Lagrangian models.  In the Eulerian  model  (Eq.  (D),  it is diffi-
                                      14

-------
cult to represent numerically the advection  term,  v  gc/ax  (Liu  and Sein-
feld, 1975; Crowley, 1968) without introducing  artificial  numerical  diffu-
sion.  The modeling of diffusion processes  in an Eulerian  framework  is also
difficult.  On the other hand, most of  the  source  and  sink  processes are
more easily formulated in the natural,  geographically-fixed frame.  In the
Lagrangian frame (Eq. (2)), there is no advection  term and  it can  be con-
ceptually simpler to determine D1.  However, the difficulties in  describing
arbitrary source functions and sink processes are  almost  insurmountable.
Only the simplest (and admittedly highly  incomplete)  representation  has
been used in existing models.

     Equations (1) and (2) are only illustrative of  the fundamental  charac-
teristics of the mathematical equations involved in  long-range  transport
and acid rain modeling.  Usually the model  includes  many  such equations in
multidimensional space, and all are coupled  to  each  other.   This  system,
then, can only be solved numerically on the  computer.   Both the Eulerian
and Lagrangian models are assumed to be valid over some mathematical do-
main, one fixed while the other moves over  the  same  fixed  physical domain.
Both mathematical domains can be discretized into  fine grids of finite size
and solutions c represented by discrete numbers c-j  at  each  grid posi-
tion.  Because of the limitations on computer speed  and memory, the  grids
are often coarser than desirable.  For  the  Eulerian  model,  this then re-
quires special treatment of the advection terms and  others. Although the
Lagrangian model avoids this difficulty,  it  introduces new  problems  such as
grid tangling.  Since each grid in the  Lagrangian  model moves with separate
velocity Vj, at times one grid can get  ahead of the  other  in their rela-
tive positions in the underlying fixed  physical space. This causes  a new
class of computational difficulties that  must be addressed. One  remedy is
the use of Gaussian plumes for representing  the discrete  Lagrangian  compo-
nents of the solution c.  In such a model, c is represented by  special
mathematical functions (Gaussian functions)  or  a set of such functions
which are special solutions to Equation (2)  under  very limited  conditions
(Seinfeld, 1975; Liu and Seinfeld, 1975;  Lamb and  Seinfeld, 1973).  This
avoids the difficulties intrinsic to the  Lagrangian  grid,  but severely
limits the generality of the model.  In particular,  the Gaussian  plume
model cannot properly represent nonlinear processes  and continuous source
functions.

     It is essential to note that, although  the concepts  of Eulerian and
Lagrangian models are comparable, the concepts  of  grid discretization and
Gaussian plumes are not of comparable generality.  The Gaussian representa-
tion is highly specialized and non-flexible.  Any  direct  comparative evalu-
ation of the advantages and disadvantages of Eulerian  grid  models  with La-
grangian trajectory models is flawed because of the  lack  of suitable mea-
sures of generality and flexibility.

     For the purpose of using a long-range  transport model  as a primary
assessment tool in studying acid rain source-receptor  relationships  and
control strategies over different geographical  areas and  possible  source
distributions, only grid-type models are  of  sufficient generality  and flex-
ibility.  There is very little information  available on developing Lagran-
gian grid models in three dimensions.  This  leaves Eulerian grid models as
the only viable general approach.  As will  be shown,  recent progress in

                                     15

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modeling atmospheric dynamics and chemistry makes  it very  realistic  to
develop such a coupled Eulerian grid model for application at this time.

1.3  Local  and mesoscale air quality models

     Numerous publications in the scientific modeling literature  survey and
review models appropriate for geographical regions up to distances of 50
km.  The majority of these models, especially the  simpler Gaussian models,
do not include provisions for simulating chemical  transformation, dry depo-
sition, wet deposition, and non-steady meteorological conditions.  Because
many references to these models are available in the literature,  we  will
provide here only a brief discussion of recent publications.

     An excellent review paper (Turner, 1979) provides an historical per-
spective of atmospheric dispersion models, many references to particular
models, and includes an appendix which lists those models contained  in the
computer tape, "User's Network for Applied Modeling of Air Pollution"
(UNAMAP).  Turner's review paper is commented on by peers in a  later report
(Egan et a!., 1979).  A more recent model survey by Liu et al.  (1982) in-
cludes an evaluation of existing atmospheric dispersion models  appropriate
for estimating air pollution concentrations from elevated point sources.
Thirty existing plume models were evaluated and analyzed.  These  consisted
of nineteen kinematic models, nine first-order-closure models,  and two se-
cond-order-closure models.  The formulation and the technical attributes of
each of the thirty plume models were compared and  examined for  differences
and similarities.  A sensitivity analysis was carried out on the  Gaussian
plume models to explore systematically what effect varying the  different
algorithms would have on the overall model prediction.  This sensitivity
analysis can assist a user in deciding which model is most appropriate for
a particular application.

     Stewart and Liu (1982) have included mesoscale air quality models in
their recent review of long-range transport acid deposition models and in-
termediate-range regional models.  In addition to  the common basic attri-
butes of these models, i.e., transport and diffusion, transformation, and
deposition, they considered other features that are important to  mesoscale
models.  These include model capability in resolving vertical pollutant
distributions, accommodating urban emissions, and  simulating detailed
chemi stry.

     Mesoscale models usually have good vertical resolution for better re-
presentation of the vertical distribution of pollutants.  They  also  allow
for better treatment of emission heights of pollutants and dry  deposition.
However, transport above the planetary boundary layer is not included in
mesoscale models, nor are cloud physics or chemistry.

     A recent emissions inventory compilation for  the EPRI/SURE region
(Klemm and Brennan, 1981) indicates that point sources and urban  sources
(industrial, commercial, residential, and transportation) contribute 87% of
the total sulfur emissions and 62% of the total nitrogen emissions.  For
acid deposition models, urban sources are subgrid  sources, and  no attempt
is made to account for the effect of subgrid inhomogeneity.  The  mesoscale
grid models (i.e. Eulerian models) usually have the capability  to treat

                                     16

-------
urban emissions with little or no modification.

     Lagrangian models may easily incorporate urban emissions  if  they  are
receptor-oriented.  In these models, emissions are gridded and  input into  a
trajectory segment, or air parcel, as they  flow  toward  a  receptor.  How-
ever, the lack of vertical resolution in these models makes them  less  ap-
plicable to intermediate- and long-range assessments.

     Source-oriented Lagrangian models may  have  adequate  vertical  resolu-
tion, but the puff or plume segment dimensions and their  dispersion rates
are normally designed for point sources.  Many of these models  would re-
quire considerable modifications to make them useful for  intermediate-range
urban plume applications.

     Several local and mesoscale models have incorporated detailed photo-
chemical submodels that are based on elementary  reactions and  basic mechan-
isms.  Demerjian  (1976, 1978) and Turner (1979)  made extensive  reviews on
the formulation,  validation, and application of  these models.

     The present  photochemical models are built  on several decades of  re-
search on photochemistry of urban air pollution  that involves  laboratory
kinetics, field observation, and theoretical studies.   Studies  using smog
chambers have led to the development of detailed chemical models  (Niki et
al., 1972; Demerjian et al., 1974).  Unfortunately, the chemistry  in these
models is far too extensive to be incorporated into air quality computer
models.  To circumvent this problem, at least two approaches have  been
utilized.  These  involve "lumping" the hydrocarbons by  classes  and using  a
generalized reaction mechanism for these classes (McRae et al., 1979;  At-
kinson et al., 1982), or using the carbon-bond approach (Whitten  et al.,
1980), which partitions the chemical species based on the similarity of
their chemical bonding.  These chemical models have been  tested against and
tuned to a variety of smog chamber data.  Usually good  agreement  is
achieved between  measured and predicted concentration-time profiles for all
measured species.  When these reaction mechanisms are incorporated into air
quality models and compared to field measurements, the  agreement  becomes
much poorer.  Discrepancies could be due to poor transport parameter!za-
tions, but there  is little doubt that lack  of understanding of  the chemis-
try in the real atmosphere also contributes.  In particular, the  chemistry
of aged and diluted air pollutants may be poorly understood because it can-
not be effectively tested in smog chambers.  Chemistry  in this  regime  is
probably most important for acid deposition models.

     Although these chemical models are not directly applicable to acid
deposition modeling, further developments outlined in Chapter  V of this
report suggest the potential for constructing an appropriate chemical  model
for acid deposition considerations.  Furthermore, experience gained in stu-
dying air quality model chemistry, both physical and computational, can
provide guidance  for the proper modeling of acid deposition chemistry.

1.4  Acid deposition models

     There exist  several excellent reviews  on LRTAP and acid deposition
models; for example, papers by Dittenhoefer (1982), Eliassen (1980), Bass

                                     17

-------
(1980), Fisher (1978), Pack et al. (1978), Smith and Hunt  (1978),  Eliassen
(1978), the earlier work of Eliassen and Saltbones (1975), Fisher  (1975),
and Scriven and Fisher (1975), among others, capture well  the  essential
results and conclusions obtained by the community of acid  deposition
models.  The OECD program reports on LRTAP and the Phase II and  III reports
prepared by the U.S.-Canada Work Group in accordance with  the  Memorandum of
Intent on Transboundary Air Pollution made extensive reviews of  current
available acid deposition models for Europe and eastern North  America.  It
would be impractical to review here the more than ten operational  acid
deposition models and the many other models under development.   We will
focus our discussion on the operational models of eastern  North  America.
Most of these are Lagrangian models.  In fact, most of the currently
available Eulerian models are in essence simply expanded urban scale
models.  They account for physical  processes that occur during daylight
hours and within about 10 km of a source (Lamb, 1982).

     Because of the important need for a comprehensive Eulerian  model, as
stated before, we will review here some of the recent efforts  in developing
these models.

a.  Lagrangian acid deposition models

     Table 1.1, which is condensed from the U.S.-Canada Work Group Phase
III report, lists the important features of three representative Lagrangian
acid deposition models and gives a general overview of the major components
of each.  Selection of these models is not based on their  quality, but
rather on the representativeness of their coverage of physical and chemical
processes.  Other models with similar quality are UMACID (Samson,  1980),
OME/LRT (Venkatram et al., 1980), CAPITA (Patterson et al., 1981), and
MEP/LRT (Weisman, 1980).

     These models usually consist of two major components—the meteorologi-
cal component that contains the preprocessed wind field and precipitation
data, and the tracer component that uses wind and precipitation  data  as
inputs and treats emission, transport, transformation, and deposition of
pollutants.

     The meteorological components are preprocessed from observed  wind
field and precipitation data.  The resultant wind and precipitation data
are stored and used as input for the tracer components.  There has been no
attempt to distinguish between different types of precipitation, such as
rain from snow, or frontal from convective precipitations.  Wind fields are
obtained from objective analysis of the winds observed at  upper-air sites.

     In these models, the mixing heights are parameterized independently
from wind fields and precipitation activities.  With the exception of the
ASTRAP model, only one layer is assumed and the mixing within  the  layer is
assumed to be instantaneous; i.e., it is a continuously-homogeneous layer.
The ASTRAP model has nine sublayers in its boundary layer, and diurnally-
changing stability and nighttime inversion layers are considered.  There  is
no consideration of mixing pollutants across the upper boundary.   Horizon-
tal mixing is treated in several different ways.  All models assume that
horizontal mixing is independent of thermal structure or convective acti-

                                     18

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vities.  The ENAMAP model uses time-dependent eddy  diffusion  coefficients,
while the ASTRAP and AES models calculate long-tern dispersion  directly
through the distribution of simulated trajectories.

     All models except ASTRAP assume S02 emissions  to  be  at one level.   The
ASTRAP model distributes the emissions vertically as a  function of  stack
parameters.  No natural emissions of sulfur  compounds  are considered.
Emissions of SQ^= are considered by all models.  Nitrogen oxide emissions
are not considered at present.  Some models  now  include nitrogen compounds
in the same manner as sulfur compounds.

     No elementary chemical gas phase kinetics or mechanism has been  in-
cluded in any of the existing models.  The transformation of  gas phase  S02
to S04= is assumed to be linearly proportional to S02  and to  be independ-
ent of cloud cover, temperature, and composition of the ambient air.  The
AES model assumes a rate of 1% per hour for  the  transformation  of gas phase
S02 to SOi+=.  The ASTRAP and ENAMAP models consider seasonal  and diurnal
variations in the transformation rate, but always a linear form; aqueous
phase chemistry is not considered.  The S02  scavenged  by  precipitation  is
assumed to be transformed instantly to SOi^.

     The rates of scavenging for S02 and S04= are assumed to  be independ-
ent of types of precipitation, temperature,  or pH value of the  precipita-
tion.  Scavenging and transformation of S02  to SO^" by  clouds are not
considered.  The rate of removal of S02 and  SQk= by precipitation is
assumed to be linearly proportional to the amount of precipitation  and  S02
or SO^3.

     Dry deposition for S02 and 30k~ is assumed  to  be  independent of wind
field, turbulence mixing, topography, vegetation, or surface  moisture.   Re-
cently the ENAMAP model incorporated a dry deposition  velocity  that depends
on land use and atmospheric stability.  The  dry  deposition velocity is  al-
lowed to vary diurnally and seasonally in some of the  other models.

     Subgrid inhomogeneities in emissions, transport,  transformation, and
wet and dry depositions are ignored by assuming  uniformity.

b.  Eulerian acid deposition models

     As stated earlier, because of the large demands for  manpower and com-
puter resources, Eulerian acid deposition models developed so far are ei-
ther highly simplified or relatively incomplete.  This  is reflected in
Table 1.2, which shows some important features of four  Eulerian models.
Except for the RCDM model, all others are used only in  the episode  mode.
Seasonal and annual source-receptor relationships cannot  be readily estab-
lished in these models.  On the other hand,  the  RCDM is highly  simplified
so that analytic solutions can be obtained for the  continuity equations  of
S02 and SOU=.

     Although RCDM is an Eulerian model, its treatments of transport  and
chemistry are quite similar to the Lagrangian models discussed  in the pre-
vious section.  The episode models (ERT, STEM, and  EPA) employ  approaches
significantly different from the Lagrangian  models:

                                     21

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     (1)  Chemical transformations are much more  sophisticated.   Basic
          reactions are included instead of an overall  parameter.

     (2)  Liquid-phase reactions are considered separately  from  gas-phase
          reactions, allowing the treatment of the  important  cloud  chemis-
          try.

     (3)  Much better vertical resolution and better treatment of diffusion
          is possible.

     (4)  Dry deposition velocity is calculated self-consistently.

     The EPA model is the most sophisticated model  with  its 16 km x 16  km
horizontal resolution and rigorous treatment of horizontal  and vertical
transport.  It also allows for above-boundary-layer transport of air pollu-
tants.  Since it is still  under active development, detailed  assessment of
this model is not possible at this time.

     At present, none of the three episode models includes  precipitation or
cloud.  It is important to include precipitation  and cloud  in a  way that is
consistent with the meteorological model.  Furthermore,  in  order to study
the long-term source-receptor relationship, it is essential to extend the
ability of episode models to assess monthly or even seasonal  effects.

1.5  Verification of acid deposition models

     The verification of acid deposition models is  hampered mostly  by lack
of data.  There is no systematic data set on simultaneously-measured con-
centrations of S02 and SO^- and fluxes of dry and wet  depositions of S02
and SOtf3.  In fact, dry deposition and horizontal fluxes  are  not routine-
ly measured.  Routinely measured ambient concentration  and  wet deposition
show poor spatial and temporal resolution.  Vertical distributions  of S02
and SOi^ are practically nonexistent, especially  above  the  boundary lay-
er.  Furthermore, accuracies and qualities of existing  measurements are not
uniform.  These factors make it difficult to test rigorously  the degree of
accuracy of model calculations.

     There have been several studies comparing acid deposition model  calcu-
lations and measurements of S02 and S04= concentrations  and sulfate depo-
sition (Bhumralkar et a!., 1980; Olson et al., 1979; Powell et al., 1979;
Niemann et al., 1980; Shannon, 1981; Shannon et al., 1982).   Furthermore,
the Phase II and III reports by the U.S.-Canada Work Group  have  conducted
model intercomparisons.  Figures 1.1, 1.2, 1.3a,  and 1.3b illustrate some
results of these studies.  Figure 1.1 is taken from Olson et  al. (1979),
and shows the AES model computed versus measured  daily  mean sulfate concen-
trations during October 1977 at Port Huron, Michigan.   Figure 1.2 compares
the S02 concentrations for October 1977 calculated  by  the ENAMAP-1  model to
measured values (redrafted from Bhumralkar et al.,  1980).   Figures  1.3a and
1.3b show the annual sulfate concentrations simulated  by  the  RCDM model
compared to a three-year average (1975-1977) of AQCR sulfate  concentrations
(Niemann et al., 1980).  Discrepancies between observed  data  and model  cal-
culations could be due to neglect of natural sulfur emissions and sulfur
compounds entering the model grid from emissions  outside  the  grid bound-

                                     24

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    40 LI i i i



    35



    30
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 o
 v.
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 I   20

1

6   «5
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o
o
     10
5



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                                   1_L_1_L I I I I  I I I  I 1
                     10
                      15     20

                       DATE
25
30   35
       Figure 1.1    AES-LRT computed and measured daily mean  sulfate
      concentrations during "October 1977 at Port Huron, Michigan
      (measured-solid, computed-dashed).
                               25

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 Figure 1 2   S0.2 concentrations (ug/rn^) for October  1977
from ENAMAP-1.
                          26

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Figure 1.3a  Isopleths of annual sulfate concentrations
(ug/m3) simulated by the RCDM.
                               27

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                                                         10
Figure 1.3b   Three year average  (1975-1977) of AQCR
average sulfate  concentrations  (ug/m3).
                           28

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aries; no treatment of transport of pollutants  above  the  boundary  layer;
poor treatment of sulfur chemistry; use of emissions  inventory  data,  mete-
orological data, and monitoring data  corresponding  to different periods;
and deficiencies in the model treatments of  dispersion, terrain effects,
frontal and convective processes,  and clouds.   Furthermore,  inadequate
measurement coverage and deficiencies in measured data  as  mentioned earlier
also contribute significantly to the  discrepancies.

     The reasonable success  in the comparisons  between  model  calculations
and measurements may be misleading because it  is likely that  many  parame-
ters used by the models have been  tuned to obtain better  agreements.  -If
the tuning involved only one or two parameters, one could  design certain
independent experiments to determine  or to narrow the uncertainties of
these parameters.  However,  as discussed earlier, the present acid deposi-
tion models include numerous parameterizations  in the processes of trans-
port, transformation, and deposition  of pollutants.   Most  of  the parameter-
izations have uncertainties  much greater than  a factor  of  two.   Thus, there
is no unique combination of  different parameters that would  give reasonable
fit to the observed data.

1.6  Model sensitivities

     Since sulfur compounds  in acid deposition  model  emissions  often under-
go transport, transformation, and  deposition,  the model results are sensi-
tive to all major processes  involved  in these  four  steps.  The  most impor-
tant processes in simulating ambient  concentrations and wet  deposition are
identified by current acid deposition models to be  the  S02-to-sulfate chem-
ical transformation rate and the dry  deposition velocities for  S02 and sul-
fate.  Samson (1982) has demonstrated the high  sensitivity of model  results
to the chemical  transformation of  S02 by modifying  the  chemical  transforma-
tion mechanisms of the acid  deposition model of Rodhe et  al.  (1981).   He
obtained significant changes in SOi+=  concentration  and  deposition  rates
by changing only a few reactions involved in the S02  transformation.

     Model results are also  sensitive to the selection  of  the wet  deposi-
tion rate for SOi^ and S02,  for which considerable  uncertainties exist.
Model sensitivity to the transport by mean wind is  obviously  very  large.
On the other hand, horizontal diffusion apparently  does not  affect model
calculations strongly.  This is probably because horizontal  dispersion in a
regional-scale model is controlled primarily by variations in the  position
of the Gaussian plume center of mass.

     Vertical diffusion and  transport of pollutants above  the boundary lay-
er are probably important in the long-range  transport of  pollutants.   The
heights of S02 emissions also strongly affect  its dispersion, as low-level
emissions undergo far greater dry  deposition than elevated emissions.  Nei-
ther of these phenomena has  been studied because of the single-layer treat-
ment and minimal attention paid to the upper boundary condition in most of
the existing models.
                                      29

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1.7  Model limitations

a.  Emissions

     Near-surface emissions must be treated carefully, since otherwise  an
acid deposition model will over- or under-predict dry deposition  near the
sources.  Most models assume emission at the surface with  instant vertical
mixing.  This is a poor approximation, considering the frequent diurnal
variations in weak inversions.  Multi-level emissions in the multi-layered
model  offer definite advantages over the simpler approach.

b.  Chemistry

     Our current understanding of gas phase oxidation of S02 to S0tt= is
that the atmospheric OH radical is primarily responsible for initiating the
process.  The atmospheric concentration of OH radical is controlled by  so-
lar UV intensity, reactive hydrocarbons, nitrogen oxides,  ozone,  and water
vapor.  Thus, the concentration of OH is  expected to have large  spatial
and temporal  variations.  In addition, the OH concentration should vary
with the local  instantaneous levels of air pollutants.  A  constant linear
conversion rate for S02 gas phase oxidation to S0^= is clearly a  poor
approximation.

     Recent experimental evidence for the atmospheric aqueous phase oxida-
tion of S02 to sulfate shows that the conversion rate is fast, so the in-
stant conversion rate assumed by current models in below-cloud washout  pro-
cesses is probably a reasonable approximation.  This assumption makes the
rate of S02 scavenging by precipitation the rate-limiting  step of aqueous
oxidation of S02 to S04=.  Since the scavenging of S02 takes place mostly
in the cloud rather than as below-cloud washout assumed by current models,
one has to be skeptical of the overall parameterizations made in  the mod-
els.  Furthermore, recent results suggest that the aqueous oxidation of S02
is dominated by dissolved H202 and 03.  Therefore, it is quite conceivable
that availability of aqueous H202 or 03 may be the actual  rate-limiting
step under certain conditions.

     An important objective of modeling acid deposition is to establish the
source-receptor relationship between acid precursor emissions regions and
acid deposition regions.  Assumptions of linear S02 to SQ^" conversion
rates and linear scavenging rates of S02 and SOi+= by precipitation when
coupled to the linear Gaussian plume transport automatically leads to a
linear source-receptor relationship.  This may not occur in a model that
contains detailed chemical reactions and basic physical mechanisms.  In
fact,  it is conceivable that, in such a model, pH in the precipitation  at
one location may not decrease beyond a certain level when  S02 emissions in
the source region are increased.  This situation could occur if the species
responsible for oxidation of S02, such as OH, H02, and H202, became exhaus-
ted.  In addition, controls on the reactive hydrocarbon and nitrogen oxide
emissions may have significant effects on the S02 oxidation rate.  This can
only be studied in a model that is based on detailed chemical-physical
mechanisms.

     Neglect of the effect of clouds in the oxidation of S02 is probably

                                     30

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one of the most serious defects of existing acid  deposition  models.   Less
than 10% of clouds will result in precipitation;  the  rest  will  evaporate.
However, SOi^ formed in the clouds by aqueous phase_S02  oxidation  may
remain as SO^ aerosols when clouds evaporate.  SO^-  produced  this way
could be more important than the direct gas phase oxidation  of S02 to


c.  Transport

     There are a number of shortcomings in the  transport components  of  ex-
isting acid deposition models.  These include neglect of vertical  air,mo-
tions, clouds and convective motions associated with  clouds, transport  of
pollutants above the planetary boundary layer,  atmospheric thermal  struc-
ture, and wind shears.  The resulting situation is  further obfuscated by
the empirical vertical and horizontal mixing parameterizations.  A fuller
discussion can be found in Dittenhoefer (1982)  and  Bass  (1980).

     The wind field is usually represented by a boundary-layer-averaged
wind velocity.  The differences in the wind velocities at  various  heights
are ignored.  As Dittenhoefer (1982) has pointed  out,  there  is little
consensus among modelers concerning the proper  specification of the  wind
field.  Several techniques are used—all with minimal  a  priori  justifica-
tion.  Large errors may result from systematic  discrepancies in the  speci-
fication of wind field.

     Daniel sen (1961) has shown that neglecting vertical air motions can
lead to large horizontal deviations from the true advective  wind field.
Errors and uncertainties in wind direction can  cause  large errors  in spa-
tial predictions over long-range travel distances.

     The poor spatial and temporal resolution of  the  U.S.  upper air sta-
tions represents a serious limitation of the accuracy  of acid  deposition
models (Bass, 1980).  Soundings are made approximately 300 to  500  km apart
at 12-hour intervals and cannot resolve all important spatial  and  diurnal
variations in the wind field, temperature structure,  wind  shear, and mixing
depth.

     Convective activities can efficiently transport  pollutants above the
planetary boundary layer.  Once above the boundary  layer,  pollutants can  be
transported over long distances without being removed by dry or wet  depo-
sition and thus can contribute to a significant "background" SOi+~  concen-
tration and deposition over clean, remote areas.

     In the boundary layer, as the turbulence activities during the  daytime
hours decrease near sunset, pollutants may remain aloft  and  become decou-
pled from surface deposition mechanisms.  Pollutants  trapped aloft tend to
be transported over long distances because they are frictionally decoupled
from the surface.  This mechanism is believed to  be responsible for  trans-
porting urban oxidants to rural areas during nighttime hours.   In  addition,
atmospheric thermal structure often involves weak,  temporal  inversions,
resulting in pollutant layers that are alternately  coupled and decoupled
over a diurnal cycle.  Different wind velocities  present in  these  layers
obviously need to be properly treated in the models.

                                     31
                                                      US
                                                      CQPVAUJ6 ENVIRONMENT- -W.SCARTH .
                                                          nrnwai , « nflBQON 97333

-------
     Vertical mixing in the boundary layer is assumed to be  instantaneous
in most models.  Models with multi-levels in the boundary  layer  in  which
the vertical diffusion equation is solved using K-theory (Shannon,  1981)
offer certain advantages over other schemes.  Further improvements  would be
the inclusion of multi-layer advection and appropriate turbulent mixing
submodels based on local dynamical conditions.

d.  Deposition

     Dry deposition depends upon two major processes:  the aerodynamic
transport of pollutants down to the immediate vicinity of  the  surface,- and
the diffusion through the laminar surface sublayer to reaction sites  on the
surface.  The former is a turbulent process involving the  transport through
the lower boundary layer, the surface layer, and depends upon  atmospheric
stability, wind fields, surface roughness, and other factors.  The  second
process involves the diffusion through the laminar surface sublayer and is
a function of the condition of the surfaces which actually react with the
pollutant.  As this surface is largely plant tissue, this  process is  de-
pendent upon plant type and maturity, water stress, and other  plant physio-
logical factors.  The aerodynamic process may be much more readily  modeled
than the surface process, but a considerable effort in measuring the  sur-
face resistance to uptake of S0£~, S02, N03~, and other nitrogen species by
various surfaces will be needed in order to improve significantly the model
simulation of dry deposition.

     Wet deposition is a function of cloud type, precipitation type,  preci-
pitation rate, and the chemical  species being deposited.  The  precipitation
rate can be highly variable and localized (i.e., subgrid scale).  The ex-
isting network does not provide adequate spatial and temporal  resolution
for the precipitation rate and physical characterization of  the  precipita-
tion event.  This poses a severe limitation on the ability of  acid  deposi-
tion models to simulate wet removal of pollutants.

     There is considerable evidence suggesting that the in-cloud wet  re-
moval  of atmospheric pollutants is much more important than  below-cloud
removal.  Proper treatment of this process is absent in present  models in
which clouds are not simulated.  This involves subgrid parameterization of
cloud physics and chemistry and represents an important area for future
research.

     Very little is known about wet removal of_pollutants  by snow.   There
are evidences that snow scavenges N03~ and S0k= more efficiently than
rain.  Current models do not treat snow and rain differently.

1.8  Model development needs

     Progress in acid deposition model development stimulates  advances in
models of subprocesses and is in turn guided by new understandings  and data
from new experiments.  However, large models will always lag behind the
submodels in complexity and detail by virtue of the fundamental  limitations
on manpower and computer resources available for large models.   Existing
acid deposition models have evolved during the past decade under limited
but continuously improving knowledge about the complex processes control-

                                     32

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ling transport, transformation, and deposition.  By necessity,  they  are
highly parameterized and over-simplified.  Considerable improvements  in
modeling the basic transport and transformation processes are  now  possi-
ble.  Some of the key areas that need to be improved are listed below and
discussed in the next three chapters.

     •  Cloud modeling.  Clouds play important roles in transport, trans-
        formation, and deposition of pollutants.  Current models practi-
        cally ignore clouds.

     •  Multi-layered models.  Multi-layered models allow room for better
        representation of wind fields at various heights, exchange between
        the boundary layer and free troposphere, inclusion  of  the  nocturnal
        inversion layer, and treatment of dry and wet deposition and  emis-
        sions.

     •  Chemical transformations.  The inclusion of elementary gas-phase
        and aqueous-phase reactions and mechanisms of sulfur,  nitrogen,
        hydrocarbons, and ozone is essential to identify and understand the
        key rate-limiting processes in the chemical transformation.   The
        linearity (or nonlinearity) of the source-receptor  relationship is
        largely determined by these processes.

     •  Subgrid parameterizations.  Diffusion, clouds, emissions,  depo-
        sition, and inhomogeneities in chemical transformations all  need
        proper subgrid parameterizations.


2.  REGIONAL METEOROLOGICAL MODELS1

2.1  Introduction

     To understand the phenomenon of acid deposition, one must understand
the atmospheric processes of horizontal and vertical transport, turbulent
mixing, and cloud and precipitation formation, in addition  to  the  complex
chemistry involved in the formation of acidic material.  Because of  the
transport of gases and aerosols out of the boundary layer by clouds,  it is
necessary to consider the motion in the entire troposphere  to  determine the
transport of chemical species on regional scales.  From a scientific  point
of view, the processes of scale interactions, boundary layer and radiative
effects, and cloud and precipitation formation are among the more  exciting
areas of atmospheric research.  From an assessment point of view,  the cor-
rect modeling of horizontal and vertical transport, turbulent  mixing, wet
and dry removal, and the possible nonlinear interactions among these  pro-
cesses is essential in evaluating potential control strategies.

     Considerable progress has been made in developing regional-scale nu-
merical models of the meteorological processes that affect  acid deposi-
tion.  This section reviews this progress and discusses the prospects for
further improvement.
    Contributed by Richard Anthes.  A  slightly  revised  version  of  this
section has been accepted for publication  in Mon. Wea. Rev.

                                     33

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     Operational numerical weather prediction of  synoptic-scale  (charac-
teristic wavelengths greater than 2500 km) atmospheric  flows  began  in  the
United States in 1954 with a barotropic  (one-layer) model  (Fawcett,  1977;
Shuman, 1978).  Multilevel, baroclinic models were developed  gradually  in
the 1960s and 1970s.   With the operational implementation  of these  models
came a slow but steady improvement in the  skill of large-scale forecasts of
sea-level pressure and 500 mb heights and  winds.  This  improvement  could be
related mainly to higher resolution (vertical and horizontal), increases in
domain from hemispheric to global, and improvement in  initialization tech-
niques.

     In spite of the improvements in the skill of predicting  the  large-
scale wind and pressure patterns, improvements in predicting  precipitation,
which exhibits greater variability on scales much smaller  than the  synoptic
scale, have been very slow (CAS, 1980; Ramage, 1982).

     The long-realized fact that much significant weather,  in addition  to
precipitation, occurs on the mesoscale (Orlanski, 1975)  stimulated  consi-
derable research on limited-area, or regional numerical  modeling  when  com-
puters became large and fast enough to make such  high  resolution  feasible.
However, the extension of synoptic-scale models, with  typical  horizontal
grid sizes of 400 km, to regional models,  with grid sizes  from 50-100  km,
has not been straightforward.  The principal difficulties  are four-fold:
(1) numerical difficulties associated with lateral boundary conditions,
(2) limitations in the density of initial  data, particularly  upper-air
data, on the regional scale, (3) the increase in  importance of and  diffi-
culty in modeling diabatic, topographic, and surface effects,  and (4)  the
reduction in the inherent predictability of smaller-scale  atmospheric  cir-
culations.  The first two are solvable with existing technology,  requiring
only implementation of existing computer and advanced  observational  sys-
tems.  Considerable progress in developing improved models  of physical
effects of terrain, surface and boundary layer fluxes  of momentum,  heat,
and water vapor, latent heating associated with condensation  and  evapora-
tion, and radiative effects has also been  made in research  models.   Thus,
we may hypothesize that the only fundamental difficulty blocking  signifi-
cant improvements to regional-scale, or meso-a scale predictions  lies  in
the increasingly stochastic nature of smaller-scale phenomena, as discussed
by Tennekes (1978).  While the ultimate  limits to predictability  of  region-
al-scale weather are unknown, we believe there is evidence  that  significant
improvements in predictions of meso-a scale phenomena  could be made  imme-
diately.  These improvements could be obtained through  a combination of
better use of existing data, incorporation of recent research results  in
operational models, and implementation of  an improved  data  network.

     This section reviews recent operational and  research  regional-scale
numerical models and discusses their current limitations,  and the prospects
for improvement of predictions on this scale for  time  periods of  12-48 h.
To limit our scope, only models that have  been tested  on real  data  in
extra-tropical regions are reviewed, in  spite of  the fact  that models  of
similar scale are showing promise in the tropics  as well (Krishnamurti  et
al., 1979; Harrison and Fiorino, 1982; Fiorino et al.,  1982). The  models
discussed here are summarized in Table 2.1.
                                     34

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2.2  Quantitative measures of forecast skill and  realism  of  simulations

     Before reviewing the components of regional  models,  it  is  worthwhile
to review methods of judging the accuracy and skill  of models,  not only to
be able to compare the relative performance of  different  models,  but also
to evaluate the impact of future changes in the numerical, physical,  or
data aspects of the models.  Two nonexclusive types  of verifications  can be
identified, those that measure the skill of forecasts and those that  mea-
sure the degree to which the model forecast or  simulation realistically
simulates atmospheric behavior.  Examples of the  first more  conventional
type of verification are Si scores, RMS errors, and  threat scores,  which
will  be reviewed in this section.  In addition  to  these traditional  methods
of verification, evaluation of mesoscale and smaller-scale predictions  and
simulations using primitive equation models requires a second type of veri-
fication.  This is because the amplitude of features predicted  by the meso-
scale models often becomes larger while the scale  becomes smaller.   Thus,
minor displacement errors in time or space can  produce enormous errors  at
individual  points.  In spite of these large errors,  the prediction of fea-
tures of the correct amplitude and structure in approximately the right re-
gion may provide useful information.  Examples  include the prediction of
heavy convective rainfall somewhere in a watershed,  the prediction of a
major hurricane-making landfall in a zone along a  coast,  or  the prediction
of severe downs!ope winds along the front range of the Rocky Mountains
sometime during a given 24 h period.  An example  of  the second  type of  ver-
ification is the model's kinetic energy spectrum.  If, over  a large number
of cases, a model produced a spectrum similar to  that of  the atmosphere,  it
would be considered a realistic model in this respect.  Statistical  charac-
teristics of the model atmosphere such as the kinetic energy spectrum may
be viewed as the model's "climate."  A model could have a good  mesoscale
climate but poor average skill scores.

     This section discusses some objective verification techniques that can
be used to judge the skill of mesoscale forecasts  and the realism of meso-
scale simulations.  Because of the many degrees of freedom in mesoscale
models and the computational expense required to  run a large number of
forecasts,  it would be desirable to develop and utilize these measures  ear-
ly, so that investigators can compute a uniform set  of comparable measures
of skill in the evaluation of experimental forecasts.  The use  of the same
criteria will enable more effective model intercomparisons and  more mean-
ingful evaluation of the impact on the forecast of different data,  analy-
sis, and initialization techniques and physical parameter!zations.

     A summary of useful quantitative measures  of forecast skill  is pre-
sented in Table 2.2, together with estimates of the  current  capability  of
regional models, where available.

a.  Measures of forecast skill

Si scores

     Synoptic-scale models have been verified over the years by calculation
of objective indices, or scores that reflect the  skill in predicting the
mass (pressure or height) fields and the precipitation occurrence and

                                     40

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    Table 2.2.  Quantitative measures of evaluating regional model
                forecasts.  Typical  values refer to 24 h forecasts
                Measure
                         A. Skill of forecasts

                                        Typical  Values (1980-1982)
             Score
             Sea level pressure
             850 mb height
             700 mb height
             500 mb height
             300 mb height
                                                     45
                                                     40
                                                     30
                                                     25
                                                     20
Errors

Surface
850mb
700mb
500mb
300mb
Vector
Wind
(m s-1)
2.5
5
7
10
15



Height Temperature Specific Hum
(m) (°C) (g kg-1)
3 mb
30
35
40
45
4
4
3
3
4
?
?
?
?
?
Correlation coefficients, forecast vs. observed changes
             Surface pressure
             500 mb heights
             Temperature

          Threat Scores
             Precipitation (0.25 mm or more)
                           (2.5 cm or more)
                                                      0.75
                                                      0.75
                                                      0.35
                                                      0.20
Areas of indices or parameters related to thunderstorm occurrence

             Convective instability                   ?
             Lifted, K indices                        ?
             Wind Shear                               ?
Characteristics of Features
                                                    ±4 mb
             Minimum pressure of cyclones
             Maximum speed of jet streaks
             Error in position of features (e.g., cyclone center)?

Band-passed difference fields of conventional variables (temperature,
pressure, moisture, winds)

             Space-filtered
             Time-filtered
                                   41

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                        Table 2.2 (continued)
          Forecast of Occurrence or Nonoccurrence of an Event
Threat score
 (CSI)
Accuracy
                  E N1/(N1+N2+N3)

                  = (N1+Nlt)/(N1+N2+N3+Nlt)

Bias              = (N1+N2)/(N1+N3)

False Alarm Rate  = N2/(N1+N2)

No Hit Rate       = N3/(N1+N3)

Forecast
Event
Forecast
No Event
Event
Observed
NI
N3
Event Not
Observed
N2
Hk
Probability of
 detection
                  = N1/(N1+N3)

                        B. Realism of Forecasts
Correlation Matrix

The spatial correlation between observed and forecast gridded  scalar  fields
are calculated for various lags, or offsets, of the observed grid  relative to
the forecast grid.  The higher the maximum correlation and the  less the  lag
associated with the maximum, the better the forecast.

Structure Function

The structure function is a measure of the fraction of variance associated
with scales of motion smaller than a given value.  It ranges in value from
zero at zero distance to twice the temporal variance of a variable at large
distances.

Spectra

    Kinetic energy
    Temperature

Terms in Budget Equations

    Kinetic energy
    Vorticity
    Water vapor
    Temperature
                                   42

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amount.  The most common measure of  skill  in  forecasting  the  pressure or
height is the $! score (Jewel es and  Wobus,  1954), which measures  the skill
in predicting the horizontal gradient  of  a scalar field.   Because of the
strong geostrophic (or gradient) relationship  between  the pressure gradient
and large-scale flow in extratropical  regions,  the  S}  score  for  pressure is
also a good measure of skill in predicting the  synoptic scale wind field.
The Si score is defined as

                                   IM
where eg is the error of the  forecast  pressure  difference  and GL  is  the
maximum of either the observed  or  forecast  difference  between two points.
The summation is over all points in  the  verification  region.   The S1 score
is sensitive to the distance  between verification  points,  as  well  as the
scales of motion present in the forecast and  analysis.   A  valid comparison
of Si scores, therefore, requires  similar spacing  of  the verification
points and filtering of the model  forecasts and analysis in a consistant
way.  Twenty years of experience with  the Sj^  score of  sea-level pressure at
the National Meteorological Center (NMC)  has  shown the  practical  range be-
tween essentially perfect and worthless  forecasts  to  be 30-80 (Fawcett,
1977).  The $! scores for 30  h  forecasts of SLP  at NMC  have decreased
steadily from about 65 in 1955  to  52 in  the early  1970s (Fawcett,  1977).
Recent operational model Si scores for 24 h forecasts  of SLP  (Table  2.3,
Figure 2.1a,b) indicate representative values of 40-50.

     Most reports of research model  simulations have  not included Sr
scores.  Those that have are  not directly comparable with  the operational
scores because they have been done for a small  number  of cases under re-
search rather than operational  conditions and probably  have a somewhat dif-
ferent spacing of verification  data  and  scales  of  motion in the forecast.
With these limitations, there is some  evidence  that further improvements
can be made.  For example, Anthes  and  Keyser  (1979) found  an  average 24 h
$! score for 32 cases of 39.1 which  compared  favorably  to  an  average of
45.9 for the Navy's operational model  and 73.4  for persistence.   Koch
(1982, personal communication)  indicates a  significant  improvement over the
LFM in thirty 24 h predictions  using a high-resolution  research model.

Categorical forecast scores

     A categorical forecast is  a yes or  no  forecast of  an  event,  such as
occurrence of a precipitation amount (usually 0.25 mm  or more), at a given
point during a specified time period.  A measure of success of categorical
forecasts is the percentage of  correct forecasts.   Records show annual  ave-
rages of correct forecasts of precipitation occurrence  over the contiguous
United States of 81-86%, with little evidence of improvement  over the per-
iod 1966-1977 (Ramage, 1982).

     Since 1965, the National Weather  Service has  issued probability fore-
casts of 0.25 mm or more of precipitation.  The reliability of these fore-
casts over the entire United  States  has  been  remarkably good  (Figure 2.2),
suggesting the value of these forecasts  to  those activities affected by

                                     43

-------
    Table 2.3.  SL score for 24 h forecasts of sea-level pressure


            Model                             Si Score

    Australian Numerical Meteorology
    Research Center, 1978, 1979 average
    (Leslie et al., 1981)                        46.5

    NMC Limited-area Fine-mesh Model
    (LFM) (Feb-Sept 1976)

           East of Denver                        44.8      (48.0)*
           West of Denver                        50.7      (51.7)*

    LFM (computed from 49 point 1976             45
    latitude-longitude grid     1977             45
    centered over U.S.)         1978             42
    (Newell and Deaven, 1981)   1979             42
*Denotes Si scores for hemispheric model.

                                   44

-------

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 52

 51

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£48
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 45

 44

 43

 42
                         MSL  SI   SKILL  SCORES
    70
72
74
76       78

   YEflR
80
82
84
         Figure 2.1b   Mean monthly S]  scores for 24 h forecasts
         of sea level pressure obtained from the Australian  Numerical
         Meteorological Research Centre model (Gaunt!ett,  1982, per-
         sonal communication).
                                   46

-------
    100
o
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O
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                  ' 7,651
                      II  	I     I     I     I     I     I
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                                    60
80
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                     FORECAST PROBABILITY (%)
        Figure 2.2   Reliability of the local  probability of
       (measurable)  precipitation forecasts  issued for 87
       stations  within  the conterminus United States.  The
       sample includes  forecasts issued once  daily for three
       projections over the period March, 1978 to March, 1979.
       The forecast probabilities were assigned the values of
       0, 5, 10, 20, 30,  ..., 90, 100 percent.   Numbers next
       to the plotted points give sample sizes  (CAS, 1980).
                               47

-------
precipitation.

Threat scores

     In contrast to the prediction of occurrence  vs.  nonoccurrence of mea-
surable precipitation, the threat score measures  the  skill  in  predicting
the area of precipitation amounts over any  given  threshold  (Figure 2.3).
The threat score TS is defined by
                        TS  =
                                   CFA
                              (FA + OA - CFA)
(4a)
where CFA is the correctly forecast area bounded  by  a  given  precipitation
amount, FA is the forecast area, and OA is  the  observed  area.   A second
form of the threat score, which is easily calculated from  numerical  models,
is
                           TS =
                                F + R  - C
(4b)
where C is the number of stations  {or  grid  points)  correctly  forecast to
receive a threshold amount of precipitation, F  is the  number  of  stations
forecast, and R is the number of stations observing the  amount.   This form
of the threat score is the same as the Critical  Success  Index (CSI)  discus-
sed by Donaldson et al. (1975).

     Subjectively prepared threat  scores at NMC  of  precipitation in  excess
of 2.5 cm in the period 0-24 h have  shown an annual  average of around 0.20
over the United States since 1960, with no  apparent trend  (CAS,  1980).
Threat scores produced by NMC's operational regional model  (the  Limited
area Fine-mesh Model, or LFM) for  0.25 mm of precipitation  in the 12-24 h
forecast period are considerably higher (averaging  around 0.40)  and  have
shown a slight increase since 1976 (Figure  2.4).  Figure 2.4  also demon-
strates an annual variation of skill, with  significantly lower skill  in the
summer.

     In addition to precipitation  forecasts, threat scores  can be usefully
applied to other parameters of significance to  small-scale  weather pheno-
mena.  Examples are measures of stability that  are  statistically related to
thunderstorms, such as areas of convective  instability or threshold  values
of various indices (e.g., lifted index, K-index).   Reap  and Foster (1979)
discuss results of a statistical technique  based on numerical  model  output
parameters to forecast the probability of thunderstorms.

Bias scores

     The bias score measures 'the tendency of a  model to  forecast too small
or too large arv area of a given amount of precipitation. In  terms of an
area of precipitation, it is defined as
                                B  =
                                    FA
(5a)
                                      48

-------
Correctly forecast area (CFA)
                                        Observed area (OA)
   Forecast area (FA)
    Figure 2.3   Schematic  illustration of the threat
    score (TS) as used in quantitative precipitation
    forecast verification.  The threat score is defined
    by TS = CFA/(FA + OA -  CFA), where the areas refer
    to regions on a map bounded by a particular isopleth
    (CAS, 1980).
                            49

-------
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                                            50

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while in terms of points  (stations) it  is


                                B =£ .                                 (5b)

As shown in Figure 2.4, there was little bias  in  the  LFM  model  until  about
1981, when a rather strong positive bias (B  «  1.4)  developed.   According  to
Hovermale (1982, personal communication),  this  bias occurred when  an  un-
real istically dry boundary layer moisture  analysis  was  replaced by a  more
realistic (and more moist) analysis.  Because  the convective precipitation
parameterization, which had been tuned  to  yield little  bias with the  dry
analysis, was not altered, an excessive number  of points  received  the
threshold amount of precipitation and a positive  bias developed.

Probability ellipses

     If the stochastic component of mesoscale  predictions is known for  var-
ious phenomena, probabilistic forecasts can  be  developed  which  give users a
quantitative measure of uncertainty associated  with deterministic  fore-
casts.  An example is the set of probability ellipses associated with hur-
ricane track prediction (Neumann and Hope, 1972); in  addition  to forecast-
ing the most probable location  of a hurricane  24, 48, and 72 h  in  advance,
the probability that the  center will fall  within  ellipses of different
sizes is also given.  Similar probability  forecasts could be generated  for
many mesoscale phenomena  over land.  At present,  probability forecasts  for
the occurrence of precipitation, for frozen  precipitation,  and  for thunder-
storms are issued by the  National Weather  Service.  The severe  weather
"boxes" issued by the National  Severe Storms Forecast Center outlining
probable areas of severe  thunderstorms  represent  crude  probability fore-
casts.

RMS errors

     In addition to the Si, threat, and bias scores,  a  common  measure of
accuracy is the RMS error.  Table 2.4 gives  two examples  of RMS wind,
height, and temperature errors  in a 24  h forecast on  a  99 km mesh  (Phil-
lips, 1978).  It shows typical  RMS vector  wind  errors of  5-10  m s   ,  height
errors of 25-75 m, and temperature errors  of 1.5-4.5°C.

Correlation coefficients

     Correlations between forecast and  observed changes are useful measures
of prediction skill, but  they have not  been  reported  extensively for  either
operational or research models.  An exception  is  the  regional  model of  the
Japan Meteorological Agency.  Nitta et  al. (1979) report  monthly averages
of correlation coefficients for 24 h changes of 500 mb  heights  and surface
pressure ranging from about 0.65 in summer to  over  0.8  in winter (Figure
2.5).

Characteristics of phenomena

     Characteristics of significant phenomena,  such as  the minimum pressure
of cyclones, maximum wind speed, or temperature and moisture gradients, can

                                     51

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Table 2.4.  RMS errors for two experimental 24 h forecasts
            on a 99 km grid of nested grid model (Phillips,  1978)


                 RMS Vector Wind Errors (m s'1)

         p(mb)       1200 GMT 9 Jan 1975  0000 GMT 19 Nov 1975

          850                  7.6               5.4
          500                  6.8               6.8
          300                 15.5              10.0
          200                 13.0               9.5


                     RMS Height Errors (m)

         p(mb)      1200 GMT 9 Jan 1975   OOOOGMT 19 Nov  1975

          850                 41.7              17.8
          500                 44.3              24.7
          300                 66.4              34.8
          200                 78.6              43.3


                  RMS Temperature Errors  (°C)

         p(mb)         1200 GMT 9 Jan 1975

          850                  4.2               4.5
          500                  1.8               1.5
          300                  3.1               2.6
          200                  4.6               1.7
                               52

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be tabulated over a number of forecasts and plotted against  the  correspond-
ing observed values.  Errors in the position of features, such as  cyclones,
are also of interest.  This statistic is routinely reported  for  tropical
cyclone forecasts.  Hollingsworth et al. (1980) report a threat  score  mea-
suring the skill in forecasting cyclone positions.

Prediction matrix of occurrence vs. nonoccurrence of events

     It is often important to predict the occurrence or nonoccurrence  of  an
event such as thunderstorms, cyclogenesis, development of a  mesoscale  con-
vective complex, or occurrence of an area of precipitation greater than a
specified amount.  Within preset limits, the exact location  and  amplitude
are not necessarily considered.  Scoring can be done over a  number of  cases
according to a prediction matrix of number of forecasts of the event's oc-
currence or nonoccurrence vs. the observed events (Table 2.2A).  From  this
table, a threat score, accuracy, false alarm rate, bias, probability of de-
tection, and misses can be calculated.

Scale separation of errors

     Most methods of evaluating the skill in numerical models calculate
errors associated with the total predicted field.  As discussed  by Bettge
and Baumhefner (1980), separation of the total error into the errors asso-
ciated with different scales in the forecast is often useful in  identifying
sources of model error.  Bettge and Baumhefner (1980) present a  method to
separate various scales in a limited-area domain.  The method consists of
applying a digital band-pass filter to the fields.  The errors associated
with different scales can be computed by comparing the band-passed fields
to the analyses, which are filtered in the same way.  In addition  to consi-
dering band-passed difference fields of conventional variables,  the error
variance of each band can be computed and normalized by the  climatological
observed variance associated with those scales.

Summary of operational skill scores

     Objective measures of the skill of operational numerical models indi-
cate a slow but steady increase in the short-range (0-24 h)  prediction of
sea-level pressure, although substantial room for improvement still ex-
ists.  The same is true of 500 mb heights (Shuman, 1978).  An increase in
the skill of predicting precipitation has been more difficult to show. The
percentage of correct categorical (yes-no) forecasts of measurable precipi-
tation over a 12-h period has remained around 85% in the past decade,  show-
ing only very slight improvement.  However, the threat score of  12-24  h
precipitation forecasts by the LFM have shown slow but steady improvement
since 1976.  Forecasts of the probability of precipitation in a  specified
12-h period are highly reliable, e.g., when forecasts of 50% probability  of
measurable precipitation are made, precipitation occurs 50%  of the time.
All measures of forecast skill show greater skill in winter  than in summer,
which reflects the smaller-scale nature of significant weather systems in
the summer.
                                     54

-------
b.  Statistical measures of realism of  simulations

     Because of the increasingly  random component of  mesoscale  predictions
as the spatial scale decreases, skill scores may indicate  a  poor  forecast
and yet the forecast model may be quite realistic for understanding the
evolution of a phenomenon and may even  have practical  utility.  An  extreme,
hypothetical example illustrates  this paradox.  Suppose  a  small-scale model
were developed that predicted the structure, intensity,  and  track  of ty-
phoons perfectly, except for small position errors  resulting from  errors in
the speed of the storm.  Figure 2.6 shows  hypothetical forecast and ob-
served sea-level pressure patterns, with the predicted storm lagging behind
the observed storm (assumed to be moving toward the northeast)  by  100 km.
The pressure pattern was computed from  the empirical  formula (Holland,
1980)

                     P  ~ P             R
                pn = -^	 = exp(-Ar"b)  0 <  r < 10RQ ,                 (6)

                     pe " po

where ps is the sea-level pressure, p0  is  the  pressure at  the center of
the storm, pe is the pressure in  the environment beyond  R0,  R0  is  the
radius of maximum wind speed, and A and B  are  constants.   In this  example,
Po is 900 mb, pe is 1015 mb, R0 is 40 km,  A is 253  km1-5 and B  is
X • 0 •

     For a two-day forecast in which the observed storm  is assumed to have
moved at a constant speed of 30 km h"1, the error shown  in Figure  2.6 re-
presents an error in the model storm speed of  2.1 km  h"1 or  a time lag of
3.6 h.  Although most people would agree that  the above  forecast would have
great utility and represents significant skill, many  conventional  measures
of skill would indicate a worthless forecast.  Figure 2.7  shows the rapid
increase of error associated with the Si score, RMS error  of pressure and
vector wind speed, and threat score for increasing  position  errors.  In the
example above, the Si score of SLP is 93 and the RMS  pressure and  wind er-
rors are 9 mb and 12.5 m s'1, respectively.

Correlation matrix

     As the previous example demonstrates, a regional  model  might  forecast
the correct intensity and shape of a field but displace  the  field  by some
small distance.  A correlation matrix scoring  method  (Tarbell  et  al., 1981)
is a measure of skill in predicting the pattern of  a  scalar  field  such as
rainfall.  An observed analysis is computed on the  model grid and  spatial
correlations between observed and predicted variables are  computed for var-
ious north-south and east-west lags, or offsets of  the observed and fore-
cast grids.  Grid points in data-void regions  are not included. The result
is a matrix that contains information about the skill  of the model  in pre-
dicting patterns.  A matrix containing  a few large  positive  correlation co-
efficients and a large number of  small  or  negative  correlation  indicates
considerable variance in the predicted  and observed fields and  that the
model is predicting the observed  structure, though  not necessarily  in the
correct location.  In the above example of the tropical  storm forecast, the
proper shift would yield a maximum correlation of 1.0, indicating  a perfect

                                     55

-------
      I   I   I    I   I
I   I   I
1   I   I   I
                            I   1  J   I   I
                         I   I   I
 Figure 2.6  Hypothetical forecast and observed sea level pressure
(mb, contour interval  15 mb) associated with a tropical cyclone.
The hypothetical model is assumed perfect except for a slow bias in
speed.  The distance between the observed and forecast storms is
100 km and the minimum pressure is 900 mb.  The distance between
tick marks is 50 km.
                              56

-------
   K
   §
   CC
   u
   i
   *
   £
   tn
   K
120

110

IOO

90

80

70

SO

SO

40

30

20

 10

 0




24

22

20

 18

 16

 14

 12

 IO

 8

 6

 4

 2
         (a)
        (c)
           100  200  3OO 400  500  600 700

               POSITION ERROR (km)
                             RMS Wind *
                                      I
                                      Q.
                                      01
                                      cc
                                          (b)
                                                                i
                                                                    i
100 200 300  400  500 600  700

    POSITION ERROR (km)
           100  200 300 400  900  600 700

               POSITION ERROR (km)
                                    0 0.1 02  03  0.4 0.5 C.6 Q7 02 0.9 1.0
Figure  2.7   Measures of forecast skill  as a function of  position error
of hypothetical  tropical cyclone model  described  in text,   (a) S] score
of sea  level pressure,  (b)  root mean  square error of sea  level pressure,
(c) root mean square error of vector wind error,   (d) threat score of
rainfall of given  amount as  a function of  a,  the ratio of position  error
to the  diameter  of the rainfall area.
                                   57

-------
prediction of pattern.  In contrast,  a  smooth  forecast  with  little struc-
ture will show a smaller maximum positive correlation and  less  variation
for a given lag.  Figure 2.8 compares two experimental  rainfall  forecasts,
verifying at 1200 GMT 25 January 1978.  The  forecast with  more  structure
(middle panel) has a maximum correlation coefficient of 0.87  when  the anal-
ysis grid is displaced four grid points to the  east and five  grid  points to
the north (Table 2.5).

Structure function

     The structure of a regional model  forecast or simulation can  be com-
pared quantitatively with that of the atmosphere by the structure  function
(Gandin, 1963), defined as
                                     m(r2,r2)  -
(7)
Here the m are correlation functions for the  deviations  of  the  meteorologi-
cal variables from their time mean values  and the  r.  are  position  vectors of
the observation pairs 1 and 2.  Thus, m(ri,r,i)  is  an autocorrelation func-
tion (the variance at station 1), while m(r,i,r.2) is  the  covariance.   We
note from (7) that, as the station separation approaches zero,  b  approaches
zero (for perfect observations).  If the covariance  vanishes  at infinite
station separation, b approaches twice the  station variance.  Thus,  the ra-
tio of the structure function to twice the  mean  station  variance  is  a mea-
sure of the fraction of variance associated with scales  smaller than the
station spacing.  When applied to observational  data sets,  as done by
Barnes and Lilly (1975), all pairs of observations are considered and the
correlation and structure functions are often grouped and displayed  as a
function of distance separation.  Figure 2.9a,b  shows examples  of the cor-
relation and structure function for thunderstorm conditions in  Oklahoma
(Barnes and Lilly, 1975).  A comparison of  the  results for  temperature and
mixing ratio indicates that there is much  more  variance  associated with
small scales for moisture.  Thus, only 22%  of the  total  variance  of  tem-
perature occurs at scales less than 200 km, while  for moisture, 68%  of the
variance is associated with these scales.   Similar calculations on model
data would indicate whether the model simulates  scales of motion  similar to
those in the atmosphere.

Spectra

     Another measure of the fidelity with  which  a  model  reproduces or simu-
lates the atmosphere is the spectrum of various  quantities  such as kinetic
energy, temperature, water vapor or vertical  velocities.

2.3  Components of regional models

     Three major components of regional numerical  weather prediction models
can be identified.  Numerical aspects include the  accuracy  of the numerical
approximations to the analytic differential equations.   Physical  aspects
include the modeling or parameterization of important energy  sources or
sinks, such as radiation, condensation and evaporation,  and frictional dis-
sipation.  Finally, a model perfect in the first two aspects  would be use-
                                      58

-------
         Figure  2.8  24-hour precipi-
         tation  (cm) over the period
         1200 GMT 25 January, 1978.
         (Top) Observed.
         (Middle) Forecast with latent
         heat included.
         (Lower) Forecast with latent
         heat neglected.
         (From one of 32 cases of ex-
         perimental forecasts summar-
         ized by Anthes and Keyser,
         1979.)
59

-------
Table 2.5.  Correlation matrix of observed and forecast  precipitation
            amounts.  Values are spatial correlation coefficients,  in
            hundredths, for various north-south and east-west  offsets  of
            the observed and forecast grids.  The central value  of  each
            matrix represents no shift.  The observed  rainfall  in this
            example is shown in the top panel of Figure  2.8.   Matrix A
            corresponds to the forecast shown in the middle  panel of
            Figure 2.8, while matrix B corresponds to  the forecast
            shown in the lower panel of Figure 2.8.
A










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80
79
78
77
76
75
73
84
83
82
80
79
78
76
75
74
72
70
83
82
81
79
77
75
74
72
70
68
66
82
80
79
76
74
72
70
67
65
64
61
79
77
75
72
70
67
65
63
60
58
55
75
73
71
68
65
62
60
57
55
52
49
70
68
66
63
60
57
54
51
48
46
42
64
62
59
57
54
51
48
45
42
39
35
                                     60

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1.0


 .8


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 16


 14


 12


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 6
            a
       K  W°°
        o   **o 8
       o oo     ,
              a
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20   40
60   80
100   120
  (KM)
140   160  180  200   220
                                      °0
                               o    o
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                   o°   o
           O O   o o O

        CO %   °     *    °
          o0?  .
         8 o
                                            I	,
  0    20   40   60   80   100   120   140   160  180  200   220
                             (KM)

     Figure 2.9a   Correlation  function (top) and  structure
     function  (bottom)  for temperature under stormy conditions
     in Oklahoma.   Units  of structure function for temperature
     are K? (Barnes  and Lilly, 1975).
                             61

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1.0




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 10




 9




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20   40   60    80   100   120   140   160   180  200  220

                      (KM)
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                            (KM)



     Figure 2.9b   Correlation function  (top)  and  structure

     function (bottom) for mixing  ratio  under  stormy conditions

     in Oklahoma.  Units  of structure  function for mixing ratio

     are g2kg-2 (Barnes and Lilly, 1975).
                           62

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less for operational prediction without  initial  data and a method of anal-
ysis and initialization.  Table 2.1  summarizes  these aspects  of some opera-
tional and research  regional  models.  This  section  reviews these components
and tries to identify those which  are currently  the most important in de-
termining the accuracy  of operational models.   Rather than provide detailed
reviews of the components themselves, which  is  unnecessary because indivi-
dual reviews exist elsewhere, we concentrate on  the impact of these compo-
nents on regional forecasts and simulations. Because systematic tests on a
large number of cases in which all  components are  varied have not been
made, some of the conclusions are  subjective and based on only a few case
studies.

a.  Numerical aspects

     Numerical components of  regional-scale  models  include the choice of
vertical and horizontal grids, the approximations  to the temporal  and spa-
tial derivatives in  the partial differential equations governing the flow,
and the formulation  of  the lateral  boundary  conditions.  There are many
variations of these  components which  have  been  studied extensively.  Ex-
cellent summaries and reviews appear  in  the  literature (Table 2.6), and
there is no need to  provide further detailed reviews here.  Instead, we
discuss the most significant  issues  involved in  the choice of a particular
grid structure, numerical method,  and lateral boundary formulation.

Grid structure

     Horizontal grids may have each variable (three velocity  components--
pressure, temperature,  and moisture)  defined at  every grid point (nonstag-
gered grid), or may  have individual  variables defined on separate grids
that are offset from each other (staggered  grids).   As indicated in Table
2,1, both nonstaggered  and staggered  grids  have  been used successfully in
regional models.  There is evidence,  however, that  staggered  grids provide
more accurate solutions for a given number  of grid  points because many of
the spatial derivatives can be evaluated over horizontal  distances only
half as great as those  associated  with  nonstaggered grids. Arakawa and
Lamb (1977) discuss  theoretical reasons  for  the  increased accuracy asso-
ciated with staggered grids.  The  superiority of a  staggered  grid over an
unstaggered grid was shown in the  three-dimensional  simulation of tropical
cyclones by Anthes et al. (1971) and  Anthes  (1972).  Increased accuracy can
also be obtained by  staggering variables in  the  vertical, and most limit-
ed-area models use stagggered vertical  grids.   The  only disadvantage asso-
ciated with staggered grids is their  requirement for shorter  time steps (a
consequence of the higher horizontal  resolution).

Numerical methods

     A large number  of  numerical approximations  to  the partial differential
equations exist.  As discussed by  Pielke (1981), the methods  may be clas-
sified as finite-difference schemes,  spectral/pseudo spectral methods,
finite-element schemes, and interpolation  schemes.   However,  with the
exception of the spectral methods,  all  methods  produce a set  of finite-
difference equations, the main differences  being the accuracy of the ap-
proximations, the conservation properties,  and  the  computational cost and

                                      63

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       Table 2.6.  Reviews and discussions of numerical aspects
                   of limited-area meteorological models
General
    Eliassen (1980)
    Pielke (1981)
    WMO (1979)
Horizontal and Vertical grid Structures
    Arakawa and Lamb (1977)
    Grotjahn (1977)
Approximations to Nonlinear Partial Differential Equations
    Finite-Difference Schemes
         Haltiner and Williams (1980)
         Richtmyer and Morton (1967)
         Kreiss and Oliger (1973)
         Mesinger and Arakawa (1976)
    Spectral/Pseudo-Spectral Schemes
         Orszag (1971)
         Gottlieb and Orszag (1977)
    Finite-Element Methods
         Strang and Fix (1973)
         Cullen (1976)
Lateral Boundary Conditions
    Moretti (1969)
    Shapiro (1970)
    Oliger and Sundstrom (1978)
    Sundstrom and Elvius (1979)
                                   64

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complexity.

     Because of their simplicity and well-tested  behavior  under a variety
of meteorological conditions, finite differences  are  used  in  the great ma-
jority of regional models.  Most of these methods  involve  simple centered
differences and are accurate to the second order  (the errors  in the  finite
differences are proportional to the second power  of the  grid  length  or time
step).  However, several research models  utilize  higher-order finite-dif-
ference approximations to some of the  derivatives  in  the complete set of
equations.  In a global model, Williamson (1978)  found an  improvement in
the phase speed of shorter waves when  a second-order  scheme was replaced by
a fourth-order scheme.  Campana (1979) showed  that a  fourth-order version
of a coarse-mesh (381 km) model gave nearly  as  accurate  forecasts in the
0-48 h range as did a second-order, finer-mesh  (190.5 km)  version of the
model.  These results were confirmed by Leslie  et  al. (1981), who compared
six 24 h forecasts differing in order  of  the advection terms  and in  grid
size.  They found an improvement in mean  SLP $! score from 47.7 to 45.0
when the second-order advection terms  were replaced by fourth-order  approx-
imations.  This improvement, which required  only  a slight  increase in com-
putational time, was almost as great as that associated  with  halving the
grid length, which required an eight-fold increase in computational  time.

     Considerable effort has gone into the design  of  finite-difference
schemes that conserve (in an adiabatic, inviscid model)  integral  quantities
such as mass, total water, total energy,  and potential enstrophy (Arakawa
and Lamb, 1977, 1981).  Except for the conservation of first-order quanti-
ties (e.g., mass and water), the general  consensus is that, for regional
short-range prediction models, local accuracy  is more important than global
conservation properties (Benwell et al.,  1971).  However,  detailed compar-
isons designed to assess the value of  conservative schemes have not  been
made with regional forecast models.  It is possible that schemes which
conserve potential enstrophy would provide improved forecasts in regional
models over high terrain, although Nakamura  (1978) found truncation  errors
over steep mountains to be considerably smaller than  expected.

     The temporal integration schemes  may be classified  as explicit, in
which the temporal rate of change of all  variables depends only on present
or past values of the variable, or implicit, in which the  tendencies depend
on future variables as well.  Solution of the  implicit schemes  is possible
through relaxation or matrix inversion techniques.  While  the explicit
schemes are simpler to implement, the  implicit  schemes are more efficient
because they may be stably integrated  with substantially longer (2-8 times
longer) time steps.  Robert et al. (1972), Gaunt!ett  et  al.  (1976),  and Mc-
Gregor et al. (1978) have successfully used  implicit  schemes  in baroclinic
models.

     Compared to the forecast errors introduced by spatial truncation er-
rors, the error caused by temporal truncation  errors  is  probably insignifi-
cant.  This is because meteorologically significant features  have important
variations on scales as small as two to four times the horizontal  grid
length where truncation errors are large. However, these  features have
periods greater than an hour or more,  which  is many times  that of the time
steps used in regional models (Table 2.1).   While  temporal truncation er-

                                  -   65

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rors adversely affect high-frequency gravity waves  (Janjic and Wiin-Niel-
sen, 1977; Collins, 1980), the overall effect on the forecast is  probably
minimal, as evidenced by the success of implicit models which use time
steps several times longer than similar explicit models (Seaman and Anthes,
1981).

     Most regional models require a method to prevent energy from accumu-
lating in the shortest resolvable wavelengths and high temporal frequen-
cies.  While some finite-difference schemes minimize this problem by  their
inherent damping properties (such as the Euler-backward time integration
scheme which heavily damps high-frequency waves), most models utilize-ex-
plicit methods to control these unwanted features.  For controlling high
temporal frequencies, a widely used method is a time filter  (Asselin,
1972).  To control the short wavelengths, horizontal diffusion terms  are
used most often.  These terms may be proportional to v»Kv or v2Kv2 of the
quantity where K is an eddy diffusivity which may be constant or  depend on
some property of the flow, such as deformation.  The latter  has the desir-
able property of being considerably more scale-selective, providing more
damping of the shortest waves and less damping of the intermediate waves
(Williamson, 1978).

Lateral boundary conditions

     Lateral boundary conditions are undoubtedly a  major source of error  in
regional models.  Conditions are required which allow internally  generated
waves of all frequencies to pass out of the domain, while allowing meteoro-
logically significant information to propagate into the domain.   While  no
completely acceptable method has been demonstrated  (because  of the ill-
posed mathematical nature of the problem), a number of reasonably success-
ful schemes have been tested and used in regional models.  One popular
method, often called the sponge method, involves utilizing an increased
horizontal eddy viscosity in a band around the lateral boundaries (Perkey
and Kreitzberg, 1976).  This zone of high-viscosity damps waves propagating
out of the interior before they can reflect off the boundary.  A  diffusion
term may be added to the prognostic equations in this zone to allow large-
scale information obtained from a synoptic-scale model to propagate into
the domain.  The movable fine-mesh model of NIC (Hovermale and Livezey,
1977) follows this approach.  In two experiments with a coarse-mesh lim-
ited-area model, Baumhefner and Perkey (1982) found that the errors asso-
ciated with the Perkey-Kreitzberg boundary conditions were considerably
less (- 20%) than the total forecast error in the 0-48 h time period.

     A second method involves the use of approximate radiative boundary
conditions which minimize the reflection of waves (Orlanski, 1976) even
without a sponge zone.  Recent results with a limited-area model  indicate
that a version of radiative boundary conditions, in which vorticity and
divergence are extrapolated outward at the boundary rather than the velo-
city components themselves, is successful in minimizing distortion at the
boundaries.  Miyakoda and Rosati (1977) have found  the radiation  boundary
conditions to be superior to the sponge technique.

     A third, and perhaps the most satisfactory, solution to the  lateral
boundary problem in limited-area models is to nest  the regional model  in  a

                                     66

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larger-scale model.  Considerable success with  two-way  interacting  nested
grids has been demonstrated by Jones (1977) and Phillips  (1978).  Discus-
sion and reviews of nested grid techniques  are  provided by  Phillips and
Shukla (1973) and Elsberry (1978).  An example  of  the effect  of  lateral
boundary conditions on 24 h forecasts of a  regional  model  and the validity
of the nested grid concept is provided by Leslie et  al. (1981).  Figure
2.10 shows the average 24 h Si scores from  six  experimental forecasts.   In
the nonnested forecasts, the variables at inflow points are assumed to be
in steady state.  In the nested grid forecasts, time-dependent values are
obtained from a hemispheric model.  The use of  time-dependent boundary
conditions results in a significantly reduced Sj score  at all  levels.-

     In summary, most regional-scale numerical  models utilize finite-dif-
ference schemes with second-order accuracy.  It is probable that the larg-
est errors associated with the numerical aspects of  the model  arise from
the lateral boundary conditions and spatial truncation  errors.  These can
be minimized at a computationally reasonable .cost  by the  adoption of stag-
gered horizontal grids, higher-order difference schemes,  and  two-way inter-
acting nested grids.  Implicit temporal integration  schemes can  reduce the
computation cost by a factor of two or more with little reduction in accur-
acy, because temporal truncation errors do  not  appear to  be an important
part of the total forecast error.

Data analysis and initialization

     Two important components of regional models are the  analysis and ini-
tialization steps.  In the analysis phase,  grid point values  of  the model's
variables are estimated from diverse types  of surface and upper-air data at
irregularly spaced locations.  A widely used analysis scheme  in  regional
models is the method of successive corrections, in which  a  first-guess
field is modified by a series of scans which use observations to modify  the
first-guess errors.  Cressman (1959) introduced this method;  others have
suggested refinements and variations (Barnes, 1964).

     Optimum interpolation (0/1) is an analysis method, introduced  by Gan-
din (1963), designed to select a set of weighting  coefficients which mini-
mize the RMS error of the analysis over a large ensemble  of synoptic situa-
tions.  The weights depend on the spatial covariances among the  difference
(first-guess minus observation) fields.  Various 0/1 schemes  have been
tested by Bleck (1975), Schlatter (1975), and Bergman (1979),  whose method
is currently used by NMC.

     Otto-Bliesner et al. (1977) compared four  analysis schemes  (a  Cressman
analysis scheme, a global multivariate 0/1  scheme, an isentropic (constant
potential temperature, e) 0/1 scheme, and a subjective  analysis).   Although
differences were relatively minor, there was some  evidence  that  the 0/1
schemes did not resolve the amplitude of some of the features.  McPherson
et al. (1979) found that an 0/1 method resulted in a better resolution of
the wind field in one case study than did a global spectral analysis
scheme.  In addition, the 0/1 scheme produced a considerably  superior anal-
ysis of humidity.  Reimer (1980) used a univariate 0/1  method on isentropic
coordinates to test the impact of grid resolution  on the  analysis.   Over a
data-rich region (central Europe), he found a significant improvement by

                                     67

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  70-
 60-
2
o
o
CO

to
 4O
 3O
                                     Si Verification
                                     24 Hour Forecasts
                                Non-nested
                  Nested
   MSL  900    800    700    600    500    400300    200
                           Height  (mb)
  70-
 60H
CO
 4O-
 30-
                                     Si Verification
                                     36 Hour Forecasts
                                  Non-nested
                         Nested
   MSL  900    800    700    600   500    400    300    200
                           Height  (mb)


   Figure  2.10    Mean  24-hour Si scores  as  a function  of
   height  for nested grid and nonnested  forecasts   (Leslie
   et  al., 1981).
                            63

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utilizing a fine grid for the analysis  (see  Figure  1.8  in  Chapter  IV,  p.
110).

     The above comparisons of analysis  methods  considered  only  a  limited
number of cases and did not  test the  impact  of  the  different analyses  on  a
subsequent forecast.  The performance of  the ANMRC  model,  however,  indi-
cates that an improved analysis scheme  can make a significant positive
impact on the forecast.  A decrease in  SLP $! score at  24  h  of  about two
points was noted when a variational analysis scheme (Seaman  et al., 1977)
was introduced.

     Because of the limited  number of comparisons,  it  is difficult to  reach
firm conclusions regarding the superiority of one type  of  analysis scheme
compared to another.  However, there  is some evidence  that local  analysis
methods are better than spectral methods.  There is less evidence  of the
forecast benefits to be gained by utilizing  the computationally more expen-
sive 0/1 methods over the simpler Cressman-type schemes.   There is some
evidence that analysis on isentropic  surfaces is preferable  to analysis on
other surfaces, because the  horizontal  scale of variation  of the  wind  is
larger on 9 surfaces, especially in frontal  zones.

     Most objective analyses result in  mass  and wind fields  that  are unbal-
anced, i.e., the temporal tendencies  are  much greater  (an  order of magni-
tude or more) than the correct values.  The  result  is  the  generation of
inertia-gravity waves.  Although in most  cases  these waves do not  interact
greatly with the meteorologically significant waves, they  are a nuisance  in
that they contaminate output fields of  interest, such  as sea-level  pressure
and vertical velocity.  It is therefore desirable to adjust  the variables
to obtain a balanced state at the start of the  forecast, a process known  as
initialization (Kasahara, 1982).  Leith (1980)  has  discussed the  balanced
state in terms of the concept of a slow manifold.   When on the slow mani-
fold, the divergence and vorticity are  consistent with  a slowly evolving, .
meteorologically significant forecast.  The  initialization phase  of a  model
forecast is designed to modify the objective analysis  to obtain initial
values that correspond to a  solution  on the  slow manifold.

     Two methods have shown  great promise for obtaining balanced  initial
conditions.  When periodic domains are  considered (global  or hemispheric),
the initial analysis can be  projected on  the model's eigenfunctions or nor-
mal modes, and the unwanted, fast modes eliminated  by  setting their ampli-
tude to zero (Baer and Tribbia, 1977).  Phillips (1981) shows how  varia-
tional analyses combined with a nonlinear normal mode  initialization can
improve the initial analysis in a more  significant  way  than  the elimination
of noise.  Reviews of this normal mode  method are provided by Daley (1981)
and Kasahara (1982).  The scheme is not well-suited to  limited-area models
which involve nonperiodic domains. However,  it  may  be  applied in  regional
models by initializing on a  global domain and interpolating  the global
fields to the fine-mesh, limited-area model.

     A related scheme, which is more  suitable for direct initialization of
regional models, is the bounded-derivative method (Browning  et al., 1980;
Kasahara, 1982).  In this method, the analyzed  data are adjusted  to reduce
the temporal derivatives to meteorologically realistic  values.  Although

                                      69

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the bounded-derivative scheme has potential  for  future  models,  it has  not
yet been tested in regional models.

     Other methods of initialization have  involved  using  various  combina-
tions of the divergence equation and "omega" equation to  obtain winds  from
the mass field or vice versa.  For example,  in several  models  (Table 2.1),
the divergence equation with the terms  involving  the divergence set to zero
(balance equation) is used to obtain nondivergent wind  component  VNQ from
the mass field, while the co-equation is used to  estimate  the divergent wind
component.  In order to minimize the amplitude of the external  gravity wave
(Benwell and Bretherton, 1968), the vertically integrated mass  divegence  is
often eliminated (Washington and Baumhefner, 1975).  Although  these tech-
niques have been partially successful in reducing noise in models (Figure
2.11), their impact on the slower modes has  been  more difficult to show
because of the weak interaction between the  slow  and fast modes.

     A difficulty with the initialization  schemes mentioned  so  far is  that
the strong, small-scale vertical motions associated with  latent heating in
regions of heavy rainfall are not resolved.  A method that utilizes ob-
served rainfall rates to obtain vertical motions  (and the associated di-
vergent wind component) has been proposed  by Tarbell et al.  (1981). An
improvement in the very short-range (0-6 h)  forecast of precipitation  was
shown with this scheme, but the impact  after 12  h was small.

     Analysis and initialization schemes,  of course, depend  on  adequate ob-
servations, and there is evidence that  limitations  in data coverge, parti-
cularly in the Southern Hemisphere, contribute significantly to errors in
regional model forecasts.  Leslie et al. (1981)  found a decrease  in the
annual average SLP S{ score from 48 in  1978  to 45 in 1979, when an enhanced
data base associated with FGGE was available.  The  extra  data  came from
ocean buoys and the TIROS-N satellite.  It is not clear to what extent
higher-resolution data would improve regional model forecasts  over the Uni-
ted States.  However, it is likely that some improvement  could  be obtained
with more dense coverage, especially in precipitation forecasts,  since con-
siderable structure in the meteorological  variables, especially moisture,
exists in scales of motion unresolved by the current radiosonde network.

b.  Physical aspects

     The physical processes represented in a numerical  model  include energy
sources and sinks associated with fluxes of  heat, moisture,  and momentum  at
the earth's surface, in the planetary boundary layer (PBL),  and occasion-
ally in the free atmosphere.  They also include  radiation and  changes  of
phase of water in clouds of all types and  scales.  Many of these  physical
processes are associated with scales of motion smaller  than  those resolved
by the model.  These are referred to as "subgrid-scale" processes, and re-
lating their cumulative effect on the flow to the scales  of  motion resolv-
able by the model is known as parameterization.   The concept cf parameter-
ization (and subgrid-scale effects) for global models is  discussed in  GARP
Publication Series No. 8 (WMO, 1972).   According to this  report,  successful
parameterization requires a number of steps:
                                      70

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                 SURFACE  PRESSURE AT 50°N; 95° W
990 -
                                                           33
36
      Figure 2.71   Plot of surface pressure as a function of time
     at one point in hemispheric  model.  Heavy solid line is fore-
     cast from geostrophic initial  state.  Dashed line is from
     forecast initialized with analyzed winds in which vertical
     mean divergence was removed.   Thin solid line is observed
      (Washington and Baumhefner,  1975).
                                71

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     (1)  Identification of the process.

     (2)  Determination of its importance for the resolvable  scales  of
          motion.

     (3)  Intensive studies of individual cases in order  to establish the
          fact that the relevant physics and dynamics are  adequately
          understood.

     (4)  Formulation of quantitative rules for expressing the  location,
          frequency of occurrence, and intensity of the subgrid-scale •
          processes in terms of the resolvable scale.

     (5)  Formulation of quantitative rules for determining the  grid-scale
          averages of the transports of mass, momentum, heat, and  moisture
          and verification of these rules by direct observations.

     The representation of physical processes in regional models and the
impact of these processes on short-range, regional forecasts  and simula-
tions are reviewed in this section.

Surface processes

     The properties of the earth's surface, including roughness, tempera-
ture, albedo, and moisture availability  (percent of saturation)  directly
affect the vertical fluxes of momentum, heat, and water vapor into (out of)
the lowest layer of the model, and hence represent sources and  sinks of
energy.  Although these processes have been studied extensively  through
theoretical and observational programs by the boundary-layer  research com-
munity, they are only recently beginning to be studied in  the context of
their relationship to tropospheric flows in regional models.

     Treatment of fluxes of heat and moisture in regional  models varies
from their neglect to rather sophisticated parameterizations  based on a
surface energy budget.  Because the sea  surface temperature is  relatively
constant over the forecast time periods, calculation of fluxes  over  water
is relatively straightforward, and most models compute these  fluxes  over
water utilizing bulk aerodynamic formulas.

     Several regional models utilize a surface energy budget  to  obtain  the
ground temperature and moisture availability (degree of saturation of the
ground).  With these parameters and an estimate of air temperature and  wa-
ter vapor, heat and moisture fluxes may be computed using  similarity theory
(Blackadar, 1979; Pielke, 1981).  Blackadar developed an  economical, accu-
rate method for predicting the ground temperature and surface heat fluxes
(Deardorff, 1978).  This model, when coupled to a boundary-layer model,
depends on the net radiation (a strong function of cloud  cover), albedo,
moisture availability, and, to a lesser extent, the thermal capacity of the
soil.  The model is simple enough  for incorporation in operational regional
models.
                                     72

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Surface-layer and planetary-boundary-layer processes

     There are essentially two methods of parameterizing the  surface  layer
(0 - 100 m) and the planetary boundary layer  (PBL) in regional models.
Most models (Table 2.1) use the well-known bulk aerodynamic method which
treats the surface layer and PBL as a single  layer and models the surface
fluxes of heat, moisture, and momentum by exchange coefficients.  The depth
of the PBL may be fixed or vary in time (e.g., Deardorff, 1972), while  the
exchange coefficients may be constant or vary with roughness  or  static  sta-
bility.  The bulk-aerodynamic method is simple, computationally  efficient,
and has been reasonably successful in regional models.

     In recent years, a number of high-resolution boundary-layer models
have been developed and tested within a one-dimensional framework (Black-
adar, 1979; Pielke, 1981).  These models, though requiring more  computer
time (they have an additional five layers or  so), provide for more gen-
erality than the bulk PBL models, for example, during the transition  from
well-mixed conditions to stratified nocturnal conditions in which strong
vertical gradients of temperature, wind, and  moisture often exist.  Black-
adar presents additional arguments for the need for high-resolution PBL
models.  Considerable testing of various high-resolution PBL  models in  a
one-dimensional framework is discussed in the literature (e.g.,  Burk,  1977;
Chang, 1979; Yamada and Mellor, 1979).

     Extensive studies of the role of surface fluxes and PBL  processes  in
regional models have not been carried out, but a few research modeling
studies indicate the importance of the PBL on regional-scale  flows over
periods as short as 0-24 h.  For example, sea-level pressure  forecasts  have
depended rather strongly on surface friction.  Graystone (1962), Bushby
(1968), Danard (1969a), and Anthes and Keyser (1979) found differences  of
5-20 mb in the minimum pressure of cyclones  in 24 h forecasts with and
without friction.

     A simplified argument, following Danard  (1969a), yields  some insight
into the effect of surface friction on the surface pressure tendency.   The
equation of motion, neglecting horizontal diffusion, can be written

                       V = V  +Ilc x (^.-lii) ,                     (8)
                       -   -9   f     ^dt    p 3ZJ

where f is the Coriolis parameter, V is velocity, Vg is geostrophic velo-
city, p is density, and T is stress.  Substitution of (8) into the pres-
sure tendency equation
                             n
                           — = - /  gv.-pV dz                          (9)
                           at     o     n  "
yields
  dV
x — )
  dt
                                             to + gfk-v.  x  T   .       do)
                                     73

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The first two terms in (10) represent dynamical and  thermodynamical  proces-
ses (density advection and changes of vorticity)  throughout  the  depth  of
the atmosphere.  The third term represents the  instantaneous effect  of sur-
face friction.  Surface friction plays a more complicated  role than  might
be indicated at first by (10), because vertical motions  induced  by friction
modify the temperature and pressure aloft and therefore  change the first
two terms.  However, it is instructive to consider the order of  magnitude
of the friction term on the instantaneous pressure tendency.  We express
the surface stress TO by the usual quadratic law

                              T0 = POCDVV ,                           . (11)

where V is the wind speed at some level and CD  is the drag coefficient
appropriate for the wind at that level.  If we  linearize (11) by taking V
as a representative constant value and substitute into the third term  of
(10), we have
                                                                        (12)
                            ot

For g = 9.8 m s~2, PO = 1.02 kg nr3, and f = IQ-1* s'1,  (12)  becomes


                              * 100 CDVc[kPa/s]  ,                       (13)
                          0 v

where V and ? are expressed in m s"1 and s'1, respectively.  As  shown  by
(12), the instantaneous effect of surface friction  in  the  pressure  tenden-
cy varies linearly with CD and with the square of the  wind speed,  since
vorticity is approximately proportional to wind  speed.  Table  2.7  gives
pressure tendencies for various values of ? and  V for  CD = 2 x 10"  .
From this table, the effect of friction in a 24  h forecast varies  from
negligible for light winds to extremely important (24  h pressure changes
greater than 190 mb).  Of course, the tendencies given  in  Table  2.7  could
not be realized as 24 h pressure changes because of  the feedback into  the
dynamical processes aloft.

     The above discussion indicates the importance  of  boundary-layer
friction on cyclone intensity.  Other studies, using more  sophisticated PBL
models, have indicated the importance of surface fluxes on the temperature
and moisture structure of the PBL in addition to the pressure.  Yamagishi
(1980) utilized a medium-resolution PBL model based  on  similarity  theory
and the level 2 (Mellor and Yamada, 1974) turbulent  closure model  in a
regional forecast of a cold air outbreak over the Sea  of Japan.  His model
simulated the observed heat and moisture fluxes  and  the height of  the  mixed
layer reasonably well when accurate sea surface  temperatures were  speci-
fied.

     Although no systematic comparisons of the effect  of different  PBL
parameter! zations on regional model forecasts have  been made,  Miyakoda and
Sirutis (1977) studied the response of a general circulation model  to  three
different parameterizations.  The schemes tested over  a 30-day integration
were (1) Mellor and Yamada's (1974) level 2.5 closure  model, (2) a  dry

                                     74

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Table 2.7.  Instantaneous pressure change due to surface
            friction alone (rab/h) for CD = 2 x 1Q-3
                         V(m s-1)
c do-" s-1)
0.01
0.05
0.10
0.50
1.00
1
0.007
0.036
0.072
0.360
0.720
5
0.036
0.180
0.360
1.800
3.60
10
0.072
0.360
0.720
3.60
7.20
20
0.144
0.720
1.44
7.20
14.40
                            75

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convective adjustment model (Manabe et a"!., 1965), and (3) a mixed-layer
model developed by Randall and Arakawa.  Both the level 2.5 closure model
and the mixed-layer model produced more realistic simulations than did  the
forecast with convective adjustment, which showed excessive cooling in  the
lowest 400 m.

     The effects of soil moisture on a model with 2° latitude-longitude
resolution over West Africa was investigated by Walker and Rowntree (1977)
in idealized experiments.  When a dry surface typical of the Sahara was
replaced by moist land, the rainfall associated with transient disturbances
increased significantly.  Not only was precipitation affected in  the  first
two days of the simulation, a strong positive feedback between increased
precipitation and increased soil moisture was noted out to 20 days, sug-
gesting a mechanism for the persistence of precipitation anomalies.

     Leslie (1980) used a scheme based on a surface energy balance to study
the generation of the summer heat lows over Australia in over a month of  24
h forecasts.  In a comparison to forecasts without surface heating, the
mean error in minimum pressure associated with the heat low was reduced
from 2.5 to 0.9 mb, and the forecasts were judged superior by independent
observers in 35 out of 37 cases.

     Using a model with 100 km horizontal resolution, a prognostic surface
energy budget, and a medium-resolution boundary-layer model, Benjamin
(1982, personal communication) found that surface heat, moisture, and mo-
mentum fluxes had a large impact on forecasts as short as 12 h over the
central United States under severe weather conditions.  Using data from
the SESAME-I (10-11 April 1979) and SESAME-IV (9-10 May 1979) experiments,
he found significant differences in boundary-layer temperature, specific
humidity, and surface pressure between 12 h forecasts with and without  sur-
face fluxes (Figure 2.12).  These differences were caused by differential
heating associated with topographic variations, cloud cover, and  variable .
surface characteristics (notably moisture availability), differential eva-
poration, and changes in the horizontal transport of mass, heat,  and  water
vapor associated with the changing pressure field.

     In summary, surface fluxes of heat, moisture, and momentum have  been
shown to be important in 0-48 h forecasts on the regional scale in a  number
of case studies.  There is also evidence that horizontal variations in  sur-
face parameters and cloud cover can produce significant horizontal varia-
tions in PBL structure on these time and space scales in numerical models.
While it has not yet been shown that the use of a surface energy  budget
over land coupled with a medium-resolution boundary-layer model will  signi-
ficantly improve regional-scale forecasts, there is enough evidence to  war-
rant testing of a model with these properties on a large number of cases.

Condensation and evaporation processes

     The release of latent heat of condensation represents an important
source of energy for synoptic-scale cyclones (Aubert, 1957; Danard, 1964;
Tracton, 1973) and is also important in modifying the larger scale environ-
ment.  Observational studies (Nh'nomiya, 1971; Maddox et a!., 1981; Fritsch
and Maddox, 1981a) have shown the development of anticyclonic perturbation

                                     76

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     0 K%
      \  ••.  •-.
      » •.
       \
      /
"	
                                . .^..../.	-Iv	,;&*'	...A
                                r\yi f     \ »    :'.-*•	\
                                : /&*/      ••  I   :   I
Figure 2.12   Difference  fields  in  12  h forecasts with and without
surface fluxes of heat and  water vapor.   Forecasts were initialized
at 1200 GMT 10 April  1979.   Thick solid lines are surface pressure
differences in mb.   Dashed  lines are temperature differences at
lowest level  in model  in  K.   Thin solid lines are differences in
specific humidity at lowest level in model  in g kg-' (Benjamin, 1982,
personal communication).
                              77

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flows in the upper troposphere over mesoscale regions  of  precipitation.
The increasing baroclinicity often induces an upper-level jet  streak  north
and west of the convective system.

     Numerical models have successfully simulated the  development  of  meso-
scale convective systems and the effect of latent heat on the  environmental
flow.  Chang et al. (1982) isolated the effect of latent  heating on a 24  h
forecast by subtracting a forecast without latent heating from a control
forecast which contained heating.  Figure 2.13 presents the  24 h forecast
height, temperature, and vector wind differences (wet-dry) on  the  700,  500,
and 300 mb pressure surfaces.  As expected, the maximum differences occur
over the regions of intense precipitation.  The major  patterns are a  cold
low at 700 mb, a warm low at 500 mb, and a warm high at 300  mb.  Throughout
the troposphere, there is a net increase in the area-mean (calculated over
the region depicted in the figures) 24 h predicted  temperature due to the
latent heat release.  This temperature increase is  largest at  300  mb
(0.85°C), decreasing in magnitude downward to 700 mb (0.03°C). The height
difference fields indicate an average increase in the  700-500  mb thickness
of 5 m and an increase in 500-300 mb thickness of 13 m.   More  significant
to the dynamics, however, are the large horizontal  gradients in temper-
atures and heights, which produce changes in the winds and vertical mo-
tions.  Comparing the vertical velocity fields (not shown) between the wet
and dry simulations, the wet case produces much larger upward  motion  in  the
area of positive temperature difference at 500 mb.  This  indicates that  the
latent heating exceeds the adiabatic cooling and, thus, the  air column is
forced to expand.  Consequently, relatively high and low  pressure  areas  are
generated in the upper and lower troposphere, respectively.

     At 300 mb, the generation of high pressure to  the north fills the
northern portion of the large-scale trough, and the generation of  low pres-
sure to the south deepens the southern portion of the  trough.  As  a result,
a cut-off low forms in the wet run.  The corresponding change  in wind cir-.
culation enhanced the north-south temperature advection.  These processes,
in conjunction with latent heating, appear to be responsible for the  dis-
tribution of positive temperature difference over a rather wide region.   At
500 mb, the temperature difference is confined to the  areas  of large  preci-
pitation, indicating that latent heating and adiabatic cooling are the main
factors in determining its pattern, i.e., the effects  of  the latent heat
are not rapidly advected out of the region.  At both 500  and 300 mb,  the
increase in temperature due to the inclusion of condensation processes
occurs largely in the colder air.  Thus the upper-level baroclinicity is
reduced.  At 700 mb, the change in temperature is related more to  cold
advection than to diabatic processes.

     In response to the enhancement of the pressure gradient,  the  winds  in-
crease their cyclonic circulation at 700 and 500 mb and their  anti-cyclonic
circulation at 300 mb.  As evidenced by the increased  vertical motion, the
wet case's low-level winds have a stronger cross-isobaric component than  do
those of the dry case.  The maximum wind difference is 21 m  s"1 at 700 mb,
14 m s"1 at 500 mb, and 35 m s   at 300 mb.  At all three levels,  this
maximum occurs over the northwest quadrant relative to the precipitation
field.  This preference is similar to that shown by Maddox et  al.  (1981)
for mesoscale convective complexes (MCCs).

                                     78

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      QEOPOTENTIAL
                      TEMPERATURE
                        VECTOR WIND
 SON
 40N
 SON
     110W   100W   90W   110W  100W   90W
                                300 mb
                                           110W   100W    SOW
 SON
 40N
 30N
     110W   100W
                     110W   100W

                            500 mb
 SON
 40N
 30N
                                                              SON
                                                              40N
                                                              30N
                                                              SON
                                                              40N
                                                              30N
                                                110W   100W   SOW
                                                              SON
                                                              40N
                                                              30N
110W   100W
                    90W
110W   100W
       700mb
 Figure 2.13  24 h simulated 700, 500 and  300 mb "wet" minus  "dry" height,
temperature and vector wind difference fields.  The height  interval is 10 m
on both  the 700 and the 500 mb levels and  20 m on the 300 mb  level ; the tem-
perature interval  is 1°C for all three levels and the isotach interval is
5 m s-1 . The  dashed contours denote negative  differences (Chang et al., 1982)
                                   79

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     The strong effects of latent heat shown  in Figure 2.13  have  been  found
in other models with rather different parameter!zations of convective  heat-
ing.  Anthes et al. (1982a) showed that latent heating induced  a  divergent
anticyclonic wind perturbation near 300 mb with a jet streak of over
15 m s"1.  In the boundary layer, the latent  heat generated  a pressure de-
crease of more than 7 mb and a cyclonic circulation with perturbation  wind
speeds greater than 10 m s"1.  Similar results were obtained by Maddox et
al. (1981) and Ninomiya and Tatsumi (1981).

     It is well known from theoretical and numerical studies that the  ver-
tical distribution of convective heating is extremely important in deter-
mining the evolution and structure of tropical cyclones (Anthes,  1982a).
As regional models are increasingly applied to study middle-latitude phe-
nomena, it is becoming clear that the vertical distribution  of  latent  heat-
ing is also a crucial  factor in the development of  real and  model  cyclones
(Tracton, 1973; Anthes and Keyser, 1979).

     Primitive equation models have demonstrated the sensitivity  of meso-a
scale extratropical circulations to rather small changes in  the specified
vertical  distribution of heating whenever substantial (greater  than about
2 cm of rain per 12 h) precipitation is predicted.  Anthes and  Keyser
(1979) showed an example of a 12 h forecast in which lowering the maximum
in the specified vertical distribution of convective heating from 480  to
600 mb produced a cyclone with minimum pressure 11 mb lower.  The greater
proportion of heat released in the lower troposphere destabilizes the  atmo-
sphere and permits a much more rapid intensification.  This  interpretation
is consistent with Sutcliffe's (1947) development theory, in which the
greatest brake on a developing cyclone is the adiabatic cooling associated
with upward motion (Petterssen, 1956, p. 329).  It  is also consistent  with
Staley and Gall's (1977) study which showed that the wavelength of maximum
growth in a baroclinically unstable environment shifts toward smaller  wave-
lengths (~ 2000 km) as the lower troposphere  becomes less stable.

     Observational studies have demonstrated  the importance  of  evaporation
on the meso-y and meso-0 structure of precipitating systems.  Zipser  (1969)
showed that evaporation was an important (indeed, essential) process in the
maintenance of a tropical precipitating system.  Moncrieff and  Miller
(1976), Ogura and Liou (1980), and Houze and  Betts  (1981) discuss the  im-
portance of evaporation in producing the downdraft  structure of thunder-
storms and squall lines.  Brown's (1979) numerical modeling  study showed
that evaporation was the primary mechanism in driving a meso-g  scale  down-
draft.  While considerable effort has been devoted  toward understanding the
role of evaporation on small mesoscale features, relatively  little atten-
tion has been paid to the effects of evaporation on meso-a scale  features.

     Although it has been demonstrated conclusively that latent heat re-
lease and its vertical distribution can influence significantly the evolu-
tion of regional forecasts, the problem of accurately parameterizing the
effects of cumulus convection is still unsolved.  As discussed  by Anthes
et al. (1982b), cumulus convection affects the environment through diabatic
heating and cooling associated with condensation, evaporation,  freezing and
melting,  through vertical fluxes of sensible  heat,  moisture  and momentum,
and through horizontal pressure perturbations.  The processes are highly

                                     80

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nonlinear and depend in complex ways upon the size spectrum of clouds  and
on the environmental flow.

     Some success with cumulus parameterization schemes of varying  com-
plexity has been reported by Kuo  (1965, 1974), Arakawa and Schubert (1974),
Kreitzberg and Perkey (1976), Anthes (1977), Hayes (1977), Sundqvist
(1978), and Fritsch and Maddox (1981b).  The Arakawa  and Schubert and  the
Kuo-type parameterizations have been verified by diagnostic studies in the
"semi-prognostic" sense, as discussed by Lord (1980)  and Krishnamurti  et
al. (1980).  Figure 2.14 shows the observed and computed rainfall rates
from a cumulus parameterization based on Kuo's (1974) scheme.  Although not
a complete test in the sense that feedbacks between the convective  heating
and dynamical fields are not allowed, such studies provide encouragement
that realistic cumulus parameterization in regional-scale models  is pos-
sible.

     Perhaps the simplest parameterization of cumulus convection  is the
convective adjustment scheme (e.g., Manabe et al., 1965), which consists of
the adjustment of model lapse rates that exceed the wet adiabatic value
under conditions of convective instability.  Convective adjustment  schemes
tend to underforecast convective  rainfall rates while simultaneously over-
predicting the area of convective rainfall (Hayes, 1977).  After  introduc-
ing a scheme in which the parameterization of deep cumulus convection  was
controlled by large-scale convergence of water vapor  and conditional in-
stability (a Kuo-type parameterization), the operational UK regional model
showed increases in convective rainfall over England  in summer by more than
40% and "significant improvements" in the "forecast patterns  and  amounts of
rainfall" (Hayes, 1977).

     Ninomiya and Tatsumi (1980), in a simulation of  Baiu frontal rainfall,
found that a moist convective adjustment scheme which worked  well in a
381 km mesh forecast gave unrealistic results with a  77 km mesh.

     Parameterizing cumulus convective effects as a function  of the resolv-
able scale becomes questionable as the grid size becomes smaller  than  about
100 km.  For finer meshes, the separation between the resolvable  and con-
vective scales becomes less and the model may begin to simulate the same
clouds it is also trying to parameterize.  For high-resolution models,
therefore, it may be preferable to abandon the concept of parameterization
in favor of explicit treatments of condensation and evaporation through the
introduction of prediction equations for cloud and precipitation  water.
This strategy has shown some success in studies by Rosenthal  (1978)  and
Ross and Orlanski (1982).

Layered clouds and radiative effects

     Clouds greatly modify the shortwave and longwave radiation budget and
thereby exert an important control on the evolution of the planetary bound-
ary layer.  The surface energy budget at the earth's  surface  is responsible
for generating important mesoscale circulations such  as sea breezes, moun-
tain-valley breezes, and in producing conditions of low-level  stability
that are favorable for moist convective systems.  Thus, even  nonprecipi-
tating clouds are probably important in perturbing regional-scale flows.

                                     81

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               KU07H
                              12  13  I*  IS  IS   17
               TIME(DflYS)
Figure  2.14   Comparison of observed (dashed line)
and predicted (solid line) rainfall rates  (mm/day)
using  Kuo's (1974) convective parameterization
scheme.   Days 1 to 18 correspond to the third phase
of GATE between 1 September and 18  September 1974
(Krishnamurti et al., 1980).
                     82

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     Clouds can have an important effect on the atmosphere  over  short  time
periods through differential heating between clear and cloudy  regions  and
through destabilization of the atmosphere by strong  cloud-top  cooling  (Dan-
ard, 1969b; Cox, 1969; Gray and Jacobson, 1977).  In  spite  of  their  impor-
tance, most regional models either neglect nonprecipitating clouds entirely
or parameterize their radiative effects in a crude manner based  on the mean
layer relative humidity.  Layered, nonprecipitating  clouds  are particularly
difficult to parameterize in numerical models because they  are often much
thinner than the vertical resolution of the models.  An  example  of the dif-
ficulty in relating middle tropospheric cloud amounts to mean  layer  rela-
tive humidity is shown in Figure 2.15.

     Slingo (1980) used statistics from GATE data to  develop a parameter-
ization for the percentage of low, medium, high, and  convective  clouds.
Because observations showed that layer clouds were concentrated  over dis-
turbances and decreased rapidly away from the disturbance,  quadratic rela-
tionships between relative humidity R and cloud amount were developed:

                 CH  =  (R - 80)2/400        R > 80

                 CM  =  (R - 65)2/1225       R > 65                  (14)

                 CL  =  (R - 80)2/400        R > 80
                                                                        o
where CH, CM, and C|_ are the percentage  of  high, medium,  and  low
clouds, respectively.  This scheme was tested  in a  large-scale  model  (2
latitude-longitude mesh) and was found to predict the  cloud distribution
reasonably well, including the difficult-to-predict stratocumulus  clouds.

     An alternative approach to the  statistical methods  of estimating cloud
cover is to predict the clouds explicitly.  Sundqvist  (1978)  proposes a
scheme involving a prognostic equation for  cloud liquid  water content.   The
scheme, tested in a one-dimensional  model,  gave realistic vertical  distri-
bution of cloud water, precipitation and evaporation.

     Probably the most important radiative  effect on short-range  regional
model forecasts is the absorption of solar  radiation at  the surface,  which
is the main driving mechanism for surface sensible  and latent heat fluxes.
In the free atmosphere, changes of temperature due  to  the absorption  of
shortwave radiation during the day and emission of  longwave radiation at
all times are approximately 1-2°C per day when averaged  over  layers of  the
thickness of most numerical models.   Because these  diabatic heating rates
are small compared to other diabatic and adiabatic  rates  of temperature
changes, most regional models neglect radiative effects  above the  surface.

     While radiation parameterizations are  uncommon in present  regional
models, considerable effort has been devoted to modeling  radiation in gen-
eral circulation models.  These methods, which range in  complexity from di-
rect numerical integration of the radiation transfer equations  to  the use
of climatological means, are reviewed in WMO (1972).

     Although layered-mean diabatic  heating rates associated  with  radiation
are small, rates over thin layers in the vicinity of cloud tops can be

                                      83

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    8

_  7


I  '
 ?  5
 o
 u
 O
-  3
            10     20      30     40      50      60      70      80      90    100%

                                    Relative humidity
                   Figure 2.15   Scatter  diagram of observed
                   middle cloud amount against mean relative
                   humidity for the layer 700-500 mb
                   (Slingo, 1980).
                                        84

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large and affect the development of clouds.  Using  a  5-band model  to  cal-
culate the infrared heating rate above layered clouds, Roach and Slingo
(1979) found cooling rates of more than 8°C h"1 in  a  thin  (1 mb) layer
above the cloud.
uy/yj round co
above the cloud
     Interaction of radiation and clouds may be significant  in modulating
cloud growth and precipitation, and may be responsible  for the observed
diurnal  variations in tropical precipitation (Gray  and  Jacobson,  1977).
Possible mechanisms are the destablization of cloud tops  during  the  night
and enhancement of mesoscale circulations through differential radiative
heating between cloudy and clear regions (Anthes, 1982).

     Compared to the efforts devoted to parameterizing  surface fluxes,
planetary boundary layer processes, and cumulus convection,  and  to evalu-
ating the effects of parameterizations in regional  models, there  have  been
only limited studies on radiative effects.  In one  of the few studies,
Kubota (1981) considered the radiative effects on an 8-day northern  hemi-
sphere forecast.  The major effect of clouds was to reduce the average
cooling in the lower troposphere and increase the cooling in the  upper
troposphere, which represents an increased greenhouse effect.  Offsetting
the greenhouse effect slightly were an increase in  reflected solar radia-
tion (albedo effect) and a reduction in surface heating (ground  effect)  in
the experiment with clouds.

     Hollingsworth et al. (1980) compared two 10-day forecasts with  differ-
ent radiation parameterizations (as well as different parameterizations  of
other physical processes).  In the simpler scheme,  the  radiative  absorbers
(H20, C02, and 03) and the clouds were specified as temporally constant
functions of latitude and height.  In the second scheme,  the moisture  and
clouds varied, allowing for a cloud-radiative feedback.   C02 was  constant
in space and time, and 03 was a specified function  of all three  spatial
coordinates.  Although differences in mean heating  rates  over the 10-day
period were several degrees Centigrade per day, there were only  minor  dif-
ferences in the forecasts.

2.4  Summary and conclusions

     This section has reviewed the current status of operational  and re-
search numerical weather prediction over limited-area,  regional  domains.
Over the past decade there has been intensive research  activity  in several
operational centers and research institutions around the  world.   While in-
creases in the accuracy or skill of operational short-range  forecasts  have
occurred over this period of time, there remains much room for improvement,
especially in the prediction of significant weather such  as  quantitative
precipitation.  These improvements, if they occur,  will  probably  not result
from a major breakthrough in any one aspect of the  regional  models because
there are so many numerical and physical factors that are important  in pro-
ducing an accurate prediction or a realistic simulation.  These  include  the
accuracy and density of the initial data, the analysis  and initialization
methods, the numerical treatment of the partial differential equations,  and
the modeling or parameterization of physical effects, including  surface
fluxes,  boundary layer processes, release of latent heat, moist  convective
transports, clouds, and radiation.

                                     85

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     A number of research models investigating the  above  effects  have  de-
monstrated the importance of each on a limited number of  cases.   What  is
needed now is a systematic testing of regional models which  includes  the
potential improvements proposed in the research models.   These  tests,  and
future research model experiments, would be most effective  if a comprehen-
sive set of verification statistics were computed.   In addition to  the con-
ventional measures of skill such as Sx scores, other less conventional  sta-
tistics such as the structure function of various variables  or  the  separa-
tion of errors by scale would be useful in assessing a model's  realism,  the
rate of improvement over time, and in model intercomparisons.   Examples  of
these measures of skill were provided in Section 2.2 of this chapter.-

     In constructing improved models, there are always tradeoffs  between
accuracy and computational requirements.  In addition, a  balance  must  be
maintained between accuracy and computational expense among  the various
components of the model.  A highly sophisticated, computationally expensive
physical parameterization, for example, is unjustified unless the errors
associated with other physical and numerical approximations  are of  the same
order as the errors introduced by that particular process.

     To close, we speculate based on the results reviewed in this section
how a state-of-the-art regional model might be constructed  in order to pro-
vide the meteorological information necessary for a regional air  quality
model of acid deposition.  Previous research has set the  stage  for  rela-
tively rapid development and application of such a  model. This hypothe-
tical model would contain about 20 layers and utilize fourth-order  spatial
finite differencing on a staggered horizontal grid  with an  implicit (or
semi-implicit) temporal integration scheme.  The high resolution  (-50
km) portion of the grid would be nested within a larger scale,  global
model.  It would be analyzed and initialized by a combination of  an optimal
interpolation analysis scheme and a nonlinear normal mode initialization
procedure.

     The physical parameter!'zations would include a medium-resolution
(about five layers) PBL formulation coupled with a  surface  energy budget
and a diurnal cycle.  The parameterization of the effects of cumulus  con-
vection would depend on the dynamic and thermodynamic structure and evo-
lution of the resolvable scales (such as moisture convergence or  rate  of
destabilization and the vertical temperature and moisture structure).   The
effect of nonprecipitating layered clouds would be  considered in  the  sur-
face energy budget by relating the amount of these  clouds to the  mean  layer
relative humidity.

     While no one model containing all of the above features exists,  each
feature may be found in at least one model and many may be  found  in sev-
eral.  Such a model is computationally feasible with existing computers and
evidence may be found in the literature for the importance  of each  feature.
                                     86

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                                CHAPTER FOUR

            THE MATHEMATICS AND PHYSICS OF METEOROLOGICAL MODELS


1.  OBJECTIVE ANALYSIS1

1.1  Introduction

     Regional acid deposition models solve initial value problems,  and  so
require initial data of all predicted meteorological and chemical  varia-
bles.  The initial data are generally required on a  regular array  of  grid
points, and yet observations are almost never regularly spaced.  In the
context of regional acid deposition models, therefore, objective analysis
is the development of computer methods for transforming meteorological  data
from irregularly-spaced observations into meaningful data at  regularly-
spaced intervals compatible with the coordinate system of a particular
numerical  model.  If the vertical coordinate used for the analysis  is dif-
ferent from that of the model, analysis errors introduced because  of  the
required vertical interpolation should be considered for overall evaluation
of the method.

     The earliest effort to analyze meteorological variables  was to fit
two-dimensional polynomials to the irregularly-spaced observations. The
advantage of this analysis was definition of the field at every  point  in
the domain, but it was not reliable in regions of nonuniform  data  coverage,
and discontinuities at the domain boundaries required excessive  smoothing.
Spectral  objective analysis, which represents distributions of meteorologi-
cal variables by a set of mathematical functions with wave-like  character-
istics, has been employed with some success—particularly on  a global
scale.  The most widely used methods today are grid  point methods  using
first guess values obtained from climatology, persistence or  a dynamic
forecast,  and then utilizing the observed values to  correct the  first guess
errors.  The final analyzed field is obtained from a linear combination of
corrections, determined for each grid point from the observations  (within
some predetermined influence range) and weighting coefficients assigned to
each observation.  A standard procedure is to analyze the "difference"
fields, i.e., the differences between the observed values and the  interpo-
lated first guess values at the observation locations.  Difference  value
fields exhibit a desirable quasi-isotropic property.

     Perhaps the most controversial aspects of objective analysis  are the
techniques used to calculate the most appropriate (optimum) weighting
     Contributed by Philip Haagenson.  A  slightly  revised  version  of  this
section has been submitted for publication in Papers  in Meteorological
Research.

                                     87

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coefficients and the degree to which physical  relationships  (constraints)
among variables should be employed.  Also, the assessment  of  computational
cost relative to the quality of the final analysis  is  an important consi-
deration.

     In this section, we will describe and evaluate objective analysis
methods with consideration given to their desirability  relative  to re-
gional-scale analysis and to their computational expense.  Global-scale
analysis is assumed to resolve synoptic-scale  disturbances.   Regional-scale
analysis is assumed to resolve both synoptic-  and mesoscale  disturbances.
Historical perspective, where appropriate, will be maintained.   Certain
aspects of physical constraints between variables will  also  be considered,
and some important issues regarding selection  of weights will  be discussed
in detail.  Experimental comparisons of a few  analysis  methods will  also be
presented.  We will begin with a description of observing  systems and the
representativeness of observations, since the  quality  of any  analysis
method is dependent on these.

1.2  Observing systems and the representativeness of observations

     The primary observing systems for measuring meteorological  variables
are surface stations including ships, upper-air soundings  (raobs),  and
satellites.  The basic measurements are pressure, temperature, wind,  and
relative humidity.  Satellites, however, measure only  vertical temperature
structure and infer winds from sequential cloud images.

     The temporal  resolution is 3 h for surface observations  and 12 h for
upper air observations.  The vertical resolution obtained  from radiosondes
is - 25 mb.  For satellite observations, the vertical  resolution of tem-
perature is ~ 200 mb and winds are resolved at only two or three levels,
typically 850 and 250 mb.  The spatial density of surface  land stations is
nearly an order of magnitude greater than for  radiosonde land stations,
which in the United States are - 300-400 km apart.  Satellite observa-
tions are utilized mainly over the oceans where radisonde  stations are
extremely sparse.

     The quality of objective analysis is lowered by observational  errors.
Most analyses are more sensitive to correlated than to random errors, par-
ticularly if the errors are horizontally correlated.   Surface and radio-
sonde measurement  errors are normally not horizontally correlated, and  the
magnitude of the random errors is usually not  large enough to degrade ser-
iously the quality of the analysis.  Satellite measurement errors, however,
are spatially correlated and of sufficient magnitude to increase signifi-
cantly the analysis error in regions where satellite observations are the
principal source of data.  A simulation study  conducted by the European
Centre for Weather Forecasts indicated the root mean square  (rms) analysis
errors of height {height of a pressure level)  and wind fields in the  tropo-
sphere are three to four times greater for the combination of satellite and
surface observations compared to the combination of radiosonde and surface
observations (Bengtsson, 1976).

     Both radiosonde and satellite data are objectively analyzed (opera-
tionally) by the National Meteorological Center (NMC)  (their method will  be

                                     88

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described later) and interpolated to a global  latitude-longitude  grid mesh
with a resolution of 2.5°.  The final analysis  is  archived  at  NMC,  NCAR,
and the National Climatic Center (NCC) every  12  h  for  ten pressure  levels
from 1000 to 100 mb.  Surface station observations,  including  cloud and
precipitation information, are archived  every  3  h,  but are  not analyzed to
a grid.

     The archived NMC meteorological fields are  the  basic input to  several
forecast and transport models.  When used  as  input for mesoscale  models,
the interpolation of data from the  coarse  NMC  grid {-  250 km)  to  the
model grid (< 100 km for most mesoscale  models)  smooths the analysis to the
extent that it should be used only  as a  first  guess  field.   In this case,
an appropriate objective analysis should again  be  performed using available
data to derive a final analysis.

1.3  Analysis methods of questionable or unknown quality

     Polynomial fitting was mentioned in Section 1.1.   It represents the
earliest efforts in objective analysis,  but is  considered unsatisfactory in
comparison with methods developed more recently.

     Fitting two-dimensional cubic  splines to  irregularly spaced  observa-
tions has certain advantages, over polynomial  fitting.   Constraints  such as
continuity of the function and its  derivatives  at  the  data  points provide
for better analyses, especially in  regions of  nonuniform or sparse  data
coverage.  However, examination of  some  experimental results indicates that
sometimes the analysis does not resolve  observed maxima and minima.

     Sasaki (1958, 1970) developed  a method of  objective analysis utilizing
the calculus of variations (variational  method).   A  functional, consisting
of analyzed-minus-observed differences and dynamical constraints, is mini-
mized.  The analysis is a quasi-initialization  analysis in  the sense that
it might be effective in making the analyzed  fields  compatible with a fore-
cast model.  The method is complex  and computationally expensive, and Sasa-
ki does not show any experimental results.

     Three-dimensional grid point analyses have  been obtained  by  construct-
ing a series of nearly parallel, north-south,  isentropic (constant  poten-
tial temperature e) cross sections  and then analyzing  the domain  between
them by using a second set of nearly orthogonal  cross  sections.   An advan-
tage of using isentropic coordinates for objective analysis is evident in
the vertical cross section analysis of 0 and wind  velocity  shown  in Fig-
ure 1.1.  We observe that the mid-troposphere  frontal  structure (the region
containing strong static stability  and wind shear)  has a fairly small  hori-
zontal scale on P surfaces (~ 100 km), but on  e surfaces the horizontal
scale is much larger (~ 1000 km).   Thus, the  frontal zone should  be
easier to analyze in an isentropic  framework.   One disadvantage of  analyz-
ing in 0 coordinates is that e surfaces  become  vertical  or  even folded in
the mixed boundary layer.  A disadvantage  of  using this particular  three-
dimensional approach is that the interpolated  values between the  north-
south cross sections are of questionable accuracy,  and the  scheme has not
been tested on enough cases to verify its merit.


                                     89

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 mb

 100
 150
 200
 300




 400



 500



 600


 700


 800

 900

1000
                                                     3OO
                                                     280
           Son    Los
           Diego  Angeles
 Point
Arguello
Oakland
Medford
Salem
Seattle
              Figure 1.1    Subjective cross-section analysis of
              potential temperature and normal  component of hori-
              zontal wind  velocity for 1200  GMT 21  April 1963.
              Solid lines  are  isentropes (degree Kelvin).  Dashed
              lines are isctachs m s~l (Duquet  et al., 1966).
                                       90

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1.4  Computationally inexpensive methods  of  reliable  quality

     Since most objective analyses  require  "inverse"  interpolation  of grid
point values to observation locations  or  interpolation  from coarse  resolu-
tion grids to higher resolution grids,  it is  appropriate,  at  this  point,  to
evaluate briefly a few grid point interpolation  techniques.

     Koehler (1977) evaluated seven techniques by  using analytic  functions
(chosen to be meteorologically realistic)  to  provide  data  values  at both
grid point and observation locations so that  the interpolation  errors could
be defined exactly.  The techniques used  and  the results of his study -are
shown in Table 1.1.  Techniques 01, D2, Cl,  and  Bl  are  four-point  tech-
niques; the others are 16-point.  The  evaluation indicates that B2, 12,
and L3 introduce the smallest interpolation  errors.   However,  since the
overlapping quadratic polynomial technique,  B2,  requires only  25  percent  as
much computational time as L2 or L3, it is  the most preferable  of  the seven
techniques.

a.  Cressman analysis method

     Probably the most frequently used objective analysis  method is the
Cressman technique (Cressman, 1959).   It  is  a grid point method using a
first guess field (normally a forecast) and  explicitly  assigns  weighting
coefficients to the interpolated difference  values  at the  observation lo-
cations.  The Cressman technique has been subjected to  years  of operational
use as one stage in the production  of  the NMC forecast  model.

     The basic analysis procedure is as follows:   given n  observations of
a difference variables, D|< (observed-minus-interpolated first guess val-
ues), at n observation locations (k =  l,n) within  some  influence  range of
radius R and distance d^ from grid  point  i,  we can calculate  the  differ-
ence D-J at location i from
                                    Wk  Dk
                         Di  '
                                   I
                                 k=l
where the weighting coefficients,
weighting function
                                       are  given  by  the  distance-dependent
                                 R2 -
                                 Rz +
Successive scans using decreasing  radii,  R,  are  employed to allow for anal
ysis of smaller scale disturbances.   In practice,  in  regions of good data
coverage (adequate observation density and fairly  uniform distribution),
ttiree or jfour scans are used, with R  ranging from  a maximum of - 47T to
d, where d is the mean distance between observation locations.
                                      91

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Table  1.1  Comparisons  of interpolated vs. observed values for  temperatures,
height,  and u  and v wind components at the 850,  500, and 300 mb  levels.   The
seven  interpolation techniques  are listed at  the bottom (Koehler, 1977).
             TOT KSU.TS RM TtHrtMtlK CO
                                                               TKT man FW «cavwan in/s)


•MR
ttwi.u
Imn
toot
mm
S4M^M
lrr»n
Wi. Irrwi
)•
tern
•50
SCO
300
no
SOD
300
MO
ITOWOUTION irnaos
ti
O.M
0.10
0.04
0.20
0.13
0.01
-0.47
02
0.10
0.0*
0.03
0.13
0.0*
0.04
-0.2S
i
C1
0.22
0.14
0.0*
0.27
0.17
0.07
-0.40
II
0.03
0.02
0.01
0.04
0.02
0.01
-0.0*
tt
0.00
0.00
0.00
0.00
0.00
0.00
0.01
12
0.01
0.01
0.00
0.01
0.01
O.W
0.02
13
0.00
0.00
0.00
0.00
0.00
0.00
0.01
            TtST KSU.TS fW 1 COVOKNT (N/S)

•Mil
IktaUt*
Irron
Iwt
MMK
Crrors
MM. Crren

m
U«L
HO
MO
300
*M
SCO
300
500
IITIWOUttOII IC1M3DS
01
o.x
O.S7
O.M
0.3*
0.7»
O.M
-3.12
02
0.17
0.32
0.3*
0.23
O.S4
O.M
O.S*
C1
O.M
0.72
0.14
O.M
O.M
I.M
-3.04
II
0.0»
0.1*
0.17
0.11
0.44
O.M
-3.4«
If
o.n
0.13
0.12
0.07
0.3S
0.2*
-2.41
II
0.0*
0.23
0.33
0.10
O.M
0.73
O.M
13
O.OS
0.11
0.2*
P. 08
O.M
O.tl
-2.17


MM
•WllU
[mm
•M
S«m«
Iinii
•M. Crr*r<
•
uni
HO
MO
300
BO
HO
300
MO
nmwouiTiw ICTMOS
Bl
0.23
O.«l
O.M
0.10
O.S*
o.;:
-1.74
w
0.12
0.27
0.30
0 15
0.44
0.45
-l.U
C1
O.M
0.52
0.61
0.3C
0.74
o.is
-3.1S
•1
O.W
0.15
0.17
O.W
o.n
C.2S
.1.17
u
o.ot
0.07
o.o;
o.os
0.21
0.1*
-1.21
12
0.05
O.It
0.21
0.11
0.35
0.47
-2. OS
13
0.02
0.11
0.18
O.W
0 15
0.41
-I.3S
                                                           TtJTS KSULTS TO HCIGMT (K1EK)


HMII
*M«l
-------
     A commonly applied modification  is  to  assume  that  the  difference field
is nonisotropic and to define a radius of influence  (dependent  on  wind ve-
locity) as

                       R*2   =  R2  (1  + a cos2  a)   ,                      (3)

where a is the angle between the position vector  (locating  an observation
with respect to the grid point) and the  wind velocity at  the  grid  point.
3 is proportional to the wind.speed.

     A conventional relationship between variables that is  often used,in
the Cressman and in other objective analysis methods  is the geostrophic
relationship between height  gradient  and observed  wind

                   32  =  f  «           8Z  -     f  ..
                   "37     £g    '        "9y"""Cgu>

where g is the acceleration  of gravity,  Z is height,  f  is the Coriolis
parameter, C depends on the map scale factor,  and  u  and v are the  compo-
nents of the observed wind along the  x and  y grid  directions.   If  we as-
sume that the observed wind  velocity  t is approximately equal to the geo-
strophic wind velocity ^g, except  at  low latitudes where  f  is small  or in
the planetary boundary layer where the friction force is  large, we can cal-
culate a height difference, D^, at observation location k (using observed
winds and the first guess height field)  from


                 Dk  =  Zs + ( " Cg  v - * Cfg u  ) - Zi  '          .     (5)

Here Zs is the first guess interpolated  height at  location  k, Zf is  the
first guess height at grid point i, and  AX  and Ay  are the [x(grid  point)  -
x(observation)] and [y(grid point) - y(observation)3  distances, respective-
ly.  If the observation at location k reports  both wind and height,  then
Zs in (5) is the observed height.

     The Cressman method has been used for  both global  and  regional  analy-
sis.  Calculations of rms differences between  analyzed  and  observed  values
suggest that for analyzing synoptic-scale disturbances, it  compares  quite
favorably with other methods that  are computationally more  expensive if a
good first guess field is available and  the analysis  is over a  data-rich
region.

b.   Barnes analysis method

     This grid point method, developed by Barnes  (1964, 1974),  is  similar
to the Cressman scheme, but the weighting function is derived using  a sim-
plified Fourier analysis and is related  to  an  accuracy  index  function that
is wavelength dependent.

     Consider an atmospheric variable distributed  as f(x,y)  = A sin(ax),
which for simplicity is uniform in the y direction,  and a = ir/L, where L  is
half the wavelength of the disturbance.  If we assume a continuum  of obser-
vations of f(x,y), and filter (weight) these data  with  respect  to  their

                                      93

-------
distance from an arbitrary point  (x,y), we  can  define  a smoothed function
g(x,y) as

                     2ir  »
         g(x,y)  =  /   /  f(x+r  cosa, y+r  sina) F(r,k)  r  dr  da  ,       (6)
                   0   0

where r is a distance vector from grid point  (x,y)  to  observation point
(x+r cosa, y+r sina), a is the angle  between  r  and  the x axis,  and  the
filter function, F(r,K), is expressed as


                    F(r.K)  -  (      exp ( -)  )   ;                  (7)
K is an arbitrary parameter.  We can  rearrange  (6)  to  define  the  weight
function, W(r,K), as

                        W(r,K)  =  exp  ( -    }   •                       (8)
     We want to determine the  relationship  between  the  observation value,
f, and the weighted average value, g, at  the  same point (x,y).   Using the
definition f(x,y) = A sin(ax), we can expand  the  expression  f(x+r cosa,
y+r sina) and substitute the result and (7) into  (6).   The final  inte-
gration of (6) gives the filtered response  to  f(x,y) as

                    g(x,y)  =  exp (-a2K) [A  sin(ax)]   .                 (9)

The response function,  "accuracy index,"  J, =  exp(~a2K),  and can be written
in a different form as


                        J  =  exp [ - ^  ( ^ )  ]   ,
                                     R2     L2

where R is the radius of influence.  J is a function of two  lengths, K,
which is related to the weighting function  and determines its shape, and L,
which is related to the wavelength of the disturbance.   The  choice of K in-
volves prior knowledge  of the  wavelength  and  observed  data distribution.

     We can utilize the accuracy index, J,  in  the following  way.  Given
some appropriate choice of K,  we can divide_the  numerator and the denomi-
nator of the exponent in (10)  by "d"2, where  d  is  the mean  distance between
observations.  Then, for any combination  of R/cT  and L/d,  we  can calculate J
which, depending upon these parameters, may range from  ~  0.5 to .95 (.95
would imply that 95 percent of the amplitude  of  the wavelength  was retained
and only 5 percent_lost through smoothing).   Normally,  the accuracy is
rather low when L/d < 2 unless R/d" < 2.   If L/d  > 4, the accuracy is high
unless R is several times larger than 1L

     The Barnes method  might be preferable  to  the Cressman method for anal-
yzing mesoscale disturbances because it provides  an index for determination
of the observation density required to resolve small-scale disturbances.

                                     94

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1.5  Computationally expensive  analysis  methods  of higher quality

     Since most objective  analyses  are  grid point methods and assign
weights to the observed difference  values  ( observed-mi nus-first guess), it
is advantageous to derive,  in an  objective manner, the  most representative
weighting coefficients.  Gandin (1963)  proposed  a statistical  regression
procedure to select the optimum weights,  hence defined  as "optimum inter-
polation," or 01.  The weighting  coefficients  are determined from the con-
dition that the rms error  of the  analyzed  difference values at the grid
points be a minimum over a  large  ensemble  of synoptic situations.  They
depend ultimately upon the  covariances  or  correlations  (spatial autoco-
variances or autocorrelations)  among  the  observation difference values.
Because an enormous amount  of historical  data  is required to calculate the
needed covariances for all  variables  at  all  levels and  all  geographical lo-
cations, they are usually  modeled mathematically as a function of distance
separating observations and grid  points.

a.   Univariate optimum interpolation

     We can write (1) in a  slightly different  form


                            D.   =    I    W.  D.   .                         (11)
                            1     k=l   K   K

To derive the optimum weighting coefficients,  W|<9 we have to minimize the
rms error of (u-j - D-j) , where  S-j is  the  true  difference value at
grid point i, and the overbar denotes an  average over an ensemble of in-
dependent realizations of  the field.  The  minimum rms error condition is


                W7  ( 61 j. WK  DK )2   *   °    (J ' X'n)  '
                  J       1\ ™X

which generates a system of n linear  algebraic equations for the weights
                                            (j  =  l,n)   ,                 (13)


where j and k are the observation  locations,  i  is  at  the grid point loca-
tion, n is the number of observations  within  influence range of the grid
point, and TJ^UJ and tTjUJ are  the covariances.  We  don't know 0-j,
so at this point it is  necessary to make  some assumptions.   We assume that
the covariances are isotropic  in two  dimensions  and that Oj  behaves sta-
tistically like any of  the D^.  Also,  since correlations of  difference
values plotted against  observation separation distance,  d, usually show
less scatter than^ covariances,  it  is  common practice  to assume that the
variances Dj2 = D-j2 = T5j<2.  Thus,  (13)  can  be written in terms of a
distance-dependent correlation  function u(d)  as
                                      95

-------
                   I  Wk n(d)..  =  v(d)..   (j = l,n)   .                (14)
                  k=l        *J          'J

     Figure 1.2a is an example of a correlation (II) scatter  diagram  de-
rived from historical data (500 mb heights during two winters)  for  50 Uni-
ted States raob stations.  Figure 1.2b shows a correlation  curve  of the
form p(d) = C!exp(-c2d ), modeled to fit the data of Figure 1.2a.   The
weights, Wfc, needed to solve (11) are now given by  the  solution of  a  sys-
tem of linear algebraic equations (14) whose coefficients are  the correla-
tion coefficients easily determined from observation separation distances
and from (grid point to observation) separation distances.

     An important advantage of optimum interpolation is  that  the  method
considers the positioning of data points with respect to each  other.   If
two stations are located on or near the  same line through the  grid  point,
the outer observation often receives a negative weight  which  can  allow the
analyzed value to exceed the largest or  smallest observed values  in its
vicinity.  Negative weights are normally not used in the Cressman method.

     Bengtsson (1976), using (12) and (13), obtained the expression for the
analysis (interpolation) error at grid point i,
                                   k=1


where e-,2 is the error normalized by the variance.  Then,  to  illustrate
the effects of observation errors  (random and correlated)  on  ZW^  and
ej, he modified (14) to allow for  observation errors  and  simulated a
simple case using the observation  distribution  shown  in Figure  1.3a.  The
analyzed values are assumed to be  height differences  and  the  II correlation
function is defined as u(d) = exp(-c2d2), where  c2  is 2.0 if  d  is given in
units of 1000 km.  The results of  the simulation are  shown in Figure 1.3b.
Observe the interesting variation  of the sum of  the weights,  zWfc, with
respect to d.  It is greater than  1.0 (no observation error case) up to
about 800 km.  This means that if  four stations  within this distance range
of the grid point are observing difference  values higher  than the reference
state, then the analyzed grid point value would  be  higher than  the observed
values.  In the Cressman method, the sum of the  weights,  expressed as in
(11), is equal to 1.0.  We also note that in this particular  simulation the
observation error has only a small effect on ei.  The e-j  curve  for the
correlated observation error implies that a maximum of -  90 percent of
the first guess error can be removed when d < 200 km, whereas no  reduction
in the first guess error (for all  three cases)  is possible when
d > 1300 km.

b.   Univariate optimum interpolation, isentropic coordinates

     Bleck and Haagenson (1968) and Bleck (1975) proposed optimum interpo-
lation on isentropic surfaces.  The advantages  of analyzing meteorological
fields in an isentropic framework  were discussed in Section 1.3  (refer to
Figure 1.1).

                                     96

-------
                     ZZ CORRELATION VS. DISTANCE
<
LU
IT

S
O
             1.0


             0.8


             0.6


             0.4


             0.2

              0


            -02

            -0.4


            -Q6
             1.0
            0.8
            0.6
         §  Q4
         UJ
         I  "
         u
             0

           -0.2

           -0.4
                                       (a) -
0.5
1.0
 1.5   2.0

DISTANCE
                                2.5
                                              3.0    35
                     ZZ CORRELATION VS. DISTANCE
                                               (b)
                    Damped
                    Persistence
                    0.5   1.0   1.5   2.0    2.5

                              DISTANCE
                                     3X)   35
Figure  1.2    Correlation of difference values (a),  between
the 500 mb  height and a damped  persistence forecast as  a
function of separation distance,  d,  (units, 103 km)  between
every pair  of 50 U.S. raob stations;  and the correlation
curve (b) to fit the data after averaging within distance
intervals.   The curve is based  on the expression:
M (d) = q  exp (-C2 d?) (Schlatter,  1975).
                                 97

-------
            1.0
            0.8
            0.6
            0.4
            0.2
                (b)
                                2        3

                            DISTANCE
Figure 1.3   Four symmetrically situated height (difference
value) observations  (a) influencing grid point i, and the
variation (b) of E wj< and ^ as a function of distance, d,
(units, 4 x 102 km).  Curve (1) denotes no observation error
Curves (2) and (3) denote random and correlated rms obser-
vation errors respectively, of 30 in (Bengtsson, 1976).
                               98

-------
     In isentropic coordinates, the Montgomery  potential, M  =  gZ  + CpT
(Cn is the specific heat at constant pressure), takes  the place of geo-
potential  in isobaric coordinates.  Bleck  (1975) analyzed the  M,  u,  and  v
difference value fields in a univariate sense,  but he  used the geostrophic
relationship, i.e., the relationship between  the gradient, vM, and the
observed winds to provide a more accurate  analyzed M field.  For  economy,
Bleck used a crude first guess for M based only on the nearest two obser-
vations.  His first guess u and v fields were based on geostrophic values
obtained from the final M field.  He obtained statistical (historical) data
from 50 synoptic situations in North America  during winter and spring
1972/73 and used all e levels simultaneously  for calculating the  correla-
tions necessary to model the correlation function y(d).  For MM correla-
tions, he assumed that y(d) has the form


                         u(d)  =   I  C  ds  ,
                                  s=l  s

where the coefficients Ci ... c6 are coefficients of a Taylor  expansion  and
d is in units of 10  km.  He did not show  the form of  the expressions used
to model the correlation functions for u and  v.

     Bleck applies his method with two scans.   The second one  of  smaller
radii is not optimal in the sense that the errors over a larger number of
cases are not minimized.  Thus, his analysis  may exhibit larger rms errors
but analyze the short wave disturbances better.  This  might  result in a
better forecast.  To assure vertical consistency of the final  M field, he
applies vertical constraints in the form of a vertical  least squares fit of
3M/30 and 32M/362.

     Few historical data sets for relative humidity exist.   Bleck and Haa-
genson (1968) used data from ten different sounding times to derive an ex-
pression for the relative humidity correlation  function.  It has  the form
y(d) = cosUd/2) exp(-1.5 d), where d is in units of 103 km.

     A comparison of results of Bleck's analysis with  results  from other
methods will be presented in Section 1.7.

c.   Multivariate optimum interpolation

     Schlatter  (1975) demonstrated a multivariate optimum interpolation
method for simultaneous analysis of the wind  and height fields.   In his
method, (11) is expanded and becomes
                      n           n           n
              DT  *   I  W.  Dk +  I  W' D'  +  I W" D" ,              (16)
               1     k=l  K  K   k=l  K  K   k=l  K  K
where D^ is the height difference  at  observation  k,  D^'  = sD^/sx,  and
D^" = 3D|
-------
computational time by a factor of 3.

     Schlatter (1975) used the historical data shown  in Figure  1.2a  and the
ZZ correlation curve shown in Figure 1.2b.  His ZZ model  has  the  form  y(d)
= 0.95 exp(-1.24 d2), where d is in units of 103 km.  A damped  cosine curve
can be used to fit the data if the negative correlations  are  not  discard-
ed.  He modeled the other correlation and cross correlation functions among
Z, u, and v difference values assuming that all the covariances and  cross
variances were related to the ZZ covariances through  the  approximate geo-
strophic relations in latitude, , and longitude, A,  coordinates.  Thus,
distance, d, between any two locations,  i,j, is given by
d
2  =          -    2    2 **   *3'
              =  A [ (A. - A..)  cos2    2  3 +  0- -  ^)   ]   ,          (17)
with A the earth's radius in units of 103 km.  Figure 1.4a  shows  the  ZZ,
uu, and vv 500 mb correlations obtained from the modeling.  Schlatter 's
correlation models compare favorably with the 500 mb correlations  calcu-
lated by Buell (1959) for a master station located at Columbia, Missouri
(Figure 1.4b).  Note that uu and vv correlations are not  isotropic, but are
elongated along the u and v directions, respectively.  Climatology was  Bu-
ell 's first guess, and the historical base (observed values of Z,  u,  and  v)
was obtained from radiosonde data for a five-year .period.

     Schlatter (1975) tested his method at Topeka, Kansas each day during
the winter of 1965-66.  The network density of United States  radiosonde
stations used in the analysis is shown in Figure 1.5a.  Rms differences
between analyzed (interpolated in observation locations)  and  observed
values of Z, u, and v at Topeka for the period of study indicated that  the
five closest stations provided all of the useful analysis information.
Figures 1.5b and 1.5c demonstrate the influence of nonuniform observation
distribution on rms differences.  When the five nearest surrounding sta-
tions were chosen, the rms differences for Z, u, and v were 14 m,  4.1,  and
3.4 m s"1, respectively.  The larger rms errors shown in  Figure 1.5c  illus-
trate that observations within influence range— outside the perimeter of  a
grid domain— should not be excluded from the analysis.  For comparison  pur-
poses, he also calculated the rms differences in a univariate sense.  The
results did not clearly demonstrate that multivariate analysis is superior
to univariate.

     Several optimum interpolation methods have been described.   The  main
advantage of optimum interpolation over other grid point  methods  is that
the method considers the positioning of data points with  respect  to each
other and thereby results in weights that can define maxima and minima  in
that field.  This does not necessarily imply that mesoscale features  will
be better resolved.  A disadvantage of optimum interpolation, besides being
computationally expensive, is the lack of historical data necessary to  ac-
curately model the correlation functions.  Rajamani et al.  (1980)  showed
that the uu and vv correlations for the observed u and v  difference values
(over India) varied with level, season, and region.  A common practice  is
to assume no variation for levels, seasons, and regions.  Clearly, more
historical data sets should be obtained.

                                     100

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  I  1  I   I  I   I  I   I  I
zz
  I  I   I  I   I
                   I	1
                                   I   I  1   I  I
                            I   I  I  1   I  I   I  I   I
                                                                        I	I
                                     (a)
 ZZ
500km
UU
                          SOOkm
                                     (b)
         Figure 1.4   Correlations of difference values (a) for each
         of the variables Z, u and v based on the expression
         u(d) = 0.95 exp (-1.24 d2) for ZZ correlation and geostrophic
         relations, and correlations (b) among the same variables as
         calculated by Buell (1959) from five years of U.S. raob data
         for master station Columbia, Mo.  In (a), the diagrams are
         centered at 1100H, 35°N, and the tick marks are 500 km apart
         (Schlatter, 1975).
                                      101

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Figure 1.5   Network of U.S.  raob stations (a)  numbered
in order of increasing distance from Topeka,  Kansas.
Rms differences between analyzed and observed values  of
Z (m), u and v components of the wind (m s -1)  calculated
for Topeka using stations located only within specified
semi-circles (b) or quadrants (c)  (Schlatter,  1975).
                              102

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     Optimum interpolation  can  be  applied  to  analysis of synoptic-scale
disturbances on a global or  regional  scale (a global  design  method will be
described in the following  section).   If 9 coordinates instead of P coor-
dinates are used in optimum  interpolation  (and also in other reliable anal-
ysis methods), certain  frontal -related mesoscale meteorological  features
(above the boundary layer) might be  resolved  more accurately.

1.6  Analysis methods used  by NMC

     We observed in Section  1.2 that the archived NMC meteorological  fields
(derived from their final analysis)  are the basic input to several forecast
and transport models.   It is therefore appropriate to discuss  the analysis
methods that have provided  these archived  data.   The Cressman  method was
used by NMC until 1972  when  it  was replaced by a global  spectral  method.
We have already described the Cressman analysis, so we will  begin discus-
sion of NMC analysis methods with  a  description  of the spectral  analysis.

a.   Three-dimensional  spectral analysis

     The spectral analysis method  (Flattery,  1970) is three-dimensional;
data at all levels are  used  simultaneously.   The analysis is spectral in
the sense that a set of mathematical  functions with the wave-like charac-
teristics describe the  meteorological  fields  rather than discrete values
associated with grid points.  The  method is designed to minimize the rms
differences between the analysis and observations, or, in regions where
observations are sparse, between the analysis and first guess  forecast
values.  The analysis incorporates a geostrophic relationship  between
heights and winds.  The permissible  wavelengths  in the east-west direction
are those which are given an integral  number  of  waves around the globe at
all latitudes.  The amplitudes  of  these wave  functions are expressed as
functions of $ and P.   The  variation of the amplitudes in the  north-south
direction is given by a summation  of functions called Hough  functions.
Thus, for example, the  equation defining I, expressed as a function of X,
4>, and P is

                        24   24    7
          Z(<,<|>,P)  -I    I     I   { [Cj cosUx) + C2 sinUx)]
                        z=0  m=l  n=l
where a, is the wave number,  H£jm(<}>)  denotes  the Hough functions,  and
En(P) indiates the empirical  functions  which describe the vertical  var-
iation of Z.  The coefficients  Ci(x.,m,n)  and C2U,m,n)  assign relative
weights to each of these  terms  so  that  the total  summation will  fit, in a
least squares sense, the  observed  heights.

     The spectral analysis method  is suitable only  for global analysis.  A
comparison of results  (with  an  optimum  interpolation  analysis method in
Section 1.7) suggests  that some regional -scale meteorological features are
not well resolved.
                                      103

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b.   Multivariate three-dimensional optimum  interpolation

     In 1978, the NMC spectral analysis was  replaced  in  the  final  analysis
cycle by an optimum interpolation multivariate method  (Bergman,  1979).
Part of the rationale for employing the new  analysis method  was  based upon
the changing character of the operational data base.   An increased volume
of meteorological data is now contributed from observation systems other
than conventional radiosonde and surface network  systems (principally sat-
ellite).  The NMC optimum interpolation analysis  is specifically designed
to enable blending of data from different observing systems  (the spectral
method did not possess this flexibility).  Observations  are  assigned rms
errors, and some observational errors are assumed to be  vertically or hor-
izontally correlated.  The method utilizes three-dimensional  correlation
functions defined as products of quasi-horizontal  and  vertical correla-
tions.  Terrain-following sicpa coordinates  are employed because NMC wanted
to avoid vertical interpolation (after the objective analysis) from pres-
sure coordinates to the forecast model coordinates.   In  this analysis,  tem-
perature replaces height as one of the analyzed variables; Z is  calculated
hydrostatically  from P and T.

     Temperature and winds are analyzed multivariately,  imposing the geo-
strophic constraint in the form of the thermal wind equations


            3u   _  GRc   3T             3v   _  GRc  ,  3T >
                 ~                            ~            "
                _
            W  ~  W  L  3y  j  »        W ~  TP~  l  ax" J   '

where f is the Coriolis parameter, Rc  is  the specific  gas  constant for
air, and G is the "coefficient of geostrophy," which  is  defined to in-
crease, nearly linearly,  from zero at  the  equator  to 0.85  at 30°  latitude
and approaches a value  of 1.0 at 50° latitude.   In practice,  however,  the
analysis is fully multivariate only in  data sparse regions;  otherwise, it
is univariate or bi van ate.

     Bergman followed Schlatter's method  to model  the  lateral  TT,  uu,  and
vv difference correlations (the first  guess is a six-hour  forecast).   Since
he assumed that the isobaric TT correlation function  behaved like  the  ZZ
correlation function, his correlations  and cross correlations  closely  re-
semble Schlatter's.  The  vertical correlation functions  were obtained  from
other vertical autocorrelation statistics.

     The procedure for  analyzing a variable at a grid  point  is normally to
select only the ten observation difference values  (sometimes there are more
than that within influence range) that  are assigned the  largest weights
(absolute value).  Since  the analysis  is  three-dimensional and partly  mul-
tivariate, some of these  values might  not be the same  variable or  located
£t the same level .

     Table 1.2 shows some experimental  results for variations  of the  analy-
sis.  We notice that the  normalized estimated analysis errors  appear  to be
more sensitive than the rms  differences to observational  errors (compare
runs J and K).  This suggests that the  rms differences should  not  be  used
as an exclusive measure of "goodness of analysis."  The  analysis does  not


                                     104

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Table 1.2  Comparison of experimental  results  for variations of the analysis
at 500 at) for 0000 GMT 13 December  1977.  The  analysis  was restricted to the
Northern Hemisphere  (Bergman,  1979).


Maximum
Normalized esti-
mated errors
number of
Run
A

B
C
0
E
F
G
H
I

J

K

Description
6 h prediction
(background fields)
MuUivariate (T, u, v)
MuUivariate (T, u, v)
Univariate T, bivariate (u, v)
Multivariate (T, u, v)
Univariate T, bivariate (u, v)
Muttivariate (T, u, v)
MuUivariate (T, u, v)
(u. v) obs. for T anal. T obs.
for (u, v) anal.
MuUivariate (T, u, v)
obs. errors halved
Multivariate (T, u, v)
obs. errors doubled
observations T

0
10
10
10
20
20
6
8

10

10

10

1.0
0.621
0.616
0.634
0.587
0.622
0.654
0.634

0.897

(0.561)

(0.736)
u.v

1.0
0.623
0.625
0.626
0.594
0.602
0.647
0.635

0.932

(0.582)

(0.713)
rms differences
from observed
data
T
(°C)

1.85
1.25
1.'26
1.25 •
1.30
1.27
1.22
1.24

1.76

1.15

1.38
M.i
Ons'1)

13.97
8.65
8.65
8.65
9.13
9.14
8.64
8.71

14.04

7.98

9.73
                                        105

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attempt to fit the data exactly; the forecast field  is  assumed  to  have  some
skill.

     For analysis of synoptic disturbances on a global  scale, this NMC
method is probably one of the best available today.  However, its  computa-
tional expense, related in part to the global aspects of  its  basic design,
does not make the method particularly desirable for  regional-scale analy-
sis.

     Since 1978, the archived NMC data have been derived  from the  optiimum
interpolation analysis.

1.7  Experimental comparisons of objective analysis  methods

     Otto-Bliesner et al. (1977) compared results  of three different analy-
sis methods (over a four-day period in a data-rich area)  to determine their
ability to fit data to the observations and to define the amplitude and
phase of synoptic-scale waves.  The methods compared were the NMC  opera-
tional Cressman analysis using a 12-hour forecast  for the first guess;  a
global multivariate optimum interpolation analysis (Schlatter et al.,
1976), where the first guess was a forecast from the NCAR global circula-
tion model; and the isentropic optimum interpolation method (Bleck,  1975)
described in Section 1.5-b, where a crude first guess was employed.   These
methods were also compared to subjective analysis  of the  same data set.

     The comparison for the 500 mb height analyses (Figure 1.6a) suggests
that the multivariate method did not resolve the intensity of the  cyclone
over the southern United States as well as the other methods  (perhaps NMC
had a better first guess).  Figure 1.6b indicates  that  rms height  differ-
ences (above the boundary layer) between analyzed  and observed  values were
minimized to the greatest extent by the isentropic method.  Considering
that Bleck used a crude first guess and had to interpolate his  final  anal-
yzed fields from e into P coordinates, the results he obtained  are impres-
sive.

     McPherson et al. (1979) compared some results (for one observation
time) of analysis obtained from the NMC spectral method and the NMC optimum
interpolation method.  The comparison indicated that the  optimum interpola-
tion analysis resolved wind speed gradients more accurately than the spec-
tral analysis in regions of pronounced cyclonic and  anticyclonic height
curvature.

     We have chosen to show a result of the moisture analysis comparison
because humidity fields usually exhibit smaller-scale gradients than other
meteorological fields.  Figure 1.7a gives the vertical  temperature and  dew
point profiles for Pensacola, Florida at 0000 GMT  14 December 1977.  Low
relative humidity (- 10 percent) is observed near  775 mb. Figure  1.7b
shows vertical cross sections of analyzed relative humidity along  30°N.
The location of Pensacola is identified by the vertical dashed  lines.  We
observe that the "dry layer" between 700 and 800 mb  is  analyzed much more
accurately by the optimum interpolation method.  The dry  layer  was also
observed at other radiosonde locations along the cross  section.


                                     106

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SON
25N
   125 W
                   NMC
       500 MB I2Z II DEC 67
                (a)
                                                     MUUTIVARIATE
              70W 125 W


    HEIGHT RMS (m) I2Z 11-14 DEC 67
                   mb
                   100


                   150


                   200


                   250


                   300


                   4OO


                   500


                   700


                   850
-(b)
                   — NMC
                   — ISENTROPIC
                   — MULTIVARIATE
                   — SUBJECTIVE

                    	i    i    i
                             10   15   20  25

                                      M
                      30  35  40  45
                                                                         70 W
  hgure 1.6    500 mb height (a) analyzed by each method  for 1200 GMT
  11 December  1967 (contours are in decameters with the leading digit
  omitted), and  rms height differences  (b)  between analyses  and observed
  data, averaged for 1200 SMT 11 - 14  December 1967  (Otto-Bliesner et
  al., 1977).
                                        107

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                         400
                          mb


                         500



                         600


                         700


                         800


                         900
                                    (a)
                        1000
                           -30° -20° -10° 0°(C) 10° 20°

                                    TEMP
                                      (b)
                  OPTIMUM ANALYSIS
                              SPECTRAL ANALYSIS
        UJ
        CC
        en
        UJ
        cr
        a.
        UJ
        x
        o
        
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     Reimer (1980) objectively analyzed  several meteorological  variables
over the data-rich region of Central Europe  (on two  different  days)  using a
univariate optimum interpolation method  in  isentropic  coordinates.   One of
the principal  purposes of his experiment was  to compare  the  analyses ob-
tained using three different grid resolutions (381  km,  190.5 km,  and
95.25 km at 60°N).  The mean distance between observation  locations  was
- 300 km.

     Some aspects of his analysis method were similar  to Bleck's.  However,
one unique aspect of his method, relative to  normal  optimum  interpolation
procedure, was that he derived the correlation functions from  data corre-
sponding only to the day of the analysis.   Thus,  to  get  enough  correlation
products, he assumed no dependence of the correlation  function  with  respect
to the vertical coordinate, i.e., he used the correlations of  the  observed
difference values on 24 e surfaces from  the  surface  to  100 mb.

     The results of his study suggest that  analyzing on  the  high  resolution
grid provides the best analysis.  Figure 1.8  shows  a comparison of  vertical
cross sections of the analyzed relative  humidity.   We  observe  that the high
resolution grid analysis (D) most closely resembles  cross  section  (A)--sub-
jectively analyzed from the observations.

1.8  Summary

     A number of considerations determine the utility  or desirability of an
analysis method.  Among these are:  (I)  the  ability  of  the method  to dis-
tinguish between accurate and erroneous  data  and  to  assign errors to ob-
servational data, (2) the ability to fit the  data  to the observations and
blend data from different observing systems,  (3)  the ability to resolve the
desired spectrum of wavelength scales and the applicability  of  the method
to global or regional analysis, (4) the  degree to which  the  analysis is
compatible with the forecast (or transport)  model,  and  (5) the  computa-
tional  expense.

     The most frequently used objective  analysis  method  is probably  the
Cressman method.  It has been used for both  global  and  regional  analysis,
and experimetal results suggest that, for analyzing  synoptic-scale disturb-
ances in data-rich regions, the Cressman method compares quite  favorably
with other methods that are computationally  more  expensive.

     The Barnes method, which is similar to  the Cressman method,  might be
preferable for analyzing mesoscale disturbances because  it provides  an
index for determination of the observation  density  required  to  resolve
small-scale disturbances.

     Optimum interpolation methods are computationally  expensive,  but they
should provide higher quality analysis because the  distance  function for
the weights is linked to the spatial autocorrelation of  the  data.  The main
advantage is that the weighting technique allows  for better  definition of
maxima and minima in the data field.  Observation  errors can also  be real-
istically accounted for in the analysis.  A  disadvantage is  the lack of
historical data necessary to model the correlation  functions accurately.
Optimum interpolation can be applied to  analysis  of  synoptic-scale dis-

                                     109

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Figure 1.8   Vertical cross-sections of relative humidity generated
by objective analysis for 1200 GMT 2 March 1977, where B, C and D
denote 381, 190.5 and 95.75 km-grid resolutions respectively.
Analysis (A) was generated subjectively.   The horizontal  extent of
the cross-sections are v!900 km  (Reimer, 1980).
                                  110

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turbances on a global or regional  scale.

     If 8 coordinates instead of P  or  a coordinates  are  used in  objective
analysis methods, certain frontal-related mesoscale  features (above the
boundary layer) might be resolved  more accurately.   This review  suggests
that more studies need to be conducted using  "observational  dense"  meteor-
ological data sets obtained from field projects  such as  SESAME  (1979)  for
further evaluation of objective analysis methods  appropriate for analyzing
mesoscale disturbances.
2.  INITIALIZATION

2.1  Introduction

     The purpose of the  initialization  for  a  numerical  model  is  to achieve
an initial data set in which  the  temporal accelerations are  small  and re-
present meteorologically significant  scales of  motion.   If this  criterion
is met, we say that the  initial data  are  balanced.   The requirement is to
prepare grid point data which  the model can integrate  forward in time with
a minimum of noise and maximum accuracy of  the  forecasts on  the  meteoro-
logical scales that the model  is  designed to  simulate.   As pointed out by
Anthes (1979), the relative  importance  to the forecast of the initial anal-
yses of wind, temperature, and moisture compared  to  the other components of
the meteorological model varies considerably  with horizontal  scale and the
meteorological situation.  A  detailed representation of the  initial  condi-
tions  is most important  on large  scales and when  the local  forcing func-
tions  are weak.  As the horizontal  space  scale  decreases, a  detailed re-
presentation of the initial  conditions  becomes  somewhat less  important.
The specified conditions on  the boundaries  assume greater importance since,
under  all but very light wind  conditions, the variations associated with
the initial conditions are advected away  from the domain early in the fore-
cast.  Furthermore, the  local  forcing by  terrain, frictional, and diabatic
effects becomes more important on the smaller scales.   On the urban scale,
therefore, detailed initial  conditions  are  unnecessary; the  solutions will
be determined almost entirely  by  the  boundary conditions (possibly time-
dependent) and the modeling  of the  local  forcing  functions.   On  the large
regional  scale (400 x 400 km  or greater), however, the initial  conditions
must be resolved in some detail.  Haltiner  and  Williams (1980) have provid-
ed detailed descriptions of  most  initialization procedures.   Here, various
schemes will be summarized.

2.2  Damping scheme

     An obvious approach to  reduce  the  noises caused by the  imbalances in
the initial data set would be  to  dampen or  filter the  noises.  It is im-
portant to apply a numerical method which can selectively dissipate high-
frequency modes.  The numerically dissipative Euler  backward  scheme has
been tested by Okland (1972),  while Talagrand (1972) has used the addition
of a divergence damping  term  in the momentum  equation.   A combination of
the horizontal diffusion and  the  Euler  backward scheme has been  suggested
by Anthes (1974).
                                      Ill

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2.3  Variational scheme

     Sasaki (1958, 1969, 1970a,b,c) has developed an  initialization  and
objective analysis scheme to obtain a balanced set of  dependent  variables
under the variational principle in which differences  between  the objec-
tively-analyzed values and the newly-adjusted values  are minimized  in  a
least-square sense, subject to one or more dynamical  constraints.  The
scheme has been applied to diagnostic studies of the  planetary boundary
layer in conjunction with a squall line by Sasaki and  Lewis  (1970)  and of
flow-over complex terrain by Sherman (1978) and Dickerson  (1978).  A
three-dimensional initialization procedure using variation analysis  has
been suggested by Barker et al. (1977), and has been  applied  by  Kaplan
et al. (1982) as one step in their model initialization.

2A  Static scheme

     Static initialization adjusts the initial data under  some dynamical
constraints in order to reduce or eliminate the generation of noise  from
model calculations at a single time level.  It is generally  divided  into
two categories as follows:

a.  Nondivergent initialization

     Vorticity fields are first computed from analyses of  horizontal winds,
and then the stream function is calculated from the vorticity by inverting
the Laplace operator.  The geopotential and temperature fields are  finally
obtained by solving the balance and the hydrostatic equations, respective-
ly.  Anthes (1976) has put forth this procedure for the mesoscale model and
it has subsequently been used by Warner et al. (1978)  for  regional-scale
simulations.

b.  Divergent initialization

     In addition to nondivergent initialization, which computes  the  stream
function from the vorticity, the velocity potential is also  retained by the
relationship between velocity potential and divergence, which is obtained
by solving the omega equation and the continuity equation.   Both the stream
functions and the velocity potentials are used to solve the  divergence
equation for geopotential.  Divergent initialization  has been employed in
studies of synoptic-scale phenomena by Houghton et al. (1971), Lejenas
(1977), and Dey and McPherson (1977), and to  hurricanes by Miller et al.
(1972) and Mathur (1974).  Application of divergent initialization  to  the
regional scale has been demonstrated by Tarbell et al. (1981).

2.5  Dynamic scheme

     Dynamic schemes allow for a mutual adjustment between the mass  and
velocity fields.  In order to obtain balanced initial  conditions for a
model, the model is allowed to be integrated  numerically forward and back-
ward about the initial time or forward for a  long enough period  to  let the
model balance itself before starting the prediction.   Miyakoda and  Moyer
(1968) and Nitta and Hovermale (1969) have shown results from some  early
experiments that accomplished dynamic initialization  by integrating the

                                     112

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model system back and forth in time about  the  initial  state.   Dynamic
initialization by nudging (Anthes 1974) has been tested with  three-fluid
models by Hoke and Anthes (1976) and has been  applied  to  simulate  a real
hurricane by Hoke and Anthes (1977).  A similar dynamic initialization  pro-
cedure can be found in a low wind speed simulation,  in order  to  bring  the
effects of orography and surface roughness into the  simulation smoothly
(Warner et al., 1978).

2.6  Nonlinear normal mode scheme

     In order to eliminate noise (i.e., gravity waves) and  make  better  use
of data of varying accuracy for a global-scale model,  a balanced initial
state can be obtained by balancing nonlinear modal  equations  through the
perturbation method (Baer, 1977) or the iteration method  (Machenhauer,
1977).  It is an ideal scheme for the global spectral  model,  but has also
been applied to the grid-point model by Temperton and  Williamson (1981) and
Williamson and Temperton (1981).  Daley (1981) and  Kasahara (1982)  have
given excellent reviews of the nonlinear normal mode scheme.   Application
of this scheme to the limited-area model has been tried by  taking  a portion
of the balanced initial data set from a global model (Machenhauer,  1980)  or
by setting periodic or zero time-derivative boundary conditions  (Kaplan et
al., 1982).

2.7  Bounded-derivative scheme

     The theory of the bounded-derivative  scheme is  based on  the observa-
tion that a solution of the scaled equations with a time  scale of  order
unity must have a number of time derivatives of the  dependent variables of
order unity.  This observation is applied  to derive constraints  on  the  ini-
tial data at the initial time.  The original theory  has been  proposed  by
Kreiss (1970), and has subsequently shown  its  applicability to the  shal-
low-water equation in both the midlatitude and equatorial data planes
(Browning et al., 1980).  To initialize a  limited-area shallow-water sys-
tem, the well-posed boundary conditions with the system can achieve smooth
numerical solutions (Browning and Kreiss,  1982).  Application of the bound-
ed-derivative scheme to a baroclinic primitive-equation model  has  been  pro-
posed by Kasahara (1982).

2.8  Summary

     Among these initialization schemes, the damping scheme is the  simplest
one and the only one which does not contain any dynamical constraints  on
the initial data.  The variational scheme  can  include  one or  more  dynamical
constraints, such as the balance equation, hydrostatic relation, steady-
state momentum equations, integral relations conserving energy and  mass,
zeroing integrated mass divergence, etc.   Except for a few  applications to
numerical models, the variational scheme has been applied mostly to diag-
nostic studies because it is quite complicated and  expensive  to  compute and
its accuracy depends in part on how well the atmosphere behaves  under  dyna-
mic constraints.  Nondivergent initialization  is straightforward and easy
to implement in numerical models.  If it is found that the  nondivergent
scheme cannot adequately obtain a balanced initial  data set,  divergent
initialization should be applied.  The static  scheme is recommended as  the

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initial test for an entire regional-scale numerical model  system.   The dy-
namic scheme is a natural one for initializing  such a model;  however,  be-
cause of its expensive computational cost,  it cannot easily  compete with
the others in an operational sense.  Unless other  schemes  fail  to  produce
satisfactory initial data, the dynamic  scheme might be  used  only  to provide
a benchmark for comparison.  The nonlinear  normal  mode  scheme has  shown
that accurate initial data can be obtained, but the construction  of normal
modes for a limited model is difficult.  The interpolation from global  ini-
tial data which is balanced by the nonlinear normal mode  scheme relies on
the global data set, and may lose some  regional-scale features.  However,
it may be possible to utilize such a balanced large-scale  analysis as-a
first guess, which is then modified by  high resolution, regional  data.   The
bounded-derivative scheme does show very high potential for  application to
the limited-area model.  Further developments and  tests are  needed before
the scheme is adopted.
3.  BOUNDARY CONDITIONS

3.1  Introduction

     The numerical treatment of boundaries  is a difficult  but  very  impor-
tant aspect of a limited-area forecast model.  A  set  of well-posed  computa-
tional  boundary conditions should be formulated for the limited-area  model
with open boundaries, where larger-scale forcings  are specified,  regional-
scale features are not affected, and smaller-scale noises  disappear.   An-
thes and Warner (1978a) have demonstrated the serious errors that result in
mesoscale models if lateral boundary conditions are incorrectly  specified.
Feeding larger-scale information into the regional-scale model  gradually
and smoothly has been relatively successful.  There are various  interpola-
tion schemes that can be combined with the  model  initialization  procedure
to interpolate the larger-scale information into  regional-scale  grids, such
as those reported by Perkey (1976), Shapiro (1977), Warner et  al. (1978),
and Ross and Orlanski (1982).  However, much of the difficulty  arises in
developing a well-posed condition to allow  the regional-scale  phenomena to
move freely across boundaries (Elvius and Sundstrom,  1973;  Oliger and Sund-
strom,  1978; Sundstrom and Elvius, 1979).

     As discussed by Moretti (1969), the only straightforward  case  occurs
when the flow is supersonic, in which case  the value  of an inflow boundary
may be arbitrarily specified, and the values of an outflow boundary ob-
tained by a linear extrapolation outward from the  interior of  the domain.
In the subsonic case, however, waves may propagate in the  flow in the in-
terior of the domain.  Thus, the arbitrary  specification of either  constant
or time-dependent boundary values may make  the problem ill-posed.  The fol-
lowing schemes are currently utilized in various  numerical  models or  are
being developed.

3.2  Sponge boundary scheme

     If the boundaries are located far enough away from the region  of in-
terest, the errors introduced at the boundaries will  remain within  some
acceptable tolerance in the interior of the domain during  the prediction

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period.  Sometimes the noise induced at the boundary  is  fast-moving  waves,
and the prediction can be ruined in a short period.   Thus,  some  damping
techniques should be applied to reduce or eliminate the  noises  along the
boundary zone.  Pielke (1974) has suggested the  expanding  grid  net because
high wavenumbers are not recognized by the expanding  grid  spacing  toward
the boundary.  A weighting factor assigned to the  time tendencies  along the
boundary zone to isolate the noises has been proposed by Perkey  and  Kreitz-
berg (1976) and applied by Perkey (1976) to a regional-scale  model.   Adding
an artificial Newtonian damping term with a relaxation coefficient to the
governing equations in the vicinity of the boundary is suggested by  Davies
(1976).  Benwell and Bushby  (1970) have used horizontal  diffusion  with a
large diffusion coefficient  to control the growth  of  spurious waves  at the
boundaries.  The sponge boundary scheme may be employed  at either  the upper
or lateral boundaries.

3.3  Radiation boundary scheme

     Formulations for open boundary conditions to  allow  disturbances to
move out of the model domain with a minimum of boundary  reflection have
been continuously developed  since the introduction of the  Sommerfeld radi-
ation boundary condition to  the limited-area model by Pearson (1974) to
simulate the land-sea breeze.  Bel and and Warn (1975) have generalized
Pearson's approach to the study of transient Rossby waves  by  direct  appli-
cation of the Laplace transform.  Orlanski (1976)  has discussed  the  problem
of open boundary conditions  and has proposed a computational  form  of the
radiation condition for specifying the boundary  values of  model  variables
during numerical integration.  In the numerical  simulations of  orographic
waves (Clark, 1977; Clark and Peltier, 1977; Klemp and Lilly, 1978).and
convective clouds (Klemp and Wilhelmson, 1978a;  Clark, 1979), the  success
of the radiation condition on the lateral boundaries  is  apparent.  Various
numerical approximations to  the Sommerfeld radiation  condition  have  been
examined by Miller and Thorpe (1981), and improvements to  Orlanski's formu-
lation have been discussed.  Raymond and Kuo (1981) recently  have  extended
the application of the radiation condition to multidimensional  flows.  In
their model which simulates  a cold front, Ross and Orlanski (1982) have
applied the same philosophy  as that of Orlanski  (1976),  but have extrapo-
lated the derivatives of horizontal velocity (i.e., vorticity and  diver-
gence) rather than the horizontal velocity itself.  By using  this  approach,
they claim, the distortions  of the field variables at the  boundary have
been reduced.  It has been demonstrated that the radiation boundary  con-
dition is superior to the sponge-type boundary condition at the  lateral
boundaries (Miyakoda and Rosati, 1977).  For the upper boundary  of numeri-
cal models, Klemp and Durran (1982) have proposed  a radiation condition to
permit gravity waves to radiate out of the domain.

3.4  Bounded derivative scheme

     As discussed in the initialization of a limited-area  model, the
bounded derivative scheme can also be applied to give proper  constraints on
the boundary conditions. 'The theory of boundary conditions for  the  open
boundary problem for symmetric hyperbolic systems  is  presented  by  Kreiss
(1970).  If a set of well-posed boundary conditions for  such  a  system is of
the right form, the bounded  derivative scheme can  be  used  to  prove the ex-

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istence of smooth solutions and an  initialization  procedure  to obtain these
solutions can be derived.  For a system of  shallow-water  equations,  Brown-
ing and Kreiss (1982) successfully  demonstrated  the  smooth  solutions with
open boundary.

3.5  Summary

     The sponge scheme is simple and can be easily implemented to  limited-
area models, but noise may still appear at  the boundary.  Also,  at least
one empirical coefficient in each variation of the scheme must be  arbitrar-
ily chosen beforehand.  The coefficient may be determined by a trial-and-
error procedure.  Because of its simplicity,  the sponge scheme should be
utilized with the model-governing equations.  After  the basic numerical
model and its physics are well-developed, the radiation boundary  scheme
should be implemented to allow the  free movement of  the regional-scale
disturbances across boundaries.  The bounded  derivative scheme is  still
being developed for the limited-area primitive equation model.  Upon its
successful  development, the application of  the bounded derivative  scheme is
desirable because this scheme considers the model  equations,  initial  condi-
tions, and boundary conditions consistently.
4.  SURFACE EFFECTS

4.1  Introduction

     The only physical boundary in a  limited-area  model  is  the  lower bound-
ary, the earth's surface.  While the  velocity  vanishes  at  the rigid sur-
face, the temperature and moisture there vary.  The  heat and moisture
transfers through the surface are affected  by  not  only  the  variations in
the underlying layers, but also by the  conditions  immediately above the
surface.  The temperature and moisture  over water  or ice surfaces  usually
have quite limited changes, and may be  treated as  steady-state  for most
regional-scale phenomena.  Over land  surfaces,  the diurnal  variations of
the surface temperature and moisture  are quite important on the regional
scale, and should be computed by energy and moisture budget equations.
Therefore, it is necessary to include all influential  physical  processes on
or near the surfaces in these budget  equations, to represent them  realisti-
cally, and to calculate the surface temperature and  moisture accurately.
Parameterizations in the energy and moisture budgets will  be considered
separately.

4.2  Surface energy budget

     A uniform description of the diurnal variation  of  temperature on the
ground surface by a pre-specified heating function (Estoque, 1961, 1962;
Magata, 1965; McPherson, 1970; Neumann  and  Mahrer, 1971, 1974,  1975; Pear-
son, 1973; Pielke, 1974; Mahrer and Pielke, 1976;  Tapp  and  White,  1976;
Estoque et al., 1976; etc.) is adequate only  for a dry  surface.  In par-
ticular, such a function cannot correctly represent  the  variation  during
rainfall because the occurrence of precipitation is  not  periodic and is
spatially intermittent.  A sophisticated method to compute  the  diurnal
variation of temperature is necessary in this  case.

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     The nonlinear energy-balance equation, which  includes  the  energy  flux-
es across the ground surface, gives more accurate  estimations of  the diur-
nal temperature variation on the ground surface.   The  iterative procedure
to solve the energy-balance equation becomes time-consuming  (Myrup,  1969;
Outcalt, 1972; Jacobs and Brown, 1973; Mahrer  and  Pielke,  1977).

     Depending on the forcing by the sum of the atmospheric  energy  fluxes,
a rate equation for the ground surface temperature has  been  developed  inde-
pendently by Arakawa (1972) and Corby et al. (1972)  in  their studies of the
general circulation.  Bhumralkar (1975) has pointed  out that this rate
equation actually calculates the bulk temperature  of the soil layer of fin-
ite depth and does not explicitly calculate the ground  surface  temperature,
and he has derived a new prognostic equation for the ground  surface temper-
ature.  His prognostic equation is similar  to  those  of  Blackadar  (1976,
1979) and Deardorff (1978).

     The atmospheric energy fluxes included in the energy-budget  equation
are the radiation fluxes, subgrid heat fluxes, soil  heat flux,  and  preci-
pitation cooling flux.  The radiation fluxes may be  further  divided into
(1) the net short-wave radiation flux which depends  on  the  solar  constant,
the zenith angle, the surface and cloud albedo, and  the atmospheric absorp-
tions; and (2) the net long-wave radiation  flux which  is a  function of sur-
face temperature, ground emissivity, cloud  coverage,  infrared emissions,
and others for both the outgoing and atmospheric-counter radiations.   A de-
tailed review on the treatment of the radiation fluxes  for  mesoscale model-
ing can be found in Pielke (1981).  Further simplifications  have  appeared
in Anthes and Warner (1978a) and Hsu (1979).   The  subgrid fluxes  consist of
the sensible and evaporative heat fluxes.  The soil  heat flux may be ex-
pressed in terms of the tendency of the surface temperature. Thus,  the
energy budget equation may take the form of a  prognostic equation of the
surface temperature (Deardorff, 1978).  Otherwise, the  time-consuming  iter-
ative procedure would be applied to an algebraic nonlinear  energy-balance
equation to obtain the surface temperature.  The precipitation  cooling ef-
fect is usually ignored.  In fact, it can drastically  change the  diurnal
variation of the surface temperature and moisture  under precipitation
events.  Hsu (1979) has demonstrated this in a rain-generating  sea-breeze
study over the Florida Peninsula.

4.3  Surface moisture budget

     In regional-scale models, the wetness  of  the  land  surface  is either
ignored or considered to be constant (Mahrer and Pielke, 1977).  In general
circulation models (Manabe, 1969; Washington and Williamson, 1977),  the
tendency of the moisture content over the land surface  is determined by the
difference of the precipitation and the evaporation.  A more sophisticated
method has been formulated by Deardorff (1978).  In  a mesoscale model, Hsu
(1979) has utilized a surface moisture budget  equation  to predict the  sur-
face moisture content over land.  The importance of  the surface wetness in
influencing the surface energy budget has been shown by McCumber  and Pielke
(1981) in their results from a series of one-dimensional  simulations.
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4,4  Summary

     In summary, the lower boundary conditions  of  a  regional-scale model
must be specified.  Besides setting velocity  to  be zero  at  the  surface,
temperature and moisture can be computed  from the  energy and moisture
budget equations.  Eventually, a complex  and  almost  complete treatment of
the surface effects, such as the parameter!"zations of  Dickinson  et al.
(1981) for the global climatic model, should  be  adopted  for regional-scale
models.
5.  PLANETARY BOUNDARY LAYER EFFECTS

5.1  Introduction

     All transfers of momentum, heat, moisture, and  other  atmospheric con-
stituents into the atmosphere  from the  surface  of  the  earth  must take place
through the planetary boundary layer (PBL).  Not only  the  supply of energy,
but also the dissipation of kinetic energy,  as  well  as the vertical trans-
ports of momentum, heat, moisture, and  other constituents  have  to be consi-
dered in the dynamical interaction between the  atmosphere  and the underly-
ing surface.  This interaction can be considered to  occur  in two stages:
first, via the fluxes carried  by small-scale turbulence from the earth to
the PBL, and next, through the transfer from the PBL to the  free atmo-
sphere.

     One of the most  important properties of the PBL is that its flow is
turbulent, not laminar.  A turbulent flow consists of  eddies with different
scales; if the size of the eddy is several times greater than the grid size
of a numerical  model, the eddy is resolvable.   This  is rarely the case in
models of practical interest,  however.  The  contribution of  unresolvable
eddies must be represented by  parameterizations, and in practice these
parameter!'zations thus represent virtually all  the turbulence.   An intro-
duction to these parameterization has been given by  McBean et al. (1979).

     Another important feature of the PBL over  land  is the strong modula-
tion of its structure by the diurnal cycle.  Acting  through  the surface
energy budget,  which  controls  the heat  transfer between the  surface and the
boundary-layer air, this typically causes (in fair weather)  a convective
state and boundary-layer deepening during the day, followed  by  decay of the
large convective eddies near sunset and the  slow evolution of a stably-
stratified PBL at night.  The  classical "neutral"  PBL  is in  fact quite
elusive; very small surface heat fluxes can  drive  the  PBL  into  convection
or into stable stratification  (McBean et al., 1979).

     The nature of PBL turbulence in the convective  and stably-stratified
states is quite different.  Wyngaard (1982b) has discussed these differ-
ences in detail; we will summarize them here.   The convective PBL, and its
largest convective eddies, are limited  in depth by the presence of an over-
lying inversion at some height which typically  ranges  from a few hundred
meters to a few kilometers.  As the day progresses,  the convective PBL
typically deepens by  entraining this stable  capping  layer; the  ultimate
growth rate (simply the imbalance between the entrainment velocity and the

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mean vertical velocity) typically  ranges  from  0  to  a  few  centimeters per
second, and in unusual circumstances can  be  as large  as a  few  tens  of cen-
timeters per second.  The turbulence structure in the convective  PBL has
simple scaling (Caughey, 1982), although  entrainment  effects at the top  can
cause complications (Wyngaard, 1982b).

     The stably-stratified PBL tends to be  relatively less steady,  much
thinner, and more sensitive to changes in its  boundary conditions than the
convective PBL.  Physically realistic but relatively  more  complicated par-
ameterizations for its structure and dynamics  now exist (Wyngaard,  19825).

     The role of the PBL transfers  in general  circulation  and  climate dy-
namics is well known.  Many large-scale general  circulation models  have  im-
plemented parameterizations to simulate the  effects of the PBL (Chang,
1977; Bhumralkar, 1976).  Because  of the  diversity  of the  empirical  for-
mulas used, a sensitivity test to  find the  best  one in a  given application
is recommended.  Arya (1977) has suggested  some  improvements to certain  PBL
parameterizations for general circulation models based on  recent  experi-
mental and theoretical studies.

     The importance of the PBL in  producing  vertical  fluxes of momentum,
heat, moisture, and other atmospheric constituents  on the  regional  scale
has been gradually revealed.  In his review, Pielke  (1981) has identified
some regional-scale phenomena, such as sea-land  breezes, mountain-valley
winds, lake-effect storms, and urban circulations,  to have direct associa-
tion with the development and decay of the  PBL.  It is also found that the
PBL can affect the circulations of  a tropical  cyclone (Anthes  and Chang,
1978), a squall line (Sun and Ogura, 1979),  winter  storms  (Anthes and
Keyser, 1979; Bosart, 1981), and frontogenesis (Keyser and Anthes,  1982).
Therefore, the parameterization of  the PBL  is  an important aspect of re-
gional-scale models, and the transfer by  fluxes  in  this layer  must be
represented with considerable fidelity.

     There are two broad appproaches to parameterizing the PBL for a numer-
ical model, depending on the vertical resolution.  One is  the  single-layer
approach for low resolution, and the other  is  the multi-layer  approach for
high resolution.

5.2  Single-layer approach

     In its simplest form, this approach  is  usually applied at the first
interior model level which is well  above  or  coincides with the top  of the
PBL.  The actual PBL structure is  not resolved.  The  turbulent fluxes of
momentum, heat, moisture, and other constituents are  determined diagnos-
tically from bulk transfer formulas.  Various  empirical values and formulas
are used for the transfer coefficients (Deardorff,  1968,  1972;  Bhumralkar,
1976; Arya, 1977).  An empirical determination of the similarity  functions
of geostrophic drag and heat transfer has been put  forth  by Zilitinkevich
and Chalikov (1968) and Clarke (1970).  Arya (1977) later  included a simi-
larity function of moisture transfer.  Again,  the forms of the similarity
functions vary widely (Arya, 1977)  because  the relationships are  deduced
from different assumptions and observational data.
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     All parameter!'zations of this type rely heavily on what  has  been
learned about the "surface layer" over the past thirty years.   By  surface
layer we mean roughly the lowest IQ% of the PBL.  This is  the  region of
Monin-Obukhov (M-0) similarity.

     By the M-0 similarity hypothesis, surface-layer structure  is  deter-
mined solely by the parameters g/T, ts/p, ews, and z:  that is, by the
buoyancy parameter, the kinematic surface stress, the surface  temperature
flux, and distance above the surface.  These detennine a velocity  scale,
u*= /Tc/p; two length scales, z and L = -u*3/(k gew^/T), where  k  is the
Karman s constant; and a temperature scale, T* = ews/u*.   An  alternative
statement of the M-0 similarity hypothesis is that surface-layer  proper-
ties, when non-dimensionalized with u*, z, and T*, are universal  functions
of z/L.

     M-0 scaling is now used routinely in experimental and theoretical
work, and in the surface-layer parameter!zations of numerical  modeling.
It has brought a good deal of order to surface-layer meteorology.   By  using
it, one is able to generate systematic and rational parameterizations  for
surface transfer in regional-air-quality applications, for example.

      A somewhat more formal single-layer approach is to use  a  "mixed-
layer" or "slab" model for the PBL by integrating the mean conservation
equations across its depth.  In this approach, one assumes simple  but  real-
istic forms for the mean profiles before performing the integration.   Zeman
(1979), for example, has developed such a single-layer model  for  the stable
PBL and shown that it simulates well its evolution.  Lavoie (1972) has  de-
veloped a mixed-layer model, and a similar approach has been  used by Anthes
and Warner (1978a) in their mesoscale model.

     An elegant variation on this approach has been developed by  Lamb
(1982) to investigate photochemical air pollution on the regional  scale.
The model consists of three dynamic layers.  They are the  surface  layer,
the mixed layer, and the tropospheric layer immediately above  the  mixed
layer.  The thickness of all layers varies spatially and temporally, which
complicates the governing equations.  Apparently, under synoptically undis-
turbed conditions, such as stagnant high pressure conditions,  the  heights
of those layers are well-defined and the model will perform as  it should.
However, when the PBL interacts with synoptic disturbances, such  as cy-
clones, fronts, and organized thunderstorms, the dynamic interactions  may
become so complex that a single-layer approach to either the  mixed layer  or
the tropospheric layer may not be sufficient to resolve this  complicated
situation realistically.  Further research in developing this  "dynamic-
layer" model should be geared toward more general synoptic conditions.

     A single-layer PBL parameterization based on a generalized similarity
theory was tested by Chang (1981) in a tropical cyclone model,  and was
judged superior to drag coefficient parameterization in his comparison
study.  In a study of PBL parameterizations, Anthes et al. (1980)  found
that the single-layer approach can obtain the average structure of the  PBL
under horizontally homogeneous conditions.  When horizontal inhomogeneities
associated with differential heating over complex terrain  and across a
land-water boundary were introduced, the single-layer approach  became  less

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accurate compared to the multi-layer approach.  Nevertheless,  the  single-
layer approach has merits and is highly recommended during  the early  devel-
opment of a multi-layer regional-scale numerical model.

5.3  Multi-layer approach

     If one can afford the higher computational expense  of  having  several
model layers within the PBL, it can be advantageous to let  the model  com-
pute its own PBL structure.  One needs turbulence closures  in  order  to
accomplish this.  We will discuss a few types.

a.  First-order closure

     Here the turbulent flux of a variable  is expressed  in  terms of  the
variable's gradient and the eddy exchange coefficient  (K) as an analogy to
the molecular viscosity (or diffusivity) utilized by the kinetic theory of
gases.  There are two main approaches to the specification  of  K.   Specify-
ing the dependence of K on a local stability parameter,  such as the  Rich-
ardson number, is one approach.  Various formulas have been summarized  by
Bhumralkar (1976) and Blackadar (1979) and  have been applied to mesoscale
situations by McNider and Pielke (1981), Ross and Orlanski  (1982), and
Zhang and Anthes (1982) and to cloud-scale  situations  by Cotton and  Tripoli
(1978) and Clark (1979).

     The second approach is to employ a function to describe the vertical
distribution of the eddy exchange coefficient.  A linearly-decreasing func-
tion has been suggested by Estoque (1963),  while McPherson  (1970)  and Agee
et al. (1973) have proposed exponential-decay functions.  O'Brien  (1970)
has provided another alternative in which a Hermite polynomial is  specified
for the vertical distribution of the eddy exchange coefficient.  Busch  et
al. (1976) have developed a prognostic equation to calculate the mixing
length which gives the vertical eddy exchange coefficient in the PBL.  From
their calculations, it has been found that  the K specifications of O'Brien
(1970), Agee et al. (1973) and Busch et al. (1976) are very much alike  in
their performance.

     The numerical results of the second-order turbulence model of Brost
and Wyngaard (1978) for the stable PBL has  given K profiles similar  in
shape to O'Brien's polynomials.  For the convective PBL, the distribution
of the K obtained from the three-dimensional, time-dependent numerical  mod-
eling of turbulence, i.e., large-eddy simulation (Wyngaard, 1982b),  is  also
qualitatively similar to O'Brien's polynomial.  However, the scaling in
these three cases is quite different and it is now evident  that the  O'Brien
profile as originally proposed does not have the correct scaling for either
the stable or unstable PBL (Wyngaard, 1982b).

     The height of the PBL is sometimes a necessary parameter  in specifying
the vertical distribution for K.  For the neutral PBL, Blackadar and Tenne-
kes (1968) have suggested an algebraic relationship between the PBL  height
and the ratio of the frictional velocity and Coriolis  parameter.   For un-
stable conditions, Deardorff (1972, 1974) has derived  prognostic equations
to predict the PBL height.  For the stable  ?8L, diagnostic  relations for
the PBL height have been proposed by Monin  (1970), Clarke (1970),  Deardorff

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(1972), Businger and Arya (1974), Zilitinkevich (1975), Brost and Wyngaard
(1978), and others, while prognostic equations to predict the PBL height
have been developed by Zilitinkevich and Monin (1974), Smeda (1979), Zeman
(1979), Yarnada (1979a), and others.  A comparison of different  schemes  to
determine the height of the stable PBL has been made by Yu  (1977).  He  con-
cluded that the diagnostic formulations give better agreement with  observa-
tions.  However, the equations formulated by Brost and Wyngaard  (1978),
Smeda (1979), Zeman (1979), and Yamada (1979a) were not included in Yu's
study.  Recently, Nieuwstadt and Tennekes (1981) have derived a  rate equa-
tion for the height of the stable PBL, and have shown that  its  performance
is superior to that of diagnostic formulas.

     With the multi-layer approach, the layer immediately above  the surface
is treated differently.  The representation of turbulence in this "surface
sublayer" is usually either a bulk transfer formula which has been  pre-
viously described in the single-layer approach, or an empirical  function
based on the Monin-Obukhov similarity theory.

b.  Higher-order closure

     This provides the opportunity to resolve the turbulent structure of
the entire PBL.  However, not only its high computational cost  but  also its
lack of dramatic improvement over the first-order closure scheme (Wyngaard,
1982a) have discouraged further implementation of the higher-order  closure
schemes into the limited-area models.  In a three-dimensional model of
thermal convection in the atmosphere (Schemm and Lipps, 1976),  the  second-
order closure of Mellor and Yamada (1974) has been used to  parameterize the
subgrid turbulence.  Except for the turbulence kinetic energy and the tem-
perature variance which are computed by two predictive equations, all other
second-order moments are treated algebraically.

     In a global general circulation study, Miyakoda and Sirutis (1977)
have also simplified the original second-order closure scheme of Mellor and
Yamada (1974), but have only retained the prognostic equation of the turbu-
lent kinetic energy.  Then K-closure is used, with K formulated  to  be a
function of the turbulent kinetic energy, mixing length, vertical thermal
stability, and vertical wind shear.  They have claimed that this mixed
scheme has shown considerable improvement over their previous PBL param-
eterizations which used simpler functional forms for K.  A  similar  but  sim-
plified procedure is used in the cloud-scale model of Klemp and  Wilhelmson
(1978a).

     In addition to using a prognostic equation for the mixing  length,
Yamada (1979b, 1981, 1982) used a procedure similar to that of  Miyakoda and
Sirutis (1977) in his PBL model.  The results compared with observations  in
general were satisfactory.  Yamada (1977) has also applied  the  same mixed
scheme to the covariance of the pollutant concentration and the  vertical
velocity, and has shown at least qualitatively realistic results.

     To include PBL transfers in a limited-area model realistically and
adequately is not a trivial task.  A number of parameter!'zations ranging
from the simplest drag coefficient scheme to higher-order closure are
available.  However, the effects of PBL transfers in regional-scale

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phenomena are yet to be studied comprehensively by using  various  degrees  of
sophistication in PBL parameterizations.

5.4  Summary

     In summary, first-order closure is the most popular  with  limited-area
numerical modelers for representing the PBL transfers.  The PBL  parameter-
izations in the models of Louis (1979), Phillips (1979),  Ross  and Orlanski
(1982), and Zhang and Anthes (1982) are examples where K  is specified  as  a
function of the local Richardson number, while the vertical profiles of
O'Brien (1970) for the eddy exchange coefficient have been adopted by-
Pielke and Mahrer (1975), Perkey (1976), Nickerson (1979), Hsu  (1979),
Ballantine (1980), Boudra (1981), and others.  None  of these approaches is
completely consistent with our current understanding of the structure  and
physics of the PBL, however (Wyngaard, 1982b).  Second-order closure might
seem more sophisticated, but in fact has the same difficulty,  although  at
one level higher, and is much more expensive.  A prudent  approach for  re-
gional-scale air quality model applications is to use a K-closure updated
to incorporate recent advances in understanding of PBL scaling  (Wyngaard,
1982b).
6.  CLOUDS AND PRECIPITATION"

6.1  Introduction

     In many regional phenomena, phase changes  of water  occur  as  cloud-
scale circulations lift air above the condensation  level  and as precipita-
tion falls back out of clouds and begins  to evaporate.   It  is  necessary  to
include the formation and dissipation of  clouds  as  well  as  the release of
latent heat in a dynamical model.  Not only does the  precipitation  gener-
ated by clouds have direct impact on the  validity of  the prediction,  but
also the clouds themselves influence radiation  processes in the atmosphere
by reflecting short-wave radiation and absorbing and  emitting  long-wave
radiation.  The need to establish an accurate,  effective, and  inexpensive
method to calculate the effects of clouds and precipitation for a region-
al-scale model is obvious.

     The production of clouds and precipitation  and the  release of  latent
energy on the regional scale can occur by either of two  types  of  processes:
those that occur under grid-resolvable conditions and those that  occur un-
der subgrid-scale conditions.  The former are usually generated in  a  rela-
tively large area where the removal of precipitation  directly  depends on
the grid-resolvable dynamics in a thermodynamically stable  atmosphere.   On
the other hand, the latter are formed by  convective clouds  in  an  absolutely
or conditionally unstable atmosphere.  Thus, they will be discussed separ-
ately.

6.2  Grid-resolvable clouds and precipitation

     Grid-resolvable clouds and precipitation occur mainly  in  the regions
of dynamic ascent of moist and stable air.  The  latent heat release from
this stable precipitation has been computed by  Krishnamurti and Moxim

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(1971) and Krishnamurti et al. (1973).  A general formulation can  be  found
in Haltiner and Williams (1980).  In such schemes, the precipitation  is
induced by an upward vertical motion whenever the relative  humidity exceeds
a critical value less than 100 percent.  The sophistication of the calcula-
tions for grid-resolvable clouds and precipitation gradually increases as
computer capacity expands.  While Colton (1976) introduced  the continuity
equations for liquid water in his model to simulate stable  precipitation, a
similar approach by Sundqvist (1978) predicted cloud water  content as well
as cloud coverage under nonconvective conditions.  Furthermore, coupled
continuity equations for cloud droplets and raindrops have  been used  by
Perkey (1976), Kreitzberg and Perkey (1977), and Ross and Qrlanski (1982).
For a model to be general  enough to be used to simulate or  predict most
regional-scale meteorological systems, a simple procedure for representing
nonconvective clouds and precipitation is necessary.  Adaptation of a vari-
ation of the general formulations of Haltiner and Williams  (1980)  is  an
appropriate first step.  In the meantime, new developments  or adaptations
of explicit calculations of liquid water content could be tested.

6.3  Subgrid-scale clouds and precipitation

     Convective precipitation is produced by subgrid-scale  clouds.  The
scale of a convective cloud (on the order of 10 km or less  horizontally)  is
much IBSS than that of regional-scale disturbances (on the  order-of 100  km
or greater).  Scale analysis shows that the motion of convective clouds  is
nonhydrostatic, while that of regional-scale disturbances is hydrostatic.
It is impractical to calculate the motions of two different scales expli-
citly in one model; thus, the processes generating convective clouds  and
precipitation in a regional-scale model must be parameterized.

     The importance of convective cloud systems in modifying regional-scale
circulations has been recognized both observationally (Ninomiya, 1971; Mad-
dox et al., 1981; Fritsch and Maddox, 1981a) and numerically (Chang et al.,
1982; Anthes et al., 1982a; Anthes et al., 1982b).  Although it has been
demonstrated conclusively that latent heat release and its  vertical distri-
bution can influence significantly the evolution of the regional-scale sys-
tem, accurate parameterization of the effects of convective clouds has not
been achieved.  As discussed by Anthes et al.  (1982c), cumulus convection
affects the environment through diabatic heating and cooling associated
with condensation, evaporation, melting, freezing, deposition, and sublima-
tion; through vertical fluxes of sensible heat, moisture, and momentum;  and
through pressure perturbations.  The processes are highly nonlinear and  de-
pend in complex ways upon the size spectrum of clouds and on the environ-
mental flow.

     Major schemes to parameterize convective clouds and precipitation are
summarized as follows:

a.  Moist convective adjustment scheme

     This scheme was developed originally by Manabe and Strickler  (1964),
and was designed mainly to remove the conditional instability  in the  moist
atmosphere instantaneously while the vertical integral of the total static
energy is invariant.  It was applied in a general circulation model by

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Manabe et al. (1965) and Manabe et al.  (1970),  and  in  a  hurricane  model  by
Kurihara (1973) and Kurihara and Tuleya  (1974).  Even  though  the scheme  is
very simple and is successful in simulating many of  the  gross  features  of
the tropics, it bypasses the real physical processes through  which the  con-
vective clouds interact with their environment.

     More recently, Kreitzberg and Perkey  (1976, 1977) used the cloud  par-
ameters computed from a Lagrangian sequential plume  model  to  adjust region-
al-scale temperature -and moisture profiles.  Apparently,  this  scheme of  the
mutual interaction between cloud scale  and regional  scale  eliminates the
oversimplification of the previous adjustment scheme.

b.  Moisture convergence scheme

     Based on the concept of conditional  instability of  the second kind
(CISK) (Ooyama, 1964; Charney and Eliassen, 1964; Ogura,  1964), the dia-
batic heating rate of convective clouds  is made proportional  to the pumping
of moisture caused by the frictional  convergence in  the  planetary  boundary
layer.  A significant advance is set  forth by Kuo  (1965),  who set  the  con-
vective heating proportional to the total moisture  convergence in  a column
of atmosphere and provided a scheme for determining  its  vertical distribu-
tion.  Later, Kuo (1974) clarified that the compensating  sinking outside
the cloud is automatically taken care of in his parameterization,  and  modi-
fied his scheme to partition part of  the moisture convergence  to moisten
the air column while the rest of moisture  convergence  is  used in heating.
Anthes (1977) combined a one-dimensional  steady-state  cloud model  and  Kuo's
scheme.  The cloud model is forced by the  regional  model,  and provides  the
essential cloud parameters for the parameterization  of convective  clouds.
Different variations of the moisture  convergence scheme  have  been  applied
to large-scale circulation models (e.g., Krishnamurti  et  al.,  1973), hurri-
cane models (a list of models is found  in Anthes, 198E),  and  regional-scale
models (Anthes and Warner, 1978a; Hsu,  1979; Phillips, 1979).  Further re-
finements are needed to include more  explicit cumulus  dynamics.

c.  Convective equilibrium scheme

     Under the assumption of the quasi-equilibrium  between the generation
of conditional instability by the large-scale dynamical  processes  and  its
destruction by convective clouds, Arakawa  and Schubert (1974)  developed  a
cumulus parameterization which contains a  spectral  cloud-ensemble  model  and
a relation between the statistical properties of cumulus  ensemble  and  the
large-scale variables.  Lord and Arakawa (1980) show some  observational
evidence of the cloud-work-function quasi-equilibrium  for  large-scale
fields in the tropics and subtropics.  This scheme  has been used in a  gen-
eral circulation model (Lord et al.,  1982) and  a limited-area model (McGre-
gor et al., 1978).  Although the Arakawa-Schubert scheme  is one of the  most
complex cumulus parameterization schemes,  some  discrepancies  in the verti-
cal structure between parameterization  and observation appear in Lord
(1982).  The validity of various assumptions which  have  been  made  concern-
ing the control and feedback processes  between  the  cumulus clouds  and  the
large-scale circulations should be verified by  observations.
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d.  Buoyancy energy scheme

     Fritsch and Chappell (1980a) have proposed  that  the  buoyancy  energy
available to a parcel, in combination with a prescribed period  of  time for
the convection to remove that energy, can be used  to  regulate the  amount of
convection in a regional-scale numerical-model grid element.  Each grid
area consists of areas of updrafts, downdrafts,  and environment.   Not only
is the effect of convective clouds considered explicitly,  but also the
buoyancy energy can be generated and stored prior  to  the  onset  of  deep
convection.  Precipitation efficiency of convection is specified in terms
of the vertical wind shear, which is a very important factor  in controlling
midlatitude convective activities.  The scheme has been applied and tested
by Fritsch and Chappell (1980b) and Fritsch and  Maddox (1981b)  for simulat-
ing the development of convectively driven mesoscale  pressure systems, and
the results are encouraging.

e.  Explicit scheme

     This scheme is different from other schemes previously  described.  The
release of latent heat due to convective clouds  is explicitly expressed in
terms of the resolvable-scale motions and the parameterized  cloud  micro-
physics, following Kessler (1969).  The advantages of this approach are (1)
that far fewer assumptions are needed to determine-the -vertical distribu-
tion of heating, (2) that the threshold for heating is the natural  condi-
tion of saturation at a grid point, and (3) that downdrafts  are explicitly
calculated.  The only disadvantage is that the convective  clouds in the
subgrid scale will not be resolved.  Such a disadvantage  may  be overcome by
reducing the model grid size to a reasonable limit.   Yamasaki (1977), Ro-
senthal (1978), and Jones (1980) have used the explicit scheme  in  their
hurricane models, and realistic hurricane simulations can  be  obtained in a
convectively unstable atmosphere.

6.4  Summary

     In all parameterization schemes except those  of  Anthes  (1977) and
Fritsch and Chappell (1980a), the momentum flux  due to cumulus  convection
has not been treated.  The parameterization of momentum exchange by cumulus
convection is discussed by Schneider and Lindzen (1976),  and  is applied to
tropical waves by Stevens et al. (1977).  The role of momentum  flux in the
interaction between cumulus convection and its environment has  been exa-
mined by Stevens (1979) for tropical wave disturbances.   For  the midlati-
tude systems, further study will advance our knowledge about  the momentum
exchange between convective clouds and their environment  and  clarify its
importance.

     For all the schemes that parameterize the effects of  convective clouds
on the larger scale, with the exception of the explicit scheme, the goal is
to determine the vertical distributions of heat  and moisture  for the larger
scale.  It has not been demonstrated that any scheme  is sufficiently gen-
eral and reliable to significantly improve regional-scale  prediction in the
midlatitudes.  Analyzing real data as well as the  model output  from simu-
lations of real events will help us to understand  more about  the mutual
interactions between convective clouds and regional-scale  disturbances.

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The ideal method is to set up a three-dimensional  system  nesting  a cloud-
scale model within a regional-scale model, with  two-way interactions  be-
tween the scales; this is further discussed  in Section 4.7  of  Chapter VI.
Before any conclusive result can be obtained  from  the nesting  system,  one
must parameterize the convective clouds and  precipitation and  adapt the
existing techniques.  The moisture convergence scheme is  a  natural  first
step because of its relative simplicity,  and  the buoyancy energy  scheme can
also be applied since it has quite general considerations for  the midlati-
tudes.  It is possible that the explicit  scheme  for  computing  clouds  and
precipitation directly will be necessary.

     The contributions of deep convective clouds to  the large-scale heat,
moisture, and momentum sources and sinks  have been reviewed.   Shallow con-
vective clouds may play a less significant role  in directly controlling re-
gional-scale dynamics, but may affect  the radiative  processes  in  the  atmo-
sphere.  The shallow-cloud effects in  the general  circulation  model  have
been treated statistically by Slingo  (1980)  with some success.  Further
understanding of shallow convective clouds may be  achieved  by  using less
sophisticated parametric models (e.g., Lilly, 1968;  Schubert,  1976;  Schu-
bert et al., 1979a,b; Albrecht et al., 1979; Albrecht, 1979).
7.  NUMERICAL METHODS

     The foundation of a dynamical model  is  a  set  of  conservation  laws.
These laws form a system of coupled partial  differential  equations which
must be satisfied simultaneously  and which  include sources  and sinks.   The
system is highly nonlinear, and analytical  solutions  for  general conditions
are impossible to obtain.  Thus,  these  partial  differential  equations  must
be approxiated by algebraic equations which  can  be solved on a computer.
These numerical solutions have to be stable  and  accurate.   In general,
there are three primary methods to approximate  differential  equations:

     (1)  finite-difference method, in  which truncated Taylor series
          are used (Richtmyer and Morton,  1967);

     (2)  spectral/pseudo-spectral method,  in  which truncated globally
          continuous base functions are utilized,  e.g., Fourier series,
          Legendre polynomials, Bessel  functions,  etc.  (Gottlieb and
          Orszag, 1977); and

     (3)  finite-element method,  in which  truncated locally  continuous
          base functions are applied, e.g.,  Chapeau functions, Hermite
          cubic functions, cubic  spline functions,  etc. (Strang and Fix,
          1973).

Among these, the finite-element method  allows  the  greatest  flexibility  in
arranging grid points in the computational  domain,  but  it has difficulty
evaluating the source and sink terms on a  prearranged uneven grid  net.   Un-
less this difficulty is overcome, the practical  application  of the finite-
element method to a complex, regional-scale  model  will  not  be feasible.
The spectral/pseudo-spectral method has been shown to be  extremely accurate
and to eliminate the fictitious nonlinear  aliasing.  However, the  require-

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ment of periodicity makes the method impossible to be applied to open-
boundary limited-area models in simulating real events.  The finite-dif-
ference method becomes the only alternative at the present time.  A combi-
nation of the finite-element and finite-difference methods has been tested
by Mahrer and Pielke (1978), and the results were encouraging.

     Kreiss and Oliger (1973), Mesinger and Arakawa (1976), Haltiner and
Williams (1980), and Pielke (1981) give rather extensive reviews of the
finite-difference methods used by meteorological models.  Additional refer-
ences are given in Section 2 of Chapter III.  For the limited-area models,
two kinds of grid systems—staggered and unstaggered—appear in the litera-
ture.  Under linear computational constraints, the time step of the stag-
gered grid is shorter than that of the unstaggered one.  However, the un-
staggered system is less accurate than the staggered one in terms of trun-
cation error.  Certain staggered systems not only can lead to considerable
reduction of the solution separation due to the leap-frog differencing on
an unstaggered system, but also can provide conserving finite-difference
form.  Usually mass, momentum, and total energy are invariants.  Various
staggered grid nets have been discussed by Arakawa and Lamb (1977).  Some
regional-scale models have staggered their grids three-dimensionally (e.g.,
Anthes and Warner, 1978a; Ross and Orlanski, 1982).  Recently, Arakawa and
Lamb (1981) suggested an energy-and-potential-enstrophy-conserving scheme
which improves the" circulation over steep topography.  Before-the energy-
and-potential-enstrophy-conserving scheme is adapted for a regional-scale
model, the energy-conserving scheme should be used and tested first.  A
fourth-order finite-difference technique for the spatial derivatives could
be introduced to reduce the phase-speed error of the common second-order
technique.
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                                CHAPTER FIVE

            THE CHEMISTRY OF ACID GENERATION  IN THE  TROPOSPHERE
1.  GAS PHASE REACTIONS

1.1  Introduction

     Sulfuric acid (HoSO^) and nitric acid  (HN03),  the  major  acids  respon-
sible for "acid rain,  are formed  in the  atmosphere from  the  oxidation of
sulfur dioxide (S02) and the oxides of nitrogen  (NO,  N02),  respectively,
through a variety of chemical reaction pathways.  These transformations may
occur in the gas phase, in the solution phase  of  aerosols,  cloud water or
rain water, or on the surface of solid aerosols  such  as graphitic parti-
cles.  In this section, we will review and  evaluate the literature  related
to the various gas phase mechanisms which result  in-acid  generation in the
troposphere.  In Section 2, the solution  phase and  heterogeneous processes
will be reviewed.  In Section 3, the important photochemical  processes
which drive many of the S0£ and NOx oxidation  mechanisms  will  be dis-
cussed.  Much of the chemistry involved in  acid  rain  development is rea-
sonably well understood today, although some possible reaction pathways
still remain somewhat ill-defined.  From  the following  discussions, it will
become clear that the quantitative treatment of  the chemistry  of acid rain
generation is non-trivial, yet the inclusion of  many  of the alternative
pathways for S02 and N0/N02 oxidation is  a  prerequisite to  the development
of a reliable regional-scale model of acid  deposition.

     In many of the long-range transport  models  which have  been developed
in recent years, the developers have assumed a fixed  linear transformation
rate for S02, and no actual chemical reactions were employed  (Niemann et
al., 1979; Bhumralkar et al., 1980; Fay and Rosenzweig, 1980;  Niemann et
al., 1980; Patterson et al., 1981; Shannon, 1980; Venkatram et al., 1982).
Such linear models by their very nature must lead to  a  proportional de-
crease in the acid generation and  deposition with the extent  of cutback in
S02 emissions.  The results from these models  may not describe well the
happenings in the nonlinear real world, especially  on a single-event basis,
and they are of uncertain value in planning acid  rain control  strategy.  It
may well be that a near-linear relationship between the magnitude of NOX
(NO plus N02) and S02 emissions and HN03  and H2SOI+  generation  and depo-
sition exists, particularly for averages  over  long  time periods (e.g.,
annual averages).  However, the true relationships  between  emissions and
deposition which are anticipated theoretically can  be recognized and
accepted only when accurate and reasonably  complete chemical  reaction
schemes for acid generation have been employed in the theoretical model.
Of course, it is only this type of model, which  has been  properly built on
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fundamental principles and has been tested  adequately  with  field data,  that
can be employed with confidence in control  strategy  planning.

1.2  The gas phase tropospheric chemistry of S02  and NQ/NQ2  in  acid
     generation

     There have been a number of reviews which  have  provided a  focus on the
seemingly important gas phase S02/NOX reactions which  lead  to acids in
the troposphere (Calvert and McQuigg, 1975; Davis  and  Klauber,  1975; Cal-
vert et al., 1978; Davis et al., 1979; Friend et  al.,  1980;  Calvert and
Stockwell, 1983a; Durham et al., 1982).  The gas  phase reactions of many
reactive species common to the sunlight-irradiated troposphere  may  in
theory lead to S02 oxidation.  For example, the possible  reactants  include:
electronically-excited molecules such as 02(1Ag),  02(1Eg"1")  and  reactive
molecules and free radicals such as 0(3P),  03,  N02,  N03,  N205,  H02, CH302
and other alkyl peroxyradicals, CH3C002 and other  acyl  peroxy radicals, and
CH202 and other Criegee intermediates derived from ozone-alkene reactions.
The reactions of these species to oxidize S02 satisfy  one criterion for
their possible importance; that is, the reactions  have a  negative enthalpy
change (AH°298), and in theory they could contribute to the  atmospheric
oxidation of S02 provided the reactions are not kinetically  limited.  In
Table 1.1, several possible oxidation reactions of S02 are  summarized
(Calvert and Stockwell, 1983a).  In many cases, the  rate  constants  for
these reactions have been measured (see last column  of Table 1.1).   From
reasonable theoretical estimates of the atmospheric  concentration of each
given transient (X) and the rate constant for its  reaction  with S02 (kx),
the importance of the individual reaction can be  judged from the elementary
rate relation, -d(S02)/dt = (S02)(X)kx.  Such an  evaluation  points  to the
possible importance of only a few of the many possible reactions shown  in
Table 1.1.  These are the following:

                      HO + S02 (+M) + HOS02 (+M)                         (1)

                      HOS02	-»• H2S04

                      0(3P) + S02 (+M) + S03 (+M)                        (2)

                      RCHOO + S02 * RCHO +  S03                           (3)

                      RCH(0)0 + S02 ->• RCHO  + S03                         (4)

                      S03 + H20 * H2SO,,

                      CH302 + S02 + CH302S02                             (5)

                      CH302S02	+  H2S04

By far the most important of these reactions is (1).  This  and  the  analo-
gous N02 reaction (6) should be the dominant sources of gas  phase genera-
tion of acids within the troposphere:

                      HO + N02 (+M) ->• HN03  (+K)                          (6)


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Table  1.1   Enthalpy  Changes  and Recommended Rate Constants  for  Potentially-

   Important Reactions of  Ground State  S02  and  S03 Molecules  in  the Lower

   Atmosphere
       Reaction
                                          -AH°? kcal

                                        mole-1(25°C)
                                                                k,bcm3molec~1

                                                                   sec"1
         02(1J:p  + S02
             S02 *  S04(biradical;cyclic)



             S02-  S03 + 0(3P)



    02(^9) + S02 ->.  O^g) + -S02


                   S04(biradical -.cyclic)



             S02 *  S03 + 0(3?)



             S02 *  S02 + 02(^9)
         j

(2) 0(3p) + S02 (+M) * S03 (+M)



    03  +  S02 •* 02 +  S03


    N02 +• S02 * NO + S03



    N03 + S02 * N02  + S03



    ONOO  + S02 - N02 + S03



    N20s  +• SOg * N204 + S03



    HO? •"• S02 ->• HO + S03



    H02 + S02 (+M) * H02S02 (+M)


    CH302 + S02 * CH30 + S03



(5) CH302 + S02 (+M) * CH302S02 (+M)



    (CH3)3C02 + S02 * (CH3)3CO + S03



    (CH3)3C02 + S02 * (CH3)3C02S02


    CH3C002 + S02 -* CH3C02 + S03



    CK3C002 + S02 * CH3C002S02


(1) HO  + S02 (fM) * HOS02 (+M)


    CH30 * S02 (+M) + CH3OS02
-2S.-28



   -13.5



    22.5
                                                     -26



                                                     -30



                                                     -33



                                                     ~37



                                                     '37



                                                     "24
                                                                        -2fl
                                                                3.9 X 10
              6.6 X  10-16






              5.7 X  10-1*



             <8 X TO'24


              8.8 X  10-30



             <7 X TO'21



             <7 X 10-21



             <4 X 10-23




             <1  X 10-18




             <1  X 10-18



              1.4 X  10^14°




             <7.3 X  10-19






             <7  X 10-1q




              1.1  X  10'12



             "5.5 X  10'13
                                              131

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Table 1.1   Enthalpy  Changes  and Recommended Rate Constants  for  Potentially-
   Important Reactions  of  Ground State  S02  and S03 Molecules  in  the Lower
   Atmosphere (continued)
Reaction
RCH^HHtcHR n
DPtJ ^UD **" W
r\wn "" ' vnn
(3) RCHOO- + SO, -

i- S02 * 2RCHO + S03
+ S02 -* 2RCHO * S03
RCHO + S03
-AH9^ kcal
mole-l(25°C)
"69
"89
"79
sec-1
See text
See text

          RCHOO- + H20 * RCOOH + HjO
                                                           !<64/k66 = 6X10-5
                                                             (R = CH3)
(4)  RCHO- + S02 * RCHO + S03

     0-            jO-
    RCHO- + CH?0 * RCHOCHO-
                                            "58



                                            •12
                                                                 k65/k68 a 4
                                                                  (R = H)
S03 +  H20 + H2S04
                                                      24.8
                                                           9.1 X 1CH3
          aEnthalpy change estimates were derived from the data  of Benson (1978),
           Harding and Goddard (1978),  and Domalski  (1971).

           The rate constants are all expressed as second order  reactions for 1 atm of
           air at 25*C; see paper of Calvert and Stockwell (1983a) and Calvert et al.
           (1978) for references to the original  literature.

          °The reverse reaction is so fast that the  rate of  oxidation of S02 through
           (5) is very dependent on alternate fates  of the CH302S02 species; see the
           discussion.
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We will review briefly here the special  features  of  each  of these possible
pathways.

a.  The gas phase HO-radical oxidation  of S02  and N02  in  the troposphere

     Although the other gas phase  reactions  may in theory contribute to
acid generation in the troposphere under special  circumstances,  it is clear
today that the reactions of the HO-radicals  with  S02 and  N02 are the domi-
nant gas phase sources of H2SOi+ and HNO^, respectively.

                      HO + S02  (+M) * HOS02  (+M)                      -   (1)

                      HOS02 (+  other reactants) •»•

                           H2SOtt  (+ other products)

                      HO + N02  (+M) -> HN03  (+M)                          (6)

The reaction (1) is believed to be the  rate  determining  step in  the reac-
tion sequence which leads ultimately to H2SOtt.  Nitric acid is  the direct
product of the HO-attack on N02 in reaction  (6).   The  rate constants.for
these reactions appear to be reasonably well-established.  From  a review of
the previous work, Calvert and  Stockwell (1983a)  recommend the  following
values for atmospheric pressures  near 1 atm:

     ki = (3.3 ? 0.6) x io-13ed-° + 0-2) *  103/T Cc molec'1 sec'1

     k6 = (1.0 + 0.2) x 10-11(T/Z98)-1*6 cc  molec-1  sec'1

Note both reactions (I) and (6) show a  negative temperature dependence;
that is, there is an increase in  rate with  a decrease  in  temperature for
given concentrations of the reactants.   These  rate constants are also a
function of the air pressure at the point of interest  in  the atmosphere.
The magnitude of the variation  in  these HO-radical rate  constants for S02
and N02 with altitude can be seen  in Figures 1.1  and 1.2, respectively.
The gradual increase in kx and  k6  up to 11  km  is  controlled by  the decreas-
ing temperature.  As the temperature stabilizes and  then  falls  at eleva-
tions above 11 km, the effective  second-order  rate constants fall  contin-
uously, reflecting both the increased sensitivity to decreasing  pressures
and the rising temperature in this region of the  atmosphere.

     One other important feature  of the HO-radical reaction with S02 must
be taken into account in any modeling effort of acid rain development.   The
choice of mechanism for the subsequent  steps of the  HOS02 radical  which
leads to H2SO,+ can alter significantly  the  results of  modeling  S02 and N02
conversions in the atmosphere (e.g., the degree of linearity of  S02 emis-
sion to acid deposition).  For  example, Rodhe  et  al. (1981), Samson (1982),
and Atkinson et al. (1982b) have  assumed that  the reactions (1)  and the
subsequent steps which lead to  H2SOi+ can be  shortened  to  the reaction (7)
for modeling purposes:

                      HO + S02  f HoSO,,                                   (7)


                                   .  133

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      10



       5
OJ

O
 u
 o>
 to
 o
 _O)

 o

 E
 i
 u
 o
0.01






300


250


200
                •Pressure
                                            j	-i
                                               1000
                                               100
                                                     33
                                                     m
                                                     CO
                                                     CO
                                               10    -_
m
«

3"
        0      10     20     30    40

                    ALTITUDE,  km
                                        50
 Figure  1.1   Variation of the apparent second order  rate

 constant for the reaction 1 as a function of altitude

 calculated from the  equations of Table III of Calvert and

 Stockwell (1983a) for the conditions of pressure and temp-

 erature defined for  the standard atmosphere (Valley, 1965),

 The pressure is shown as the dashed line.  The temperature
 is  shown on the lower part of the curve.

 HO  + SO? (+M) *  HOSOz'(+M) (1).
                              134

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       10


       5
CM

 2     I
 o
 Qj

 O

 E
 I
 O
 O
  O
O.I
    0.01
                            Pressure
                                 i
                                                        1000
                                                        100
                                                                   m
                                                                   CO
                                                                   C/)
                                                                   c
10
         0
            10   15  20 25  30  35 40  45  50

                    ALTITUDE
  Figure 1.2   Variation of the apparent second order rate constant for
  the reaction 6,  HO + N0£ (+M) •»• HN03 (+M)  as a function of altitude,
  calculated from  the equations summarized by Calvert and Stockwell (1983a)
  for the conditions of pressure and temoerature defined for the standard
  atmosphere (Valley, 1965).
                                   135

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The acceptance of this overall reaction is equivalent to assuming  that  the
HO-radical addition to S02 terminates the chain reactions of the HQ-radi-
cal, and by some undefined process the initial product of reaction  (1)
leads to H^Q^ without regenerating chain-carrying species.  This  perturbs
the atmospheric reaction cycles involving H02 and HO radicals which  lead  to
the oxidation of hydrocarbons, aldehydes, CO, S02, NO, N02, and other im-
purity species.  For example, the oxidation of CO occurs in reactions (8)-
(10) by way of HO-radical attack on CO:
                      HO + CO •>• H + C02

                      H + 02 (+M) + H02 (+M)

                      HO, + NO + HO + NO,
                                                   (8)

                                                   (9)

                                                  (10)
Note that although an HO-radical is lost in (8), another is regenerated  in
(10).  Similar cycles occur involving CH20, the.hydrocarbons, etc.  Now  if
a reaction such as (7) occurs, an HO-radical is removed and no further re-
generation of the HO-radical occurs.  However,  recent evidence shows  clear-
ly that the HO-radical concentration in a photooxidizing mixture of CO,  or
hydrocarbons in air, is not perturbed significantly by S02 additions  to  the
reacting mixture (Stockwell and Calvert, 1983a).  Thus, a reaction sequence
such as (1)-(11)-(12) describes better the net  reaction of OH and S02:
                      HO + SO, (+M) + HOSOo (+M)
                                                   (1)
                      HOS02 + 02 > H02 + S03                            (11)

                      S03 + H20 + H2S04                                 (12)

Reaction (13a) summarizes the net chemistry involved in  these  steps.
HO + S02 (+02,H20)
                                                   H0
(13a)
In writing reaction (13a), it is assumed that a chain carrying  radical
(H02) is developed following the occurrence of reaction  (1).  Presumably
reaction (11) would be followed often by the HO-radical  regeneration
through the reaction (10), at least in NO-rich, polluted atmospheres:
                      HO, + NO •* HO + NO-
                                                  (10)
The involvement of reaction (7) results in a direct nonlinear  feedback  into
the S02 oxidation mechanism, while the net reaction (13a)  does  not  perturb
seriously the HO-radical concentration.  As we have discussed  previously, a
net reaction such as (13a), rather than (7), describes  best  the  experimen-
tal results available today; chain termination as  implied  in reaction  (7)
is probably unimportant.

     The choice of the  seemingly similar reactions  (7)  or  (13a)  to  describe
the chemistry of the H0-S02 reaction is of more than academic  interest;  it
can lead to very different results when these reactions  are  used in long-
range transport models.  To illustrate this, the results obtained in  recent
simulations by Samson (1982) are summarized in Figure 1.3.   The  solid
                                     136

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II
<
ss
       50
      30
       10
      -10
      -30
     -50
                       /96h
                     /48h
                                                    96 h7/
                                                    24h
        -50
                    -30
-10        10

 % A S02
30
50
    Figure  1.3   Tests of the linearity of regional scale SOe - NOX  models
    from Samson (1982).  The model  is similar  to that used by Rodhe  et al.
    (1981).  The solid lines represent the relation of S02 cutback to
    change  in sulfate aerosol at various times of transport downwind from
    the sources.  The dashed lines_show results from similar simulations in
    which background sources of S0| aerosol  were removed and the reaction
    HO + S02  •»• H2S04 was replaced  with HO + S02 -»• H2$04 + H02-  Note the
    near linearity for the results  at long transport time which comes from
    these mechanism changes.
                                   137

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lines, calculated using the Rodhe mechanism  including  reaction  (7),  show
the relation between the percentage reduction in ambient  sulfate  concentra-
tion for various times of transport (24, 48, 96 hr)  and the  percentage  cut-
back in S02 emissions in the source regions.  The  dashed  lines  are  from
Samson's results calculated using the same conditions  and mechanism,  with
one change—the reaction which leads to homogeneous  oxidation of  S02  in the
Rodhe et al. model was changed from (7) to (13a).  Note that the  results
are altered significantly; the observed relation between  AS02 and ASO^
approaches much closer to the "linear" dependence  for  results with  long
transport times (96 hr).

     Some measure of the typical rates of S02 and  N02  oxidation through
homogeneous chemical reactions can be obtained from  computer simulations
which have been made recently by Stockwell and Calvert (1983b).  The  rates
are, of course, strong functions of the NOX, hydrocarbon, aldehyde,  rela-
tive humidity, and solar intensity.  For a typical cloudless summer day in
a relatively clean tropospheric air mass,1" the maximum[HO] of about 9.1 x
106 molec cc"1 is achieved near noontime.  The 24-hr average [HO] is  about
1.7 x 106 molec cc"1; this leads to a 24-hr  averaged rate of S02  oxidation
through reaction (13a) of 0.7% hr'1 or 16.4% per 24-hr period.  The equiva-
lent N02 oxidation rate in (6) is 6.2% hr"1  or 150%  per 24 hr.  The average
wintertime rate of gas phase oxidation is expected to  be  much lower;  for
S02 in an air mass with similar levels of the impurities, the 24-hr aver-
aged rate is about 0.12% hr"1 or 3% per 24 hr; for N02, it is about 1.1%
hr"1 or 25% per 24 hr.  These rates can be very much slower  in  air  masses
rich in NO such as exist in the early stages of stack  gas plume releases.
However, it is clear that in theory we expect the  homogeneous gas phase
conversion of S02 and N02 through the HO-radical reactions alone  to-provide
a significant quantity of sulfuric and nitric acids  within the  troposphere.

b.  The oxidation of S02 by products of the  alkene-ozone  reactions

     Probably the second most significant of the S02 atmospheric  oxidation
pathways in the gas phase is that derived from the intermediates  formed in
the alkene-ozone reactions.  Although the rate of  reaction of ozone with
S02 is extremely slow, the addition of an alkene to  a  dilute 03-S02 mixture
in air results in the significant oxidation  of the S02 (Cox  and Penkett,
1971).  Several possible chemical species could be the oxidizing  agent  here
(Calvert et al., 1978):  the oxonide formed  in (13b);  the primary Criegee
intermediate formed in (14); the rearranged  intermediate  formed in  (15);
or, possibly, the HO- or other radical fragmentation product of the re-
arrangement and decomposition of the vibrationally rich products  of the
reaction (16):

                                       P-o-o. t
                      03 + RCH=CHR + RCH	RCH                         (13b)
    "h"he concentrations of  impurities  at  sunrise were  taken  as  (ppb):  03,
30; NO, 0.75; N02, 0.25;  alkane  (non-methane),  4;  alkene,  1;  CO,  100;  CH20,
0.2; CH3CHO, 0.1; ketone, 0.05;  S02, 0.6; CHt,,  1400;  relative humidity,
10%; temperature, 25°C.

                                     138

-------
0-o-Q
                     ,0--,  t
                   RCH - RCH  > RCH + RCHOO                            (14)
                                    9"
                    •  •     v
                   RCHOO  > |)CHR # CHR-0*                             (15)
                            0
                   o-        ot
                   CRH-0* - R&-OH  + Radical products                  (16)

Each of the possible reactants could oxidize S02 in the highly exothermic
reactions which follow:

                     ,0-0-0%
                   RCH - RCH + S02 •»• 2RCHO + S03


                   RCHOO' + S02 * RCHO + S03                             (3)

                    O'
                   RCH-0* + S02 - RCHO + S03                             (4)

The species RCHOO* and RCHO* appear to be the most viable candidates
for the reactant with S02 here (reactions (3) and (4)).

     Subsequent more detailed studies of the 03-alkene-S02-air system by
Cox and Penkett (1972) gave strong kinetic evidence of an inhibition of  the
S02 oxidation by increased H20 vapor concentration.  Calvert et al . (1978)
speculated that an H20-RCHOO complex could form and catalyze the  rearrange-
ment of the ftCHOO* (or RCHO*) species to the corresponding acid:
                                        CH-
Indeed, Hatakeyama et al. (1981) found that the CH202 species reacted with
H2  0 to produce labeled formic acid as expected from this picture.  Cox
and Penkett's results gave no absolute rate constants, but Calvert et al.
(1978) have treated their data from cis-2-butene reactions in terms of this
mechanism and derived the rate constant ratio, k17/ki+(3) = (6.1 + 0.3)
x 10-5
                   RCH02 + H20 * RC02H + H20                           (17)

                   RCH02 + S02 * RCHO + S03                           (4,3)


                                     139

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Whether the explanation of the effect given by Calvert et al .  is  correct  or
not, the remarkable inhibition of the S02 oxidation shown by H20  is  unex-
pected from species such as HO, H02, and R02 whose concentrations  are  lit-
tle affected by the presence of H20 vapor.  Thus, a maximum  of  only  a  few
percent of H02 radicals are hydrated in the gas phase (H20-H02) at ordinary
temperatures and humidities (Calvert et al., 1978; Hamilton  and Naleway,
1976).  CH302 radicals also show no evidence of significant  hydration  as
monitored from the insensitivity of the CH302-CH302 reaction rate  constant
to H20 vapor concentration (Kan and Calvert, 1979).  The H20 effect  ob-
served by Cox and Penkett seems to be most reasonably related  to  the H20
effect on the Criegee intermediates, RCH02, as discussed above.

     Several experiments demonstrate the reality of the Criegee interme-
diates in these gas phase O^-alkene systems.  The identification  of  the
intermediate dioxirane, CH^x, in the low temperature reaction  of  ozone and
ethylene (Lovas and Suenram,  1977; Martinez et al., 1977) provides convinc-
ing evidence for the role of Criegee intermediates in these  systems.   Pre-
sumably, it arises in reaction (15).  Niki et al . (1977) showed clearly
that a large fraction of the gas phase ozonolysis of cis-2-butene  occurs
via the Criegee intermediates as well.  In a further study of  this system,
Niki and his coworkers (1980) found new evidence of the nature  of  the  S02
reactant in 03-alkene-S02 systems.  The normal propyleneozonide product
formation in cis-2-butene-CH20-03 mixtures (reaction (19)) was  quenched
with the addition of a small  amount of S02, and the S02 was  consumed (to
form aerosol, presumably H2SOit) to the extent the ozonide was  formed in  the
absence of S02.  Reactions (18)-(20) show the mechanism involved.  Presum-
ably S02 in reaction (20) competed favorably with CH20 in (19)  for the
CH3CH02 species.

               CH3CH=CHCH3 + 03 •»• ozonide •»• CH3CH02 + CH3CHO            (18)


               CH3CH02 + CH20 + CH3CH^ ^CH2                           (19)
               CH3CH02 + S02 -»• CH3CHO + S03                             (20)

In further recent studies, Su et al . (1980) used ppm concentrations  of
C2H4, 03, CH20, CO, and S02 in N2/02 mixtures near  room  temperature  and 700
torr total pressure.  They determined the relative  rates of  the  reaction
intermediate (presumably CH202) with S02, CH20, and CO gases.  The mech-
anism for the C2Hlt-03-S02 system suggested by this  work  and  that of  the
further studies by Kan et al . (1981b) and Niki et al .  is as  follows:

                                .0-0-0
               CH2CH2 + 03 * CH2 - CH^ (A)                           (21)

               A  *  CH202t + CH20                                      (22)

               CH^1"  + CO + H20  (58 + 10%)                            (23)
                                     140

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                       •»- C02 + H2           )                            (24)
                                  (35 + 6%) \
                       + C02 + 2H           )                            (25)

                       •»• HC02H    (7 + 1%)                              (26)

               CH2Q2* + M * CH2°2 + M(38£)                              (27)

               CH202 + S02 * (CH202S02)t ->•  CH20 +  S03                   (28)

               S03 + H20 + HzSOi,  (aerosol)                           -  (12)
               CH202 + CH20 •»• CH2     CH2     (8)                        (29)
                                 ^F
                                              Q
               (B)  ->  *OCH2OCH20*  -  HOCH2OCH                         (30)

               CH202 + CO + (HCO)20                                     (31)


     The fraction of the initial CH202 species formed  in  the  03-C2Hit  re-
action in air near 1 atm pressure which  is  yibrationally  relaxed and  lives
to react by means other than decomposition  is large:   - 38%  (Suet al.,
1980), 35 ? 5% (Niki et al., 1981), and  37  +  2%  (independent  of  temper-
ature, 9-30°C, Kan et al., 1981b).  The  relative  rate  constants  for CH202
reactions with S02 in (28), CH20 in (29), and CO  in  (31)  are:  400 :  100 :
0.7.  It is clear that S02 oxidation can occur efficiently through the
CH202 species, and the higher analogues  appear to behave  similarly.   Thus,
with the higher alkenes, Cox and Penkett estimated that about 10% of  the
intermediates survived reaction with H20 at 40 -  10%  relative humidity  and
could oxidize S02.

     Unfortunately, it is difficult to assess the significance of the al-
kene-03 reaction products as S02 oxidants in  the  real  atmospheres, since
one important relative rate constant for the  active  intermediates is  mis-
sing at this time.  Data for the competitive  rates with S02  and  NO are
required.  The exothermicities of the possible reactions  of CH202 with  NO
are equal to or greater than that of the analogous reaction with the  struc-
turally and electronically similar compound,  ozone:

            'CH200* + NO * CH20 + N02; AH = -97 kcal mole'1             (32)

            •OCH20' + NO •>• CH20 + N02; AH « -51 kcal mole'1             (33)

            03 + NO •»> 02 + N02; AH = -48 kcal mole'1                    (34)

Thus, one might anticipate that k32 = k33 = k34 = 1.6  x lO-1**  cm3 mole'1
sec"  (Clyne et al., 1964).  Until reliable kinetic  information  on the
influence of NO on the oxidation of S02  by  CH202  and equivalent  species is
available, the significance of these Criegee  intermediates in S02 atmo-
spheric reactions must remain somewhat speculative.  However,  for relative-
ly clean tropospheric air, low in NO, but with levels  of  ethene  at the  ppb

                                     141

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level and 03 near the 0.1 ppm level, the maximum rate of S02 oxidation  from
these 03-C^ product reactions is 0.03% hr   .  The presence of  the more
reactive alkenes at this level leads to somewhat higher rates of S02 oxi-
dation.  Since these reactions are not directly dependent on sunlight gen-
eration, they will continue unaltered in rate at night, as well  as during
the day, as long as the alkene and ozone supply is maintained.   Further
quantitative work on the RHC02 rate constants with NO and other  atmospheric
impurities is needed to allow a more quantitative assessment of  this prob-
able S02 oxidation pathway.  Models under development today should include
the S02 oxidation by Criegee intermediates in the more complete  mechanistic
versions.  In highly simplified chemical versions used in modeling acid
rain generation, the neglect of the Criegee intermediate should  not in-
troduce large errors.

c.  The 0(3P)-atom oxidation of S02

     The 0(3P)-atom does react readily to oxidize S02 in the reaction (2):

                      0(3P) + S02 (+M) * S03  (+M)                        (2)

Combining the data of Westenberg and de Haas  (1975) for this reaction with
M = N2 and that of Mulcahy et al. (1967) for M = 02, we estimate a value of
the apparent second-order rate constant, k2 = (5.7 + 0.5) x 10    cm3
molec   sec   for air at 1 atm and 25°C.  During the daylight hours in  the
usual polluted atmosphere, the 0(3P) concentration is roughly proportional
to the N02 concentration.  Whenever [N02] is  high, the rate of 0-atom gen-
eration is high through the N02 photolysis reaction (35):

                      N02 + hv (A < 4300 A) + NO + 0(3P)                (35)

The dominant loss reaction for 0(3P) in the troposphere is through the
rapid reaction with molecular oxygen (reaction (36)) so that the steady
state concentration of 0(3P) is low in the troposphere, typically below
2 x 10  molec cm   (Demerjian et al, 1974).  This results in a maximum  rate
of S02 oxidation of about 10~2%/nr in the sunlight-irradiated, N0x-pollu-
ted troposphere.

                      0 + 02 (+M) > 03 (+M)                             (36)

However, for the special case of stack gases  at relatively high  concentra-
tions of impurities, a burst in S03 formation from reaction (2)  is antici-
pated during the early stages of dilution of  the stack gases (Calvert et
al., 1978).  Thus, if the concentrations of impurities shortly after re-
lease from a stack were:  NO, 500; S02, 500;  N02, 20; 02, 1 x 105 ppm,  then
the instantaneous rate of S02 oxidation through reaction (2) alone can  be
as high as 1.4%/hr.  As plume dilution with air occurs by factors of 4, 8,
16, and 32, the instantaneous rate of reaction (2) falls quickly to 0.43,
0.20, 0.10, and 0,05%/hr, respectively.

d.  The CH302 reaction with S02

     The detailed evidence related to the reaction (5) has been  reviewed
recently by Kan et al. (1981a) and Calvert and Stockwell (1983a). From the

                                     142

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available mechanistic and kinetic data, it is clear  that  the  analogues  to
the CH302 radical, namely H02, t-Ci+H302, and CH3C002  radicals,  are  unim-
portant in oxidizing S02 in the gaseous phase of the  atmosphere.  There  is
conflicting evidence related to the reaction (5):

                      CH302 + S02 * CH302S02	*  H^               (5)

The interpretation of Kan et al. suggests that  reaction (5) and the subse-
quent reaction (37) are reversible:

                      CH302 + S02 £ CH302S02                          -   (5)

                      CH302S02 + 02 * CH302S0202                        (37)

Only when the CH302S0202 radical is converted to the  CH302S020  radical
through reaction with another peroxy radical or reaction  with NO  is the  S02
molecule locked into the higher oxidation state represented in  CH302S020:

                      CH302S0202 + R02 + CH302S020 +  RO + 02            (38)

                      CH302S0202 + NO •> CH302S020 +  Nn2                 (39)

This radical cannot reform S02 but forms S03 on dissociation:

                      CH302S020 + S03 + CH302                           (40)

In terms of this reasoning, it appears probable at this writing that the
CH302-S02 reaction will be unimportant for S02  oxidation  in the atmospheric
mixtures relatively low in NO, N02, and R02 impurities.   In a highly pollu-
ted atmosphere, the effective rate of S02 oxidation  by CH302  could  in the-
ory become very significant, presumably with a  rate  constant  as high as  1.4
x 10-14 cm3 molec-1 sec'1.  Calvert and Stockwell (1983a) concluded that
there is no realistic alternative to modelers today  but to use  k5 =0 in
atmospheric simulations, although this practice may  result in the under-
estimation of the importance of this reaction for the conditions  of high
pollution.

1.3  The gas phase chemistry of the troposphere and  the mechanism of
     generation of the reactants for S02 and N0/N02

     The generation of the reactive species HO, 0(3P), CH202  (and its ana-
logues), and the seemingly important reactants  for the solution phase oxi-
dation of HS03" to H2S04 and N02 to HN03 in cloud water and rain, namely
H202, 03, N03, and N205, occurs in a series of  interrelated reactions.
This complex chemistry must be described in any model in  sufficient detail
to allow a reasonably accurate estimate of the  important  reactants  for  S02
and N02 which we have identified in the previous sections, namely,  HO,
0(3P), CH202, H202, 03, N03, and N20s.  It is important to review the
elements of the chemistry at this point.

     The typical urban atmosphere receives a variety  of trace impurities as
a result of emisions from vehicles, power plants, industrial  operations,
and other human activities, as well as from natural  sources such  as trees,

                                     143

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plants, and soils.  Commonly these are rich in oxides of nitrogen  (NO,  N02)
and sulfur (S02), a great variety of hydrocarbons (alkenes, alkanes, and
aromatics), and their oxidation products such as the aldehydes and  ke-
tones.  The action of sunlight upon this complex mixture may result  in  the
creation of secondary pollutants whose properties are often very different
from those of the original mixture.  Thus, ozone, peroxyacetyl nitrate,  ni-
tric and sulfuric acids, and other reactive compounds may form.  The chem-
ical mechanism of ozone generation within an NO, N02, hydrocarbon,  alde-
hyde-polluted air mass appears to be well understood (Leighton, 1961;
Demerjian et al., 1974; Niki et al., 1972; Stedman and Jackson, 1975;
Calvert, 1976).  The important sequence of reactions shown below can be
used to rationalize 03, NO, and N02 concentrations in polluted, sunlight-
irradiated, urban atmospheres:

               N02 + hv (X < 4300 A) + 0(3P) + NO                       (35)

               0{3P) + 02 (+M) + 03 (+M)                                (36)

               03 + NO > 02 + N02                                       (34)

               03 + N02 + 02 + N03                                      (41)

               03 + alkene (RH) -»• Products                              (42)

               03 + hv (x < 3100 A) -> 0(10,3P) + O^Ag^Ig-)           (43)

               03 + HO + H02 + 02                                       (44)

               03 + H02 + HO + 202                                      (45)

Thus, the approximate instantaneous rate of ozone generation in the  absence
of significant atmospheric turbulence, heterogeneity, dilution, loss at
ground level, or diffusion within the volume element of interest should be
given by (46):

   d[03]/dt = [N02]k35 -  [03]{[NO]k3u + [N02]km + [RH]kH2 + k43...}    (46)
In a highly polluted atmosphere, the rate of change of 03 with time  is  of-
ten small compared to the first two terms on the right of equation (46),
and for many conditions encountered in these polluted atmospheres, the
terms involving km, ki+2, k^3, etc., are small compared to that containing
k3i+,  For these circumstances, the approximate relation (47) may  describe
the impurity concentration relationships reasonably well:

                      [03][NOJ/[N02] = k35/k3lt                          (47)

Deviations from relation (47) up to 50% can be expected, however, for rela-
tively clean atmospheres which are low in NO, as the alternative  reactions
of 03 in (41), (42), etc. become more important for these conditions  (Cal-
vert and Stockwell, 1983b).  However, relation (47) holds qualitatively for
most of the conditions encountered in the regions of acid rain concern
(eastern United States) and  it provides a useful guide to the  [03] to be
expected in various atmospheres; the [03] = ( [N02T/[NO])(k35/k3tJ.   For a

                                     144

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typical sunny day, the ozone level continues  to climb  slowly  throughout the
day, reflecting a rise in the  [N02]/[NO]  ratio.  Obviously, the  conversion
of NO to N02 occurs in the troposphere as  the  day  progresses,  and  it  is the
mechanism of this very important process  which governs much of the chem-
istry of the troposphere.  It  has been well established  both  through  so-
called "smog chamber" experiments and theoretical  considerations using
computer modeling of the chemistry of these systems, that  hydrocarbons  and
their oxidation products, e.g., the aldehydes  and  carbon monoxide,  are  in-
strumental in effecting the NO to N02 conversion.  Obviously,  when in the
photostationary state, interplay between  NO, 03, N02,  and  sunlight through
reactions (35), (36), and (34) does not result in  any  net  NO  to  N02 conver-
sion.  Other reactions must be involved.   At  the very  low  levels of NO  in-
volved in the ambient troposphere, the thermal oxidation of NO by  02  (2NO +
02 -»• 2N02) is much too slow to be a significant conversion mechanism.  In
the past twenty years, a great deal of insight into  the  nature of  these
reactions has been gained.  Studies have  shown clearly that the  hydroperoxy
(H02), alkyl peroxy (R02), and the acyl peroxy radicals  (RC002)  are the
dominant primary driving force for NO to  N02  conversion, and  these ori-
ginate largely from the attack of the important hydroxy  (HO)  radical  on
hydrocarbon (RH), aldehyde (RCHO), and CO  impurity molecules.  Typical
generalized reactions which occur are the following:

                      HO + RH  + H20 + R                                 (48)

                      R + 02 + R02                                      (49)

                      R02 + NO * RO + N02                              (50)

                      HO + RCHO + H20 +• RCO                             (51)

                      RCO + 02 •»• RC002                                  (52)

                      RC002 +  NO > RC02 + N02                           (53)

                      RC02 •»• R + C02                                    (54)

                      CH20 + HO * HCO + H20                             (55)

                      HCO + 02 * H02 + CO                              (56)

                      H02 + NO + HO + N02                              (10)

                      HO + CO  * H + C02                                  (8)

                      H + 02 (+M) > H02 (+M)           •                  (9)

     Alkoxy radicals (RO) formed in (50)  can  generate  efficiently  the H02
radical.  For example, the CH30 radical reacts largely by  (57) when in  the
lower troposphere:

                      CH30 + 02 + H02 + CH20                            (57)
                                      145

-------
When one couples NO oxidation steps such as (50),  (53), and  (10) with  the
regeneration of the HO-radical in (10) and reformation of peroxy radicals
in (48), (49), (51), (52), (55), (56), (8), and  (9), then one  has  the  ele-
ments of a chain reaction which can occur over and over again  as MO  is  con-
verted to N02 and hydrocarbon, aldehyde, and CO  react in these free  radical
processes.  The cycle of events can be summarized  in the following diagram:
                   NO
RCOOr
R0  '
                                      RH
                                      RCHO
                                 (50,53,101
                                               hv(35)
                                              + NO
     In the highly polluted troposphere, the 03 level is established large-
ly through the rapid reactions (35) and (34), but the cycle of  (48),  (49),
(51), (52), etc., followed by (50), (53), and (10),  followed  again  by (48),
(49), (51), (52), etc., raises the [N02]/[NO] ratio  and accordingly raises
the [03] as implied by relation (47).

     We cannot claim that we understand well all of  the detailed  reactions
that make up this NO to N02 conversion sequence, although  the general  fea-
tures as outlined above can account reasonably well  for laboratory  and
field measurements made to date.  The limitations to our understanding will
become somewhat clearer when one notes the extreme complexity of  the reac-
tant mixture in an urban atmosphere.  Thus, Laub and Smith  (1982) have re-
solved chromatographic peaks corresponding to over 850 different  compounds
in a sample of Shell unleaded gasoline.  Mot only does a small  portion of
these hydrocarbons enter the urban atmosphere by evaporation  and  incomplete
combustion, but the many different products of partial oxidation  of each
compound form to create a mixture of almost incomprehensible  complexity
when joined with the many other emissions from other human  activities and
natural sources.  Most of these compounds undergo a  series  of reactions
initiated by the HO-radical (generalized reaction (48)), and  the  subsequent
primary reactions of the radicals formed are not only diverse but often
ill-defined.  For example, in Table 1.2, we have illustrated  some of the
variety of degradation pathways for a simple hydrocarbon,  n-butane.  Here,
the primary attack of the HO-radical on butane creates either the secondary
butyl radical (about 78% of the time at 25°C) or the n-butyl  radical  (about
22%).  Note that in Table 1.2, following the initial HO-radical attack, re-
actions occur which lead to every structurally-allowable aldehyde and ke-
tone as well as difunctional hydroxyaldehydes, etc.  Ozone  attack on the
alkenes also leads to complex degradation pathways which give many  new
species in addition to the aldehydes and ketones; these include ozonides,
Criegee intermediates (CH202, CH3CH02, etc.), acids, etc.   Some typical
                                     146

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Table 1.2  Typical Hydrocarbon Reaction Pathways in the Polluted Troposphere
OH + CH3CH2CH2CH3 —*• H2O + CH3CHCH2CH3	> Other Products

                    ^ H20 + CH3CH2CH2CH2
              CH3CH2CH2CH20
                 I (o2)
              CH3CH2CH2CHO    CH2CH2CH2CH2OH

                                  |(02)

                             OOCH2CH2CH2CH2OH

                                  |(NO)

                             OCH2CH2CH2CH2OH

                                  j(02)
     CH3CH2CH2CH202
     CH3CH2CH2 + CH2O
                       hv
     CH3CH2CH2 + HCO
        J<02>

     CH3CH2CH2O2

                         j(02)

     CH3CH2 + CH20   CH3CH2CHO


               . hv
     CH3CH2 + HCO

       j(02)

     CH3CH202     > CH3CH20
     CO  -I- H-
HCO + H
                 ,(02)

                CO
                               OCHCH2CH2CH2OH
                                         | hv
                             CH2O + CH2CH2CH2OH (+  HCO)
                                        (o2)
                                    OOCH2CH2CH2OH
^
CH3 + CH20
JW (o2)
CH302 < 	
J-(NO)
CH30
|(02)
CH20
j(02)
CH3CHO <
jhv
CH3 + HCO

>
C

                                       J
                                                        (NO)

                                                   OCH2CH2CH2OH

                                                      |(02)

                                                      OCHCH2CH2OH
                                    CHO + CH2CH2OH
                                                                       HCO)
                                                       OOCH2CH2OH
               I(NO)
          OCH2CH2OH

              I
OCHCH2OH     CH2O + CH2OH
    fhv
HCO + CH2OH

                                                            CH20
                                     147

-------
reactions in the sequence involving the simplest of  the alkenes,  ethylene
(C2HiJ, are summarized in Table 1.3 for illustration.  The alkenes  also  re-
act readily with the HO-radical where addition to the  double  bond is  fol-
lowed by peroxy radical generation and a variety of  other reactions similar
to those shown for the C^-^H^ system.  The aromatic hydrocarbons (benzene,
toluene, xylenes, etc.) also undergo a unique series of reactions with the
HO-radical, which leads to both HO-substitution on the ring and  ring  rup-
ture with a variety of complex products (e.g., see Atkinson et al., 1980).

     Each of the more than 850 hydrocarbons of the gasoline analysis  and
the extremely large number of partial oxidation products of these,  coupled
with the thousands of other volatile organic compounds released  into  the
atmosphere from the many non-combustion and other combustion  sources,  has
different complex degradation pathways which must lead to literally hun-
dreds of thousands of different chemical species in  a  polluted tropo-
sphere.  The nature of the general pattern of these  reactions can be
theorized reasonably well, but many reactions are not  well characterized;
e.g., the competitive reactive channels for the many alkoxy radicals  is  un-
known.  It is clear that we have little hope today of  incorporating all  of
the detailed chemistry which occurs in a polluted troposphere into  models
which we develop to describe it.  Model development  based upon generalized
reaction schemes has progressed through the years, particularly  in  relation
to ozone control strategies.  At this stage of our understanding  of the
many complex reaction schemes, there are no reasonable alternatives which
we can call upon.  However, we should recognize that the output  from  models
which employ highly simplified reaction schemes may  not simulate  well  the
happenings in many real atmospheres of unusual compositions (e.g.,  those
containing a dominance of terpenes).  It is also evident that any highly
simplified model cannot be used for predictive purposes beyond those  for
which it has been parameterized and "validated" against experimental  data
derived from simulated atmospheric mixtures and actual atmospheric  measure-
ments.

     Various detailed chemical mechanisms have been  developed through  the
years with the aim of simulating by computer the experimental results  from
the photooxidation of very simple hydrocarbon-NOx-air  mixtures.   Reaction
schemes were designed for NOX mixtures with isobutene  (Westberg  and Co-
hen, 1969), propylene (Hecht and Seinfeld, 1972; Niki  et al., 1972),  and
propylene, trans-2-butene, isobutene, n-butane, formaldehyde, and acetalde-
hyde (Demerjian et al., 1974).  In the latter study, several  hundred  ele-
mentary reactions were required to define the chemistry of these  relatively
simple mixtures.  Such detailed reaction schemes play  an important  role  in
the identification of the important reactions in these systems and  in  the
ultimate formulation of more tractable, simplified reaction schemes of com-
parable accuracy in the estimation of key species.   It is apparent  from  our
previous discussions that the formulation of detailed  mechanisms  for  the
multicomponent mix of the real troposphere is an impractical  venture.  If
indeed such a model vsre developed, it would require literally hundreds  of
thousands of elementary reactions.  The rate constants for most  of  these
reactions would be unknown.  Although a reasonable theoretical judgment
could be made to estimate most of these, it is obvious that a computer
program containing this degree of detail could not run in any useful  time
frame.

                                     148

-------
      Table 1.3  Alkene-Ozone Reactions in the Polluted Atmosphere
                          (AH in parentheses)
CH2=CH2 * °3
 (A)  -OCH20-
          CH2   CH2
               H-C-O-C-H + H2?
                               H-C-O-C-H + H202?


 (B)  -OCH20.  + S02 —+- (OCH20S02)—*- ^2° + S03  (H2S04)
 (C)  -OCH20-  + CO —


 Relative  Rate Constants:  kA:kfi:]cc: :100:400:0.7

 (D*  -OCH2°'  + NO-*• (CH202NO>	*• CH2O 4- NO

     kD is unknown.today.
                                  149

-------
     Several groups have developed rather simplified yet  generalized  reac-
tion schemes which they have employed in transformation-transport models.
The sophistication of the chemistry was very low  in the early  attempts  to
model  ozone formation in the Los Angeles Basin; for examples,  see Wayne et
al. (1971) and Eschenroeder and Martinez (1972).  Most of the  half-dozen or
so reactions in these highly simplified, parameterized models  bear  little
resemblance to the actual chemistry which occurs  in the troposphere,  and
they focused mainly on predicting ozone levels.

     In recent years, rather sophisticated, "lumped" models have been de-
veloped to simulate the RH-NOX chemistry in smog  chamber  studies and  in
the troposphere.  They retain much of the detail  related  to the elementary
chemistry, yet the total number of reactions is usually less than one hun-
dred (e.g, see Hecht et a1,., 1974; Duewer et al., 1975; Graedel et  al.,
1976;  Bottenheim et al., 1977; Gelinas and Skewes-Cox, 1977; MacCracken
et al., 1978; Duewer et al, 1978; Atkinson et al., 1982b; Whitten et  al.,
1980;  and Killus and Whitten, 1982).  In all of these reaction schemes,  an
attempt is made to generate in realistic numbers  the important H02, R02,
and RC002 radicals following HO-attack on the hydrocarbons.  The major
differences in the existing simplified models lie in the  methods with which
the complex hydrocarbon chemistry is handled.  The usual  approach is  to
have several different types of hydrocarbons; that is, hydrocarbons of  dif-
ferent reactivities and structures (alkane, alkenes, and  aromatic hydrocar-
bons)  whose reactivities span those of the real atmosphere.  For example,
the recent reaction scheme proposed by Atkinson et al. (1982b), duplicated
in Table 1.4, utilizes propane and a higher "alkane" to represent the al-
kanes; ethene, propene, and butene to represent the alkenes; and benzene,
toluene, and xylene to represent the aromatic hydrocarbons.  Thus,  there
are eight different hydrocarbons (RH) with eight  different rate constants
for HO-reaction, and eight different chemical pathways which generate R02,
H02, aldehyde, and other products.  In addition,  eight different carbonyl
products are involved in this mechanism: formaldehyde (CH20),  acetaldehyde
(CH3CHO), RCHO (representing propionaldehyde and  all higher aliphatic alde-
hydes), acetone (CH3COCH3), methyl ethyl ketone (CH3COC2H5), glyoxal  (CHO-
CHO),  methyl glyoxal (CH3COCHO), and but-2-ene-l,4-dial (HCOCH=CHCHO).   The
inclusion of the carbonyl compounds is very important in  that  they  act  to
accelerate the photooxidation since they develop  free radicals through
their photo-decomposition in the sunlight.  The mechanism of Atkinson et
al. has a great deal of sophistication and detailed chemistry, and  it
represents well many of the features of a real, RH-NOx-polluted tropo-
sphere.  The terpenes, the natural hydrocarbons emitted by trees, etc., are
not treated explicitly in the mechanism, but presumably they would  be in-
cluded within the reactive alkene class.  This mechanism  appears to be  es-
pecially well-suited to the auto exhaust polluted atmosphere which  is rich
in NO, N02, and hydrocarbons.  It does not include termination reactions
involving the many R02 radicals; these radicals must linger in the  hypothe-
tical  atmosphere to react with NO, the fate of all the R02 radicals in  the
Atkinson et al. mechanism.  Although R02-R02 interactions are  unimportant
in the N0x-rich atmospheres, it is less realistic to assume this is the
case for the relatively clean atmospheres which are also  involved in  the
long-range transport of air pollutants.

     Another recently developed, attractive "lumped" mechanism, the so-

                                     150

-------
Table 1.4  Reactions  and  Rate  Constants Used in  the  Basic Standard Model
of  Atkinson  et al.  (1982b); rate constants,  etc.  from Atkinson et al.
(1982b)  unless otherwise  noted.
    Reaction
Notes
            Rate constant (ppm nun units)
    Inorganics
     1. NOj +
     1 NO + Oj-NOj + Oj
     3. Oj + hv-2OH
     4. OH+NO*HONO
     5. OH-t-NOj^HNO,
     6. HONO + hv-OH + NO
     7. HOi+NO-OH + NO,
     8. H
     9. H
    10. H
    11. H2Oj+hv-»2OH
    12.
    13.
    14.
    15.
    16.
    17. N2O,4-H2O-2HNOj
    18. NOj + hv-.0.3NO+0.7NO2+0,7Oj
    19. OH + Oj-HOj
    20. HOj + Oj-OH
    Formaldehyde
    21. HCHO-fh
    22. HCHO + hv-CO + Hj
    23. OH + HCHO^lHOj+CO
    Aceialdehyde
    24.
    25. OH + CHjCHO ^ CH,COS
    26. CHjCOj + NOj-PAN
    27. PAN-CH3COj + NOj
    28. CHjCOj-t-NO^NO2-t-CH,O3
    29 CHjOj + NO - HCHO + HO2 + NOj
    Propane
    30. OH -I- PROPANE -. POS
    31. POj + NO-HOj+NOj+CHjCOCHj
    Alkanes
    32. OH + Alkane - AO2
    33.
Z
3.
3.

4.
3.
5.
6
7.
7.
8.
9.
10.

10.

10.




11.



13.

14.
       ki variable
       k2-1.0xl06T-'e-|4SO'T
       *, -^,4, x 7.5x10-* [H2O]
       k4-8.7xlOiT-2
       k, -3.7xlO*T"1
       *,-1.5xlO»T-1
       k, -7.8xl013e-|000'T
     k,,
     k,,
     k14
           UxlO'T"
           5.3xl04T-'e-1<50'T
           8.4xlO*T-'
       ku«3.5xlO'fe-|Ja»-T
       k,,~1.33xlO-JT-1
       klt - ^k,
       k,, -7.0xl05 T-'e-
       k,, - ftk,

       *M * ft*!
       k23-4.4xlO*T-'


       *J4 - Ml
       k26-ZlxlO*T-'
     k2i
     k2,
           3.1xlO*T-'
           3.1xlO*T-1
       kjo-6.6xlO*T-1e-w°''r
       *„ -3.1xlO*T-'
     k,j - 8.0 x 10* T - ' e-
     kj, - 6.6 x 10» T - ' e-
 14    Explicit n-buiane
                          for explrat n-butane
                            for   lumped * C«
                            alkane
       + 0.6CH jCHO + ai RCHO + 0.5 MEK
               -.1.7NO2-0.8NO+0.9HO,+0.15 HCHO+0.3 CHjCHO+0.1 RCHO + 0.3 CH.COCH,
       +0.45 MEK
                                                Lumped > C» aikane mechanism
                                                fcjs « 3.1 x 10*T-' for both systems
                                           151

-------
Table 1.4  Reactions and Rate Constants Used in  the Basic  Standard  Model
of  Atkinson et al.  (1982b);  rate  constants,  etc.  from  Atkinson  et al.
(1982b)  unless otherwise noted (continued).
    Reaction                              Notes       Rmte constant (ppra nun units)
     Higher aldehydes
     34. OH -t- RCH02< RCOj                   15.    k» - 9.2 x 10* T"'
     35. RCOj + NOj-PPN                    15.    kjs - 2.1 x 10*1"'
     36. PPN-RCO,+N02                    16.    	"-'
     37. RCOj + NO-.C2H5O2-l-NO2             15.

     39.
     Keiones
     40. OH + MEK=3XO2                     17.   k««, - 4.4 x 1    ^
     41
     43. CH,COCH, + hv2JCH.CO,+CHjOi       18.
    Alkenes
    44. OH + Ethene ^ 2HCHO-t-NO2 - NO        19.
                         + HO2
    45. OH + Propene ^ HCHO -t- CH,CHO         19.
                         + HO2 + NO2
                         -NO
    46. OH + Butene^i l.g CHjCHO -t-0.9NO2       19.   k^ - 5.0 x 10* 1"
     -t-0.9H02-NO
    47. O3 + Ethene -. HCHO+0.4CH262
     +0.4CO + ai2HO2

     •h 0.2CH2o7+0.2 CH jCHOC •(- 0.3 CO
     + 0.2 HO2 -i- 0.1 OH + 0.2CH jO2
    49. Oj + Butene~CH3CHO-s-0.4CH,CHo6
     + 0.3 H02 +0.2OH + 0.45CHjO2 -f- 0.2 CO
    50. CH202 + NO -» HCHO + NO,                  k,0 - 3.1 x 10*T"
    51. CH,02+NOj -»HCHO + NO3                 k3l -S.lxlO^T"
    52. CHj02+S02-.HCHO + SOj-            20.   kJ2-3.0xlO*T-
    53. CH202-i-H2O-Product                      k,, - 1.ST"1
    54. CHjCHOO + NO-CHjCHO + NOj             fc,4 - 3.1 x 10*1"
    55 CHjCHOO-t.NO2-CH,CHO + NOj            ksj - 3.1 x 10JT"
    56. CH3CHOO-t.S02-.CH,CHO-t-SOi-       20.   k,. - 3.0x 10*T-
    57. CHjCHOO + H,O - Product
                                          152

-------
Table 1.4   Reactions  and  Rate Constants Used  in the Basic  Standard  Model
of  Atkinson et al.  (1982b);  fate  constants,  etc. from Atkinson  et al.
(1982b)  unless otherwise  noted (continued).
    Reaction
Notes
            Kate constant (ppm mm units)
    Aromatics
    58. OH + Benzene - 0.25 Cre$ol + 0.25 HO,
      + 0.75 ADD
    59. OH + Toluene-* 0.15 ARO, + 0.20CresoI
      + 0.20 HO, +0.65 ADD
    60. OH + Xytene - 0.25Cresoi + 0.25 HO,
      +0.75 ADD

    61. ADD + NO -0.75 NO, +0.75 HO,
      + 0.75 DIAL + «, (CHO), + «, CH,COCHO
    61 OH •(- DIAL-* El
    63. El + NO, -El NO,
    64. E1NO, -*E1 + NO,
    65. E1 + NO-3NO,-2NO + «,HO,
      + a,(CHO), + «4CH,CO, + a. CH,COCHO
    66. OH + (CHO), » HO, + CO
    67. (CHO), + hv-.HCHO + CO
    68. OH+CHjCOCHO^CHjCOj+CO
    69. CHjCOCHO + hv^CHjCOj + HOj
    70. OH+Cresol-ADD2
    71. ADD2 + NO-0.75NO,
         +0.75 HO, +0.75 DIAL
    71 NOj + Cresol -» HNOj + Pbenoxy
    73. Pbenoxy + NO, -» Products
         (o-. p-nitrophenols)
    74. ARO, + NO - tt75 NO, + tt75 HO,
         +a75ARCHO
    75. ARCHO + h»-> Products
    76. OH + ARCHO2>ARCOj
    77. ARCOj + NO, - PBZN
    78. PBZN -. ARCOj + NO2
    79. ARCO, + NO - PhO, + NO,
    80. PhOj + NO-Phenoxy + NO,

    50'        M  ,
    81. OH+SO, -SOi"
    Chamber dependent reactions
    82. 7-.OH
    83. Oj - Wail
    84. General Dilution
21.

21.

21.


2Z

23.

16
24.
       k,t -
  25.
  26.

  27.
  27.
       k«0 - 7.9 x 10* T ' ' for lumped %yiene

          - 1.05 x 10'T"' for esphcit m-xylene
       *., -.3.1x10*7-'
       k«, -11x10*?-'
       k«4-1.2xlOue-l)5WT
       k«, -3.1xlO*T-'
      1^-8.8x10*7-'

      fc,,-6.6x10*7-'

      k*c-l-'9x'l077-'
      t,,-3.1x10*7-'

      471- 6.6x10*7-'
      k,.- 6.6x10* 7-'
           5.7xlO*T-'
  27.    k,4-3.1x10*1"'
  27.
  27.

  27.
  28,
  29.
  29.
      *„- 3.1xlO*T-'
      k»o- 3.1x10*7-'
      *,,-1.5xlOu7-*

      ktl - ~ 1-5 x 10'*
                                            153

-------
called carbon bond mechanism, has been applied successfully  to  the  simula-
tion of a variety of RH/NOx/air mixtures  (see Whitten et al., 1980,  and
Killus and Whitten, 1982).  This method was developed expressly to  provide
a reasonable compromise between chemical  realism and computational  effi-
ciency.  In this very interesting approach, the reactivities of the  hydro-
carbons are sorted according to the kind  of carbon bond present in  the
hydrocarbon mixture.  That is, the reactivity per paraffinic carbon,  per
olefinic bond, or per aromatic ring is considered.  There are certain ad-
vantages to this system.  For example, it facilitates the development of a
mechanism which is carbon conservative.  Also through this system,  a  reduc-
tion is achieved in the range of reaction rate constants that must  be .cov-
ered for each lumped hydrocarbon species  that uses an appropriate averaged
rate constant.  The latest mechanism from this research group,  the  carbon
bond III mechanism, is shown in Table 1.5.  This has been used  successfully
in simulating a variety of smog chamber experiments.  The obvious disadvan-
tage of this mechanism, and it is not clear how important this  disadvantage
is, lies in its abstract formulation; the chemistry of the individual reac-
tions of the hydrocarbons bears little similarity to actual  elementary
chemistry involved in these systems.  Certain computational  "tricks"  (such
as that involving reaction 15 of Table 1.5) are included to  adjust  for in-
herent problems introduced by the carbon  bond formulation.   However,  the
carbon bond reaction system offers a well-tested alternative to those who
simulate smog chemistry.  Ongoing studies of Seinfeld (personal  communica-
tion, 1983) supported by the Environmental Protection Agency are designed
to identify the key roles of hydrocarbons in tropospheric simulations.  The
results should be useful to those who plan chemical model development when
they are available.


2.  THE SOLUTION PHASE AND HETEROGENEOUS  PROCESSES

2.1  Aqueous phase (aerosol, fog, cloud,  rain water) chemistry  of S(IV)
     oxidation to H2SOit

a.  Gas-particle and particle-particle interactions

     In this section, an analysis is provided of the aqueous and hetero-
geneous chemistry pertinent to the tropospheric production and  deposition
of acidic species.  Topics discussed include the physical interactions of
gases with particles and particles with particles, solution  and heterogen-
eous chemistry of sulfate production, solution and heterogeneous chemistry
of nitrate production, the interaction of nitrate and sulfate chemistry,
the potentially significant role of organics in these chemistries,  and  im-
plications for chemical feedback on a few meteorological processes  dis-
cussed previously (e.g., Section 6, Chapter IV).  The very nature of these
topics necessitates the coupling of particle physics with chemistry.  A
brief description of the fate of sulfur emissions will illustrate this
linkage.  Sulfur as emitted from a stack  is primarily gaseous S02 (with
some S03).  Once in the atmosphere, S02 can be oxidized homogeneously by
reacting with HO or other less important  species and result  in  sulfuric
acid vapor formation.  Depending upon meteorological conditions, the H2S0lt
vapor will acquire water vapor and additional H2SOif and result  in fresh
particle nucleation.  Additionally, the H2SOtt vapor produced homogeneously

                                     154

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Table 1.5  The Carbon Bond Mechanism III (Killus and Whitten, 1982)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
Reaction
N02 * NO + 0
0 * (02) + (M) * 03
NO + 03 * N02 + 02
N02 + 03 •»• N03 + 02
N02 + 0 -> NO + 02
OH + 03 * H02 + 02
H02 + 03 * OH + 202
OH + NOo * HNO,
°?
OH + CO -» H02 + C02
NO + NO + (02) * N02 + N02
NO + N03 •" N02 + N02
N02 + N03 + H20 * 2HN03
NO + H02 * N02 + OH
H02 * H02 * H202 + 02
X + PAR +
°2
OH + PAR -» MEOo + H70
Q
0 + OLE -* ME02 + AC03 + X
0 + OLE * CARB + PAR
°2
OH + OLE -» RA02
03 + OLE * CARB + CRIG
Oo + OLE * CARB + MCRG + X
Rate Constant
at 298K
*
4.40 x 106t
26.6
0.048
1.3 x 104
100
2.40
1.60 x 104
440
1.50 x 10-4t
2.80 x 104
§
1.20 x 104
1.50 x 104
105
1300
2700
2700
3.70 x 104
0.008
0.008
Activation
Energy
(K)
0
0
1450
2450
0
1000
1525
0
0
0
0
-1.06 x 104
0
0
0
560
325
325
-540
1900
1900
                                 155

-------
Table 1.5  The Carbon Bond Mechanism III (Killus and Whitten, 1982)
                            (continued)

22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38

39
40
41

0 +
0 +
OH +
°3 +
w
NO +
NO +
NO +
NO +
NO +
NO +
°3 +
°3 +
OH +
OH +
OH +
CARB
CARB

N02
PAN
H02
Reaction
°2
ETH -* ME02 + H02 + CO
ETH * CARB + PAR
ETH -£ RB02
ETH + CARB + CRIG
o2
AC03 -4 N02 + ME02
RB02 -2- N02 + CARB + H02 + CARB
°2
RA02 -4 N02 + CARB + H02 + CARB
°?
ME02 -4 N02 + CARB + ME02 + X
°2
ME02 -4 N02 * CARB + H02
ME02 * NRAT
RB02 + CARB + CARB + H02 + 02
RA02 * CARB + CARB + H02 + 02
CARB * CR02 + X
CARB -£ HO? + CO
°2
CARB -4 AC03 + X
* CO + H2
+ (Q2) -I 2/3 (2H02 + CO)
(2ME02 + CO + 2X)
+ AC03 * PAN
* AC03 + N02
+ AC03 •»• Stable products
Rate Constant
at 298K
600
600
1.20 x 104
0.0024
1.04 x 104
1.20 x 104
1.20 x 104
3800
7700
500
5.0
200
500
7000
6000
(=£.001 Kj)*
(=0.002 Kj)*

7000
0.022
1.50 x 104
Activation
Energy
(K)
800
800
-382
2560
0
0
0
0
0
0
0
0
0
0
0
0
0

0
1.35 x 104
0
                                 156

-------
Table 1.5  The Carbon Bond Mechanism III
                            (continued)
         (Killus  and Whitten,  1982)

42
43
44
45
46
47
48
49
50
51

52
53
54
55

56
57
58
59
60
61
62
Reaction
H02 4 ME02 * Stable products
NO 4 CRIG * N02 4 CARB
N02 4 CRIG * N03 4 CARB
CARB 4 CRIG * Ozonide
NO 4 MCRG * N02 4 CARB 4 PAR
N02 4 MCRG * N03 4 CARB 4 PAR
CARB 4 MCRG * Ozonide
CRIG * CO 4 H20
CRIG + Stable products
°2
CRIG -* H02 4 H02 4 CO

MCRG * Stable products
°2
MCRG -» MEO? * OH 4 CO
0.
MCRG -* ME02 4 H02
°2
MCRG -* CARB 4 H02 4 CO * H02
°?
OH 4 ARO -* RARO 4 H70
0-
OH 4 ARO -* H0? 4 OPEN
°2
NO 4 RARO -* N02 4 PHEN 4 H02
°2
OPEN 4 NO -* N02 4 DCRB 4X4 APRC
°2
APRC -* DCRB 4 CARB 4 CO
°2
APRC -* CARB 4 CARB 4 CO 4 CO
PHEN 4 NOo * PHO 4 HMO,
Rate Constant
at 298K
9000
1.20 x 104
• 8000
2000
1.20 x 104
8000
2000
670**
240**
90**
**
150
340**
425**
85**

8000
1.45 x 104
4000
6000
104**
104**
5000
Activation
Energy
(K)
0
0
0
0
0
0
0
0
0
0

0
0
0
o-

600
400
0
0
0
0
0
157

-------
      Table 1.5  The Carbon Bond Mechanism  III  (Killus  and  Whitten,  1982)
                                 '(continued)
63
64
65
66
67

68
69
70
71
72
73
74
75

PHO
PHO
OPEN
OH +
DCRB

PHEN
CR02
DCRB
HONO
OH +
°3 *
0*0 •
0*0
Reaction
+ N02 * NPHN
+ H02 * PHEN
+ 03 + DCRB + X + APRC
PHEN -£ H02 + APRC + PAR + CARB
-£ 1/2 (H02 + AC03 + CO)
1/2 (ME02 + H02 + 2CO)
+ OH * PHO
°9
+ NO -* N02 + H02 + DCRB
+ OH * AC03
* OH + NO
NO * HONO
O!D
*m o
+ H20 * OH + OH
Rate Constant
at 298K
4000
5.00 x 104
40
3.00 x 104
(=0.04 Kj)*

104
1.20 x 104
7000
(=0.06 Kj)*
9770
(=10-^!)*
4.44 x 1010
3.4 x 105
Activation
Energy
(K)
0
0
0
0
0

0
0
0
0
0
0
0
0
   Sunlight-dependent; units of
   Units of

 § Heterogeneous; pseudo third order.  Equal to  591  x  N205 + H20.

** Units of min"1.
                                       158

-------
may sorb on preexisting particles.  The pollutant S02 can  also  adsorb  on
dry particles containing carbonaceous material and through a  heterogeneous
reaction be oxidized to sulfuric acid.  Either way,  the  resulting  acid par-
ticle will behave according to the physicochemical principles governing the
growth of atmospheric particles through water vapor  acquisition.

     The subsequent wetted particle, whether  it be aerosol, cloud  droplet,
or hydrometeor, provides additional pathways  for S02 oxidation.  S02 vapor
can dissolve into the water of the particle and therein  form  S02'H20 and
its ions.  These species may then react with  aqueous 03  or H202  to produce
sulfuric acid.  The relatively low liquid water content  of typical  tropo-
spheric aerosols (<10-10 liters of H20(*)/liter of air;  Ho et al.,  1980)
compared to that for fogs and clouds (10~7 to 10~5 liters  of  H20(ji)/liter
of air; Pruppacher and Klett, 1978) restricts the net S02  incorporation and
conversion in aerosols compared with the fog  and cloud chemistry pathways;
this assumes that suitable oxidizing agents (H202, 03, etc.)  are present  in
each case.  A similar scenario can be described for  nitric acid  formation
(see Section 2.2).  The occurrence of these three mechanisms  of  sulfate or
nitrate formation leads to the interrelationship of  chemistry and  micro-
physics.

     At issue in the literature on acid precipitation are  the relative con-
tributions to acidity of in-cloud, in-precipitation  generated acid and the
scavenging of precloud preprecipitation acid.  We have seen in  Section 1  of
this chapter that the homogeneous oxidation of S02 and N02 by HO radicals
leads to rates of H2SOt,. and HN03 formation which are not insignificant.
However, both laboratory and field observations suggest  that  solution  phase
mechanisms can be important additional sources of these  acids;  in  fact,
they may dominate.  Latest field measurements and analyses  (Lazrus et  al.,
1982; Scott, 1982) indicate that a substantial fraction  of the  sulfate and
nitrate found in precipitation results from acid production during the pre-
cipitation event.  In-cloud measurements by Hegg and Hobbs (1981)  also dem-
onstrate a rapid transformation of S02 to sulfate.   Analyses  of  field  aero-
sol data from plume experiments point to a rapid heteorogeneous  or aqueous
production of sulfate and nitrate (Van Valin  et al,  1981;  Parungo  and  Pues-
chel, 1980; Gillani et al., 1981; McMurry et  al., 1981).  In  deference to
these observations, a model which is to describe the long-range  transport
and deposition of acid and its precursors must properly  account  for the
role of particles (clouds, etc.) in the transformation and removal  of  acid.

     In view of the relevance of atmospheric  particles to  acid  chemistry,
the following review of the physical and chemical processes of  particles  is
presented, along with a description of their  previous treatments in atmo-
spheric models.  The significance of particle processes  has only recently
become a concern in long-range transport modeling.   Consequently,  the  ma-
jority of works cited herein pertains to small-scale modeling efforts  in
zero or one dimension.  It must also be pointed out  that,  until  the chem-
ical-cloud modeling work of Heikes and Thompson (1982) and Chameides and
Davis (1982), models of particle chemistry focused only  on aerosols or
precipitation.

     The nomenclature used in this section follows the definitions and con-
ventions given in the Glossary of Meteorology (Huschke,  1959).   Particles

                                     159

-------
as used here refer to solid or liquid material  found within  the  atmosphere
and as defined are composed of the subgroups aerosol, cloud  droplets,  and
hydrometeors.  Aerosols may be either wet, dry  (particulate),  or mixed
phase, and are generally assumed to be smaller  than a few micrometers  in
radius.  Cloud droplets are composed of water in either the  liquid  or  ice
phase and are small enough such that they are borne by the  atmospheric mo-
tions.  Hydrometeors are composed of water in either the liquid  (rain) or
ice (snow) phase, but are sufficiently large to have an appreciable fall
velocity and move, in part, independently of the surrounding air.   Hydro-
meteors which reach the earth's surface are termed precipitation, and  those
which evaporate before reaching the surface are virga.  The  latter  distinc-
tion has practical importance to the vertical redistribution of  acidic ma-
terial within the atmosphere and is discussed further below.   Figure 2.1
summarizes the spectrum of atmospheric particles and the physical processes
interrelating them.  It is beyond the scope of  this review  to  treat fully
the particles and mechanisms shown, let alone the chemistry  appropriate to
each.

     The development of a realistic acid deposition model requires  the in-
corporation of microphysics through appropriate parameterization schemes.
The formation of clouds and the development of  precipitation are discussed
in Sections 4 and 6 of Chapter IV.  For the purpose of chemistry, the  par-
ticle microphysics may be simplified along the  lines of Figure 2.2  (Scott,
1978; Scott, 1982; Molenkamp, 1982), which we call bulk process  parameteri-
zation.  Within a grid volume, there will exist gas-phase constituents and
the three types of particles.  Depending on meteorological  variables (e.g.,
vertical velocity, saturation, etc.), the particles are assumed  to  exist as
aerosol or mixtures of aerosol and cloud droplets or aerosol,  cloud drop-
lets, and hydrometeors.  A useable model, while providing for  descriptors
of the particle types within a grid volume in time, cannot  resolve  spatial-
ly or temporally the history of individual particles from their  point  of
inception in the atmosphere to their point of deposition.   Instead, the
particles may be treated as time dependent ensembles of aerosol, cloud
droplets, and hydrometeors (e.g., Scott, 1982).  However, parameterized
treatments of nucleation, (de)activation, and conversion  (dashed arrows
shown on Figure 2.2) will be required, in addition to those  of any  asso-
ciated meteorological model, to facilitate the  transfer of  particles and
their constituents from one particle class to another.  Each group  can have
its own mass and number density and unique chemical composition. Their
size distributions may be defined in terms of two parameter  number  density
distributions (e.g., Junge, Khrgian-Mazin, and  Marshall-Palmer). The  par-
ameters for these example distributions can be  defined in terms  of  total
number density and total mass density of each particle type.   Number den-
sity distributions such as these are necessary  to evaluate  the gas-particle
and particle-particle interactions shown in Figure 2.2.  A  few examples
will help illustrate this point.  Heikes and Thompson (1982) used a form of
the Junge aerosol distribution to examine the rate of NOy uptake by aero-
sol.  Heikes and Thompson (1982) and Chameides  and Davis  (1982)  have used
the Khrgian-Mazin distribution to describe the  rate of uptake  or release of
gases by cloud water.  Levine and Schwartz (1982) have evaluated the preci-
pitation scavenging rate of HN03 vapor by using the Marshall-Palmer, Best,
and Sekhon-Srivastava distributions for precipitation.  Beard  (1977) has
used both the Marshall-Palmer and Sekhon-Srivastava distributions to eval-

                                     160

-------
                             MICROPHYSICS
  I   ( Auto Conversion J
            t               f           1
        x	'"-	v           I Hydrometeors I
       (Activation)          I             I
                                            Cloudy Air
                                                                 CJoar Air
             Aqueous
             Stable
             Particle
  Hiomogeneous
  Nucleation
Heterogeneous Nucleation
    (Deliquescence)
Heterogeneous Nucleation
     (Sublimation)
                        Crystaline
                         Aerosol
                        Gas-to-Particle
                         Conversion
                             Mechanical Weathering \
                                     +
                                Bubble Bursting
Figure  2.1   Schematic diagram  illustrating major  particle  types
and the physical  processes which  interrelate them  in the troposphere.
Solid arrows indicate particle  growth and  production processes.
Dashed  arrows describe.mechanisms of particle size reduction.
Rounded boxes enclose process names.
                                     161

-------
o
  I
II     2
II     5
  I   _,
  I
        II. Aerosol
           a. dry
           b.aqueous
           c. ice
                          (de)activation


                            kb (II, III)
            I. Gas
                                             I. Cloud
                                               a.aqueous
                                               b. ice
                                           IV. Hydrometeor
                                              a. aqueous
                                              b. ice
      I
      In
>     ii
=     'I
                                                              o
     Figure 2.2   Conceptual design of phase speciation and
     particle mechanics within an air parcel.   Solid arrows
     depict theoretically resolvable material  exchanges
     between classes.  Dashed arrows represent processes
     possibly requiring parameterization,  k's  are  the material
     exchange coefficients described in the text.
                                162

-------
uate particle-particle scavenging rates. Lastly, Clark  and Hall  (1982)  have
used log-normal distributions to parameterize stochastic collection  and the
development of warm rain.

     Evaluation of the interaction coefficients, k's  in Figure 2.2,  is  an
ongoing research effort.  A complete set of formulations for  them  is  not
available at this time, but one set will be forthcoming soon  from  Batten e
Northwest Laboratories (Hales, personal communication,  1982).  However,
their usage and their first-stage development can be  envisaged along  the
lines suggested by Scott (1978, 1982) and Fisher (1982).  The exchange  of
gases between the atmosphere, Phase I,  and the  particle types, Phases -II,
III, and IV, can be predicted through the equations governing the  diffusion
of a gas to a particle.  The rate at which molecules  diffuse  to  and  stick
upon a particle is proportional to the  vapor gradient evaluated  at the  par-
ticle surface (a) and at an infinite distance away, Cj(I») -  C-j(Ia).
Factors controlling the gradient will be discussed  further below.  The
proportionality constant for condensation is kc(I,j)  and for  evaporation
is ke(I,j), where j indicates either aerosol (II),  cloud particles (III),
or hydrometeors (IV).  kc(I,j) in this  formulation  is defined equal  to
ke(I,j).  One form of kc(I,j) has been  developed from a consideration
of first principles by Heikes and Thompson (1982).  It is very similar to
that used by Petersen and Seinfeld (1980) and Chameides and Davis  (1982),
and is given by
                                  a2(j)
                                        k..(a)n.(a)da
where kjj is the rate of diffusion of the  ith  vapor  species  to  a  jth  type
particle of radius a, nj(a) is the number  density  of jth  type particle
whose radius is between a and a + da, and  aj(j)  and  a2(j)  are the radius
limits of j type particles.  The rate of diffusion,  k-jj(a),  was shown by
the previous authors to be dependent on the  diffusivity of the  ith  species
in air, the sticking coefficient of the ith  species  on the jth  particle,
and the radius of the jth particle.  Of all  these  terms,  the most crucial,
yet least well-known, is the sticking coefficient  (Heikes  and Thompson,
1982; Chameides and Davis, 1982).  Figure  2.3  illustrates  the variation  in
kjj(a) with particle size for selected vapors.   kc(I,i) is most sensi-
tive to the sticking coefficient at the smallest particle  sizes such  as
aerosols or the small end of the cloud particle  population.  A  few  typical
values for kc(I,j) or kp(I,j) can be found in  Table  2.11  (p. 214).   It
should be noted that kc(I,j) as treated above  represents  a first-order
rate constant.

     The collection or accretion of small  particles  by large particles  is
treated through the ka(i,j) interaction coefficients, where  i indicates
the small particle type, j indicates the large particle type, and the al-
lowable combinations are (II, III), (II, IV),  and  (III, IV).  These coeffi-
cients are analogs to aerosol -precipitation  or cloud particle precipitation
scavenging coefficients discussed by SI inn (1980), Beard  (1977),  and  Berry
(1967).  The accretion coefficients might  be described by
                                     163

-------
ro
 O
 L?
  O
 o
 o
      -2
      -4
      -8
     -10
             	ac=0.l
             	  ac=O.OI
             	ac= 0.001
             Aerosol, Particle   ]   -^fiO^Dropierx^|Hydrometerj^^
        -6        -5        -4       -3       -2

                                LOG|0 a, cm
-I
             Figure 2.3   Variation of the vapor-to-particle diffusion
             rate, 4ira FvVD, as a function of particle radius, a.  Each
             curve represents a aiven sticking coefficient value, ac
             D,  T and P are vapor diffusivity, temperature and total
             pressure, respectively. Particle names along abscissa
             indicate normal size range of that particle type.
                                   164

-------
                   a2(j)   a2(i)           m(a.)
      ka(i,j)  =  /       /       K(ajfa1)   H]  n(a.)  r\(a.)  da.  da.
where K(aj,a-j) is the collection kernel  for  a jth  type  particle  of  ra-
dius aj colliding with and assimilating  an ith  type  particle  of  radius
a-j, m(af) is the mass of water on an  ith  type particle  of  radius aj,
Mj is the total mass density of ith type  particles,  and n(aj)  and
n(a-j) are the respective number of j  or  i type  particles whose radius
lies between a and a + da.  The collection kernel  is  involved and includes
the effects of Brownian diffusion, electrostatic forces, relative sedimen-
tation, and particle scale turbulence, which are all  dependent upon ith  and
jth particle sizes and properties of  the  atmospheric  medium.   Both  empiri-
cal and theoretical evaluations of K(aj,ai)  are available  (e.g., Jonas,
1972; Klett and Davis, 1973, Lin and  Lee, 1975; de Almeida, 1977).   Again
it should be noted that ka(i,j)'s describe a first-order process.

     The last type of interaction coefficient describes the collisional
breakup of a hydrometeor resulting from  hydrometeor-hydrometeor, hydro-
meteor-cloud particle or hydrometeor-aerosol collisions.   In  this  breakup
process, a fraction of the mass involved  in  a particle-hydrometeor  colli-
sion is transferred to particle types  smaller than hydrometeors  (for a
complete discussion, see McTaggart-Cowan  and List, 1975, or Pruppacher and
Klett, 1978).  Consequently, material  which might  have  been deposited at
the surface is resuspended at lower altitudes in the  atmosphere. The
breakup and redistribution of hydrometeor mass  is  one of the  least  theore-
tically understood processes in precipitation physics and  must be evaluated
empirically.  As a first guess or approximation to k^d'jj), the  accretion
coefficient description could be applied  with an additional factor  which
describes the number of collisions between particles  which results  in the
reformation of aerosol or cloud particles (e.g., Gillespie and List, 1978;
Passarelli, 1978).

     The interaction coefficients can  be  grouped together  and used  to de-
velop a set of predictive equations for  the  concentrations of species with-
in the assumed four phase categories  of  an air  parcel.   Let c(i) be the
concentration of a species in phase i, molecules cm~3.   It is common to
define the particle phase concentration  in terms of  moles  per kilogram of
liquid water and let c' be that quantity.  If WA(i)  is  the liquid water
content, g m~3 of air, for the ith particle  type,  then


                        c'(i)  =  109c(i)
where n0 is Avogadro's number  and the  109  is  a  unit  conversion  factor.
For condensation/evaporation interactions,  it is  necessary  to  define  the
thermodynamic equilibrium-concentration of  a  gas-phase  species  at  the sur-
face of each particle type.  Let c*(i) be  this  quantity.  The  net  rate  of
loss or gain for c(I) through  condensation  or evaporation with  all  particle
types can then be expressed

                                     165

-------
             c/e
                                                         ke(I,IV)c*(IV)
                  - [k(I,II) + k (1,111) + k (I,IV)] c(I).
                      v.          I*           C
The rate of change in a particle phase species concentration (c(i), i = II,
III, or IV) due to condensation/evaporation is
     3c(i)
       3t
               - k
             c/e
The rate of change in the particle phase species concentration through par-
ticle-particle interactions is type dependent.  Values for the three parti-
cle types are:
             a/b
                  - k
                                        kb(II,IV)c(IV)
      3t
             a/b
=  k (II,III)c(II) + k,(III.IV)c(IY)
    u                 U



- k(III,IV)c(III) - k. (II.IIDcdII),
   u                  D
and
             a/b
                    kb(ii,iv)c(iv) - kb(in,iv)c(iv).
b.  The particle sulfate formation mechanism

     Aerosols, cloud droplets, and hydrometeors serve not only as pollutant
storage sites (aerosols and cloud droplets) and transport mechanisms (hy-
drometeors), but also provide a medium upon which pollutant transformation
can occur.  The solid-liquid, solid-gas, and liquid-gas particle interfaces
provide surface sites upon which heterogeneous reactions can occur (see Ta-
ble 2.1).  The hygroscopic nature of the majority of particulate particles
leads to the presence of suspended liquid water when humidities exceed
- 60%, thereby making aqueous solutions present within which liquid-phase
reactions can occur.  The conversion of S(IV) to S(VI) in the atmosphere is
thought to occur, in part, through these mechanisms.  Since S(VI) is one of
primary acid species, a description of its particle chemistry is necessary.
                                     166

-------
                 Table 2.1
       HETEROGENEOUS INTERFACES
  Gas Phase
Aqueous Phase
Paniculate Phase
   Ice Phase
             Chemical Examples
Interface
1
2
3
4
5
6

Species
soot, S02, H20, N02, H2SO,,
N0y, H20, HN03
NO, H20, HN02, HN03
soot, H20, S02, H2SO,,
?
7

Reference
Gofer, et al . (1981)
Gofer, et al . (1980)
Chang, et al . (1981)
Britton and Clarke (1980)
Baldwin (1982)
Heikes and Thompson (1981)
Thompson and Heikes (1982)
Heikes and Thompson (1982)
Fezza and Calo (1982)
Benner et al . (1982)
7
7

                     167

-------
Carbonaceous particles and acid generation

     The mechanism of S(IV) oxidation on particulate  surfaces  in  the  atmo-
sphere is not well understood.  Carbonaceous particles have been  shown  in
the laboratory to absorb S02 until the S02 active sites are filled.   The
specific quantity of S02 which saturates the surface  is highly  variable,
with the greatest variation due to the source of the  carbon particles (Tar-
tarelli, 1978).  Experimental parameters such as humidity  and  NOX concen-
tration have been shown to influence the amount of sulfur  sorbed  (Gofer et
al., 1980 and 1981; Chang et al., 1981).  Their effect on  S02  absorbance is
thought to be brought about by the freeing of active  sites through S(IV)
oxidation to S(VI) and a subsequent migration of the  sulfate to other parts
of the surface.  Not all of the sulfate is migratory.  Consequently,  at
long exposure times, all sites eventually become poisoned  and  the amount of
sulfur absorbed reaches a maximum.

     Indirect atmospheric evidence has been interpreted to show that  S02
absorption and sulfate formation does occur on carbonaceous particles.
Morphological studies of aerosol from multiple origins show that  in some
circumstances the aerosols which contain sulfate also have particulate
carbon inclusions (Ferek, 1982).  Yet not all carbon  particles  show signs
of sulfate, nor do all sulfate-containing aerosols have carbon  inclusions.
The electron microscopy techniques used in these studies to observe carbon
are difficult to perform and easily misinterpreted.   Hence, there is  a
question as to the reliability of the analysis techniques  and  the results
there obtained.

     The results are also subject to a different interpretation.   The con-
version of S02 to sulfate is known to occur homogeneously  in the  atmosphere
(see Section 1 of this chapter).  The product sulfuric acid could result in
new particle formation (nucleation), or it may diffuse to  and  stick to  pre-
existing particles (carbon, in this case) (see Middleton et al.,  1982).
This stochastic event will result, through the hygroscopic nature of  sul-
furic acid, in the increased absorption of water vapor by  this  particle
with respect to the other particles.  The condensation of  water preferen-
tially increases the likelihood of this particle to acquire additional  sul-
fate.  The physical increase in particle size increases its surface area
and the rate at which sulfuric acid vapor will condense.   The  particle  li-
quid water also allows for aqueous S02 oxidation to occur.  In  this manner,
a plume which initially contains S02 and carbon particles  as contaminants
could in time contain sulfuric acid particles without carbon inclusion  (nu-
cleation), aerosol with both sulfate and carbon inclusions (sulfuric  acid
vapor and water vapor absorption on particulate carbon), and particulate
carbon without sulfate.  Empirically, it is not obvious whether dry car-
bonaceous particles are important to tropospheric sulfate  production  or
whether they are of negligible impact, although sensitivity studies would
suggest the latter (Moller, 1980).

     Observations of S(IV) and S(VI) oxidation in the non-cloudy  atmosphere
exhibit both a diurnal (Forrest et al., 1981; Gillani et al.,  1981) and
seasonal character.  The maximum rates of conversion  are found during day-
light hours in summer and have been used to illustrate the importance of
photochemical reactions (Gillani et al., 1981; McMurry et  al.,  1981).  S02

                                     168

-------
transformation at night through gas-phase reactions  is  too  slow  to  account
for nocturnal ly-observed rates, and it has been necessary to  invoke  hetero-
geneous and aqueous reaction mechanisms.  The  importance of a gas-solid  re-
action does not appear viable, although some would argue for  the occurrence
of the parti cul ate carbon process just described; it has been necessary  to
assume that aqueous reactions are responsible  for sulfate formation  under
nocturnal conditions and partially responsible during daylight hours.

Aqueous phase reactions leading to acid formation

     The search for aqueous reactions which could account for the measured
sulfuric acid formation rates has evolved rapidly over  the  last  15 years.
The primary step in this process is the dissolution  of  S02  in water  which
is governed by the following reactions:
                      S02(g) + H20(Z)  Z  S02.H20(a),                  (1)

                      S02.H20(a)  Z  H+(a) + HS03-(a),                (20)

and

                      HS03-(a)  *  H+(a) + S03=(a).                   (21)
     The total aqueous S{IV) concentration  in  equilibrium with  an  S02  par-
tial pressure of p(S02),(atm) is equal to


    [SUV)]  =  p(S02)K,  {1 + - ^0 - + - *20 K21 - }   (A)
                      1      Y(H+)Y(HS03-)[H+]   Y(H+)2Y(S03=)[H+]2

where K7- is the equilibrium constant  for reaction  i  (M  atnr1 or M),
y(j) is the activity coefficient of the jth  ion, and the  [  ]'s  denote  a
molar concentration.  The equilibrium constants and  activity coefficients
are temperature dependent.  In general, the  solubility  of a gas such as S02
increases with decreasing temperature, and  the dissociation equilibrium
constants increase with  decreasing temperature.  The degree of  dissociation
is  strongly dependent upon solution ionic strength and  the specific mixture
of  anions and cations (see Clarke, 1981; Maahs, 1981; and Heikes,  1983).
In  dilute solutions, the ion activities approach unity.  Between ionic
strengths of 0.5 molal and 5.0 molal, the activity coefficients pass
through a minimum value  substantially less  than unity.  At high ionic
strengths, the activity  coefficients  increase  and  eventually plateau.   The
range in activity coefficient values  is conservatively  between  0.01 and
20.0, with the highest values associated with  concentrated aerosol  salt
solutions, the lowest values associated with cloud droplets of  moderate
concentration, and the midrange values associated  with  all three aqueous
particle types.

     The aqueous partitioning of S(IV) between the hydrate of S02  (S02-
H20), bisulfite (HS03~), and sulfite  (S03=)  as a function of pH is  shown
in  Figure 2.4.  Also shown is the total equilibrium  concentration  of S(IV)
calculated from (A) as a function of  pH for  25°C,  unit  activity coeffi-

                                      169

-------
                               '            /
                                  [s(E)]xlO-12
                                          /
             34567    8   9   10  II  12
                                                      1-6  -
                                                      r9
Figure 2.4   Total  aqueous  S(IV) concentration is
represented by the  dashed line and S02'H20, HSOjj and
503 mole fractions  are  shown  by the solid lines as a
function of pH at 25°C,  SC>2  gas-aqueous equilibrium
is assumed.  S02  partial pressure is set at 10~9 atm.
                          170

-------
cients, and S02 partial pressure of 10~9 aim  (- 1 ppbv).  The specific
form of S(IV) in solution and the total concentration of S(IV) are  very
important in calculating aqueous rates of sulfuric acid formation.  De-
pending on oxidant and reaction mechanism, the speciation of S(IV)  will
determine for a given quantity of S(IV) whether the sulfate production is
relatively small or large.

     The principal oxidizing species involved in aqueous sulfate  production
are believed to,be oxygen, ozone, and hydrogen peroxide (Beilke and Graven-
horst, 1978).  With the recent experiments of Heikes et al. (1982), Zika
and Saltzman (1982), and modeling studies of Chameides and Davis  (1982),
possible oxidation reactions between S(IV) and aqueous neutral and  ionic
radicals must be considered.  The significance of aqueous radical mech-
anisms is still in the speculative stage.  Tables 2.2 - 2.5 summarize the
mechanisms and rate constants for S(IV) oxidation by 02, 03, and  H202
available in the literature.  Table 2.6 presents a few of the mechanisms
and rate constants for oxidation by aqueous radicals.  Tables 2.7 and 2.8
list pertinent mixed-phase and aqueous sulfur chemistry.

     The salient features of the aqueous sulfate production reactions will
be discussed here.  Only those developments which have occurred later than
about 1977 are described (see discussions by  Beilke and Gravenhorst, 1978;
Hegg and Hobbs, 1978; and Peterson and Seinfeld, 1980 for descriptions of
earlier work).  First, specific features of oxidation reactions involving
02, 03, and H202 with and without catalysts are presented.  Second, the
proposed reactions of S(IV) with nitrogen compounds, organics, and  radicals
are outlined.  Lastly, a comparison of some of these reactions is made un-
der typical tropospheric conditions.  Reaction numbers refer to Tables 2.7
and 2.8.

     S(IV) oxidation by Q2.  Scott and Hobbs  (1967) demonstrated  that the
uncatalyzed aqueous reaction between dissolved oxygen and sulfur  dioxide
was insufficient to generate appreciable amounts of sulfate in atmospheric
water under normal conditions.  S(IV) appears to react with oxygen  as
S03 = through the overall reaction:

                      S03=(a) +-02(a)  *  SOiT(a)                  (59)
                                2
The rate constant for (59) is small for atmospheric  conditions  (k5g[02]
- 2 x 10"5 s"1).  Also, at normal atmospheric water  pH's  (3  to  5.6),  the
concentration of S03= is below 10~6 M and  the rate of  sulfate production
via (59) is less than 2 x 10'11 M s   .  Reaction  (59)  is  catalyzed  by dis-
solved metal ions.  Ions of iron, manganese, and  copper have been identi-
fied as catalysts, with there being some debate as to  the effectiveness of
copper (Martin et al., 1981a; Petersen and Seinfeld, 1980; Huss  et  al.,
1982a,b).  Martin et al. (1981a) and Huss  et al.  (1982a,b) have  found that
vanadium, cobalt, scandium, titanium, chromium, nickel, zinc, and lead were
not effective catalysts.  For all practical purposes,  the uncatalyzed 02
reaction (59) can be ignored in modeling efforts.

     S(IV) oxidation by 03.  The atmospheric relevance of aqueous ozone
oxidation of S(IV) has been investigated since  about 1974.   Larson  et al.

                                     171

-------
         Table 2.2.  Rate Constants  ks for the  Liquid-Phase  Oxidation of S02  by 02
                                            dt
               ks(s-M
     Coranents
    Reference
             1.7xlO-3
             3x10
                 ,-3
             3.5xlO-3

             3.7xlO"3-O.SxlO-3


             6xlO-3-0.6xlO-3
             0.013  + 59[H*]
                         0-S
pH 6.8, 25°C from measure-
 ments of Van den Heuvel
 and Mason (1963)

25'C
pH 7, 25*C

pH 4-6, 2S°C with 0.6xlO-3
 at pH » 6
                      k,H*1/*
              ki *  (4.8 ; 0.6)xlO-3
                   s-1 (298'K)

              k2 '  (4.9 5 1.0)
                   S-1 M-1/2

              k, »  (3.9 ? 0.6)xlO-12
                   s-1 M atn-1

             5.66X101" exo
              (-13,180 T-1)
             < 10
                 -5
pH 4-12, S-25*C,
 p(0z) * 0.11-1.0 ata
pH 4.7, 23-42'C


pH 0-3, 2S'C
Larson et al. (1978)
Penkett et al. (1979)


Martin et al. (1981a)
Peterson and Seinfeld  (1980).

     (aThe  value  given  in  the  table  has been  computed for the  pH range stated by  Beilke and
 Gravenhorst (1978).

     (b)Bei1ke and Gravenhorst (1978)  conclude that the  value  of McKay deduced  from  the
 measurements of Fuller and Crist  (1941)  is  unrealistically high because  Fuller  and  Crist
 did not account for  the variation  in pH  during  the  source of the  reaction.
                                                     172

-------










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-------
Table 2.6.  Liquid-Phase Oxidation of  S02 by Oxides of Nitrogen  and  Aqueous  Radicals
Reaction
NO + SUV) » S(VI) + ?
N02 + SUV) * S(VI) + ?
N02 + SUV) » S(VI) + ?
N(IH) + SUV) • S(VI)
+ I N20 + i H20
HUH) + suv) + s(vn
Rate Constant ' Comment
< 10-2 M-1 s-1 pH <_ 3; T = 25'C
No rate given Chain reaction scheme
H02 + H20 * K02- + H+ + HO
N02 + S03* » N02- + S03-
HO * HS03- » H20 + S03-
HO + S03- * H* + SO^"
< 2.Sxl07 M-1 s-1 From comparison study
of Nash (197U) and
reactivity of o-
methoxy phenol
with N02
142 [H*]1/2 pH =" 0.6-3.1; T « 25*C;
no catalysis by Fe, Mn,
M-; s-1 or VO
Coop! ex Mechanism
Reference
Martin et al.
(1981b)
Nash (1979)
Lee and Schwartz
(1982)
Martin et al .
(1981b)
Chang et al .
(1981)
                                  Rate controlling step:
                                  (HN02 + NO2-) + 2(S02-Ag + HS03-
                                     HOM(S03)2« * H20
                                  with

                                                        [H+]2 [nt.}
                                                         H2  [H*] [N02-] [HSO,-]
                                                         H3  [N02-]  [HS03-]2
                                  where
                                  k, • SxlO5 M-2 s-1; T * 23'C
                                  kz » 3.7xl012 exp  (-6100 T-1) M-2 s
                                                                  '1
                                   k3 * 9.0x10-" exp  (2.1
                                   and I * Ionic strength
                                                           -2  -1
                                                    182

-------
Table 2.6.  Liquid-Phase Oxidation of S02 by Oxides  of Nitrogen  and Aqueous  Radicals
                                    (continued)

N03-
HO +
HO +
H02
H02
H2PO
H
co3-
co3-
02-
o2-
o- +
e--»
«-•*
Reaction
+ S(IV) - S(VI) + ?
HS03- *
S03" *
«• HS03- *
+ S03» *
„ + HS03- »
2PO»- + HS03
+ S03S « C03a + S03-
+ so3- * co2 + sok-
•f HS03- *
+ S03« *
S03= *
q * S03- »
q + HS03- « H + S03*
Rate Constant
< 10-2 M-1 s"1
9.5xl09 M-1 s*1
S.SxlO9 M-1 s-1
- 105-107 N-1 s-1
- 105-107 M-1 s-1
2.7xl08 M-1 s'1
IxlO7 M-1 s-1
SxlO8 M-1 s-1
- 10* -10s M-1 s-1
- 10*-10S M-1 s-1
3xl08 M-1 s-1
< 2xl06 M-1 s-1
2T107 M-1 S"1
Comment
pH <^ 3; T » 25'C
T - 20-25'C
T - 20-25'C
Estimated from comparison
of HO, H02, and H202 rate
constants for reactions
with coMKn second species
pH « 4; T « 20-25*C
pH » 11; T » 20-25'C
pH » 9.6; T » 20-25'C
Estimated rate
Estimated rate
pH = U; T » 20-25'C
alkaline; T » 20-25'C
pH » 8.0-8.5; T « 20-25'C
Reference
Martin et al.
(1981b)
Fartiatazlz
and Ross (1977)
Farhatazlz
and Ross (1977)
Helkes et al.
(1982)
Ross and Neta
(1979)
Ross and Neta
(1979)
Ross and Neta
(1979)


Ross and Neta
(1979)
Ross (1975)
Ross (1975)
                                        183

-------






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(1978), Penkett et al .  (1979), Martin  et  al .  (1981a),  Harrison et al .
(1982), and Maahs (1982) have performed the most  recent  studies on the
reaction:
                  Oa(a) + s
-------
et al. measured the rate constant for

                    N02-(a) + S(IY)(a)  }  S(VI) +  ?                  (71)

and observed N02 as a product.  Given that (71) does  occur  in  atmospheric
water and some specific environmental conditions, Chang et  al.  (1981)  con-
cluded that significant amounts of sulfate will be  produced in  cloud  water
from an aqueous HONO - S(IV) reaction.  However, Martin et  al.  (1981b)  have
concluded that this process in aerosols will not be a major mechanism of
sulfate production.  In addition to N02~, Martin et al. (1982b)  determined
that NO, N20, and N03~ do not react with aqueous S(IV) under their  experi-
mental conditions.

     It should be noted as well that the oxides of  nitrogen, principally
N02, will oxidize S02 to sulfate upon soot particles  (Cofer et  al.,  1980;
Cofer et al., 1981; Britton and Clarke, 1980); however, Baldwin  (1982)  did
not observe this reaction.  The particulate odd-nitrogen-sulfur  dioxide
reactions just described provide an unknown and unquantified link to  the
interactions between NOX and SOX in addition to homogeneous HO  competi-
tion discussed in Section 1 of this chapter.

     It has been speculated that an aqueous atmospheric reaction between
formaldehyde and S(IV) occurs, since ambient measurements have  shown  the
coexistence of both S(IV) and H202 in precipitation samples (Richards et
al., 1983).  H202 is expected to oxidize free S(IV) in solution. H202 does
not, however, react with the formaldehyde bisulfite complex.  The analysis
technique used to measure S(IV) cannot distinguish  free S(IV)  from  organi-
cally-complexed S(IV).  Consequently, the coexistence of S(IV)  and  H202 in
rain water may indicate the presence of S(IV) complex.  If  true,  then in
regions of high H2CO concentrations, part or all of the S(IV)  available for
aqueous oxidation may be unable to produce sulfate.  Key issues  in  this ar-
gument are the relative rates at which free S(IV) is  oxidized  or complexed
in droplets, the rates at which H2CO, S02, and oxidants are delivered to
droplets, and the relative atmospheric concentrations of these  species in
space and time.

     The last research area which bears on the liquid phase oxidation of
S(IY) is the radical - S(IV) reaction; this has been  a topic of  considera-
tion only since mid-1981.  The occurrence of radicals in atmospheric  water
was not considered important until Heikes et al. (1982) and Zika and  Saltz-
man (1982) found that 03 when bubbled through water produced H202.  The
precursors of H202 are thought to be HO, 02~, and H02.  These  radicals re-
act rapidly with most species in solution, and, in  particular,  they  react
extremely fast with S(IV) (Farhatazis and Ross, 1977).  The exact mechanism
of HO and H02 production through aqueous ozone decomposition has not  been
established soundly, although unsaturated organic material  and  hydroxide
ions do appear to be potentially important reactants. The  fundamental
question yet to be answered is "where do aqueous HO and H02 and  other
radicals come from?"

     There are at least seven potentially significant pathways  of aqueous
radical production.  One of these, aqueous ozone decomposition,  has  already
been discussed.  The others are:

                                     193

-------
(1)  The diffusion of gas phase photolysis products (e.g., 0, HO, H02,
     R, RO,  and R02) to particle surfaces.  This has been shown in
     theory  to be significant during daylight hours (Chameides and
     Davis,  1982).

(2)  Direct  deposition and absorption of energy (e.g., u-v, visible,
     and cosmic radiation, on particles).  The primary products of
     water radiolysis are H,  HO, 0, H0~, 0", e--H20, H+, or H20+, and
     the secondary products are H02, 02~, or H202.  Other species
     which could act as sensitizers are N02, N03, 03,  HONO, N02",
     N03~, transition metals, and organometallics.  The relevance of
     this mechanism is unknown, but it seems to be low at this writ-
     ing.

(3)  Deposition of electrons  or ions to particles.  Cosmic rays pro-
     duce -102 ion pairs cm"3 s"1 in the troposphere and are thought
     to be one of the principal charging processes leading to light-
     .ning (Wagner and Tel ford, 1981).  Lightning strokes and cloud
     corona  provide strong but very localized sources of ions and
     radicals, as evidenced by observations of ozone and lightning
     spectra.  A correlation  between cloud electrical  activity and
     H202 water concentration has been qualitatively noted (Kok,
     1982).   Also, in aqueous electron beam experiments, primary pro-
     ducts are aqueous radicals and radical ions.  Electrochemical
     reactions in clouds may  constitute a significant source of S(IV)
     oxidants, but significant research is needed to evaluate this
     possibility before any form of this process could be incorporated
     into a  model .

(4)  Organic autoxidation in  aqueous solution.  Reactions of the form

                       RH(a)  + 02{a)  ->-  products

     are known to occur under certain conditions with products includ-
     ing HO, H02, 02~, H202,  R, RO, R02, ROOM, and carboxylic acids.
     Galloway et al . (1982),  Dawson et al .  (1980), and Farmer and Daw-
     son (1982) have measured gas phase and aqueous formic and acetic
     acid in the atmosphere.   Lazrus (personal communication, 1982)
     has found a non-H202 interference in the measurement of aqueous
     H202 and has tentatively attributed this to organic peroxides.
     Graedel and Weschler (1981) have also speculated as to the impor-
     tance of organic species in aqueous atmospheric chemistry.  It
     must be concluded, however, that once again there are insuffi-
     cient data available to make an assessment of this process.
(5)  Organic oxidation by species other than 02, 03, and C^ were
     suggested by Heikes et al. (1982) to be H202 precursors.  Organic
     material may also be oxidized by N02 or N03 in solution and  re-
     sult in the same products listed in (4) above.  Aqueous PAN  de-
     composition is expected to result in N02~ and other products
     (Stephens, 1967).  Spicer et al. (1981) have observed nitrate
     formation.  The difference in products may result from N02~  oxi-
     dation by intermediate organic material from PAN decomposition.

                                194

-------
          Again, the relevance of this chemistry to sulfate production  is
          unknown.  Oxidation of S(IV) by a similar reactive species,
          H02N02 (peroxynitric acid), is also possible but unevaluated.

     (6)  Nitrate radical deposition onto particles.  The diffusion  of  N03
          to particles is discussed in Section 2.2 and assumed to  result in
          N03- and radicals  (Heikes and Thompson, 1982).  The electron  af-
          finity of N03 is greater than that for Cl~ and other ions  common
          to atmospheric water, and Daniels (1969) experimentally  observes
          N03 -»• N03".  This  process, while important for N03~ production,
          may also be very important to radical initiation and significant
          to any modeling effort (see reactions in Table 2.9).

c.  Comparison of aqueous S(IV) oxidation mechanisms

     The myriad solution reactions presented are not all relevant  to atmo-
spheric chemistry.  The specific mechanisms, rate constants, and oxidant
concentrations will limit the effectiveness of some mechanisms to  generate
sulfate with respect to others.  This can be demonstrated by assuming con-
ditions appropriate to a cloudy or precipitating atmosphere and calculating
the instantaneous aqueous production rate of sulfate.  Then by further  as-
suming atmospheric liquid water contents, the aqueous reactions may  be  com-
pared with the gas-phase rates of sulfate production.

     The oxidation of sulfur in aqueous solutions is strongly dependent on
pH and has led to discussions of ammonia "catalysis" (McKay, 1971) and  acid
inhibition.  Acid inhibition results from (1) the decreased solubility  of
SO? with increasing acidity, (2) shifts in S(IV) speciation with changes in
[H*] (most dramatically at pH = pK(20) and pH = pK(2D), and (3) apparent
changes in the oxidation mechanism as evidenced by rate constant dependen-
cies on [H+3.  Figure 2.4 illustrates the effect of [H+] on S(IV)  solubil-
ity and the partitioning of  S(IV) between S02«H20, HS03~, and S03=.   Ta-  .
bles 2.2 - 2.6 list rate constants for S(IV) reaction with 03, H202, and a
few other possible oxidants which show a marked dependence on [H*].

     Figure 2.5 shows the combined effects of the above chemistry  on the
aqueous rate of sulfate production.  Each line depicts the rate for  a given
oxidant under the following  assumed conditions:
     T = 15 or -5°C, P(S02) = 5xlQ-9 atm, [S02*Aq = P(S02) K(l),
     P(S02) K{1) K(20) [H*]-1, [S03=] = P(S02) K(l) K(20) K(21)
     P(03) = 5xlO;8 atm, [03] = P(03) K(ll),  [soot] =  10'3 g  I'1,  k(R)
     [HO] = 5xlO-3 s -1, P(HONO) = 10-10 atm, [HONO] = P(HONO) K(R3),
     [NO,-] = P(HONO) K(3) K(24) [H+]-1, [Fe+++] = 10~5 or 10'7 M,
     [Mn*+] = 10-1[Fe+-H']f [H202] = 10"5 M, and [H+] = 10° -  10~7.

The equilibrium constants, K(i), are given in Table 2.7.  The oxidation
rate constants are summarized in Tables 2.2 - 2.6, and are taken to  be:

     k(59) Penkett et al.  (1979), k(60) Maahs (1982),  k(61) Martin
     and Oamschen (1981), k(59') iron catalyzed Martin et al. (1981a),
     k(59') soot catalyzed Chang et al . (1981), k(62)  Farhataziz and
     Ross (1977), and k(79) Oblath et al . (1980) or Martin et al .  (1981)

                                     195

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            Aqueous Rates of Sulfate Production
           sk
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                             3     4

                                 pH
                                                  6     7
         Figure 2.5   Aqueous sulfate production rate as a
         function of pH   (see figure key on following page).
                             198

-------
                                           Figure  2.5

                                           Figure  Key
         Label           Mechanism


          a        SO,' + I 02 + SO,,'


          b        S(IY) +  Q3 « S(¥I) + 02

          C        SUV) +  H202 * S(VI) * H20

                      [H202] « 10*s N


          d        S0a« + 1 Oj » SO,."


          e        S(1V) +  Oj » S(VI) + 02

          f        S(IV) *  H202 * S(VI) + H20

                      [H202] « 10-5 H
   [Fe**] « 10-5 M

   [Mn**] * 10-6 M


SO," + i 02 Fe**' *** SO,,'
      2

   [Fe**] « 10-7 M

   [Mn**J > 10-8 M


           Soot  „, ,
Temperature

    15*C


    15*C

    15*C




    -5'C
                   S(I¥)
                      S(VI) + i M20 + H20
                             2
                   SUV) + N(III) -
   S(VI) » i
         2
                                        SO,,'      15*C
                                                 15*C
                                                 IS'C
   [Soot] » 10-3 9 f1

SUV) +  HO(H02) « S(VI) + ?      15*C

   k[OH] • k[H02] - SxlO-3 s-1
                                                  15'C
                                                 1S«C
                                             Rate Constant Reference


                                             Penkett et al. (1979)


                                             Maahs  (1982)

                                             Martin and Danschen (1981)




                                             Penkett et al. (1979)


                                             Maahs  (1982)

                                             Martin and Danschen (1981)
                                              and activation energy of
                                              Penkett et al. (1979)
                                              for pH » 4.6


                                             Martin et al. (1981a)
                                                                Martin et a). (1981a)
                                                                Chang et al. (1981)
                                                                 FarhatazU and Ross (1977)
                                                                001ath et al. (1980)
                                                                Martin et a). (1981a)
                                    M20
Gas-aqueous equilibrium  Is assumed  for S02, 02,  03,  and  HONO.   Partial pressures of  Oz,
S02,  03,  and  HONO  are assumed  to be.  respectively,  0.2,  10'9,  SxlO"8, and 10'10  atm.
Aqueous concentrations of H202,  Fe**,  and  Mn**,  and  soot  are given under  the mechanism
listed above  where  appropriate.
                                                 199

-------
The rate constants chosen reflect most  recent measurements  and  analyses,
and their selection here is not meant to be judgmental with  respect  to  the
accuracy of the other rate constants presented.  The Oblath  et  al.  (1980)
expression for k(79) is determined under experimental conditions  atypical
of atmospheric water and includes terms which are  probably  unrealistic  at
more normal atmospheric concentrations  of S(IV) and N(III).  The  uncertain
region is shown as a dashed curve in Figure 2.5. .

     The assumed reaction conditions are selected  to represent  typical  con-
centrations over eastern North America.  The aqueous H202 concentrations
are not calculated from a consideration of vapor-aqueous equilibria  since
gas-phase measurements of H202 suffer from sampling errors.  H202 measure-
ments in atmospheric water do not exhibit the same errors,  are  consequently
more reliable, and the [H202] value chosen is representative of the  ambient
aqueous measurement in cloud and rain water (Kok,  McLaren,  and  Lind,  per-
sonal communication, 1982).  Measurements of MONO  or N02~ are not available
for the eastern United States, and P(HONO) is taken to be approximately
one-tenth the value measured in Southern California (see Platt  et al.,
1980b; Liljestrand and Morgan, 1981).  The assumed concentrations of  iron,
manganese, and soot are chosen to bracket measurements in precipitation.
The concentration of HO in solution is  taken from  the steady-state cloud
model results of Chameides and Davis (1982).  It should be  pointed out
that, aside from the catalytic sulfur oxidation reactions {58'),  the  other
reactions are all first order with respect to S(IV) and oxidant.  Thus, to
examine the effects of different assumed species conditions  on  the  rate of
sulfate production, one need only multiply the rates shown  in Figure  2.5 by
an appropriate factor.

     It is readily apparent from Figure 2.5 that the rate of sulfate  pro-
duction is dominated by H202 at solution pH's < 4.5 (curve  c) and by  03 at
pH's > 4.5 (curve b).  If the Oblath et al. (1980) rate constants for the
HS03~ - N02~ reaction can be extrapolated to low pH, then sulfate produc-
tion at pH s < 2 will depend on MONO (curve k).  This extrapolation  does
not seem valid in light of the measurements by Martin et al. (1981b)  at
pH's < 3 which predict rates of sulfate production six orders of  magnitude
lower at pH=3 and eleven orders of magnitude lower at pH=0  than the  Oblath
extrapolated rates.  Only when Martin's rates are  extrapolated  to pH's  > 6
do the two N02~ rates come into agreement (curves  1 and k).

     The effect of temperature on S(IV) oxidation  by H202,  03,  and 02 can
be seen in Figure 2.5.  At lower temperature, the  Henry's Law solubilities
of S02, H202, 03, and 02 all increase.  K(20) and  K(21) also increase,
which further increases the total S(IV) solubility.  On the  other hand, the
H202, 03, and 02 rate constants all decrease with  decreasing temperature.
The combined effects of temperature on  sulfate production rate  are  shown by
comparing curves a and b for 02, curves b and e for 03, and curves  c and f
for H202 rate.  The increase in H202 rate is not as large as is possible
theoretically, since Henry's Law solubility did not enter into  the  calcu-
lation; [H202] in solution was directly assumed.   The H202  solubility will
increase by a factor of six in going from 15°C to  -5°C.  However,  the
[H202] may be limited by the rate of H202 generation in the  gas phase.

     At no time does it appear from Figure 2.5 that an uncatalyzed  02

                                     200

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reaction is important.  For a soot catalyzed reaction to compete effective-
ly with H202 at pH < 6, the soot concentration must exceed - 0.1 g T  ,
and to compete with 03 the soot concentration must exceed 0.1 g 1-1 at pH
- 4.5 and 10 g I'1 at pH - 5.6.  Only at high concentrations of iron or
manganese does it appear that an 02-metal-catalyzed oxidation mechanism can
contribute to sulfate production.

     Lastly, the hydroxyl radical does appear to contribute to sulfate for-
mation given that the conditions assumed by Chameides and Davis (1982) are
appropriate; namely, HO sticking coefficient > 10, droplet size less than
- 2x10   cm radius, cloud transmissivity > 0.5, midday solar fluxes, and
moderately clean air.  Not shown is the contribution from H02 or 02~.  Rate
constants for H02 or 02~ reactions with S(IV) are not available, and it is
generally inferred that the rate constant times the radical concentration
for HO and H02 or 02~ are equal, i.e., k[HO] - k[H02] - k[02'].  There-
fore, it is assumed that the sulfate production from H02 or Q2~ is equal
to that for HO.

     Figure 2.5 in conjunction with Figure 2.6 can be used to assess qual-
itatively the importance of aqueous sulfate production mechanisms in the
atmosphere.  Figure 2.6 shows the equivalent gas-phase rate of species
formation (ppbv hr'1) as a function of liquid water mixing ratio,
WjiU-H20/£-air), and aqueous production rate (M s~M at T = 288K and
P = 1 atm.  The following relationships between aqueous rates and gas-
phase rates are also useful:

     r  (molecules cnr3 s-1) = 6.02 x 1020 W. r ,
      g                                     x,  a
and
     r  (ppbv hr-1) = 2.95 x 1011 W. T P'1 r  ,
      g                            *        a
     r, (% hr'1) = 2.95 x 10* W0 T P'1 X'1 r  = 2.17 x 102k W0 n'1 r,,
      9                        *            a                x      a
where ra is the aqueous production rate  (M s"1), T is temperature  (deg
K), P is pressure (atm), W^ is volumetric liquid water mixing  ratio  of
the air, n is the molecular density of the gas  (molecules cm"3), and X  is
the total (gas + aqueous) equivalent gas-phase  volume mixing ratio of the
reactant species (ppbv).  The following  three examples will help clarify
the use of Figures 2.5 and 2.6.

     Example 1:  Haze aerosol, WA = 10~10, pH = 5.6

     We would like to know the rate of sulfate  formation through an  aqueous
0? - S(IV) reaction in a very hazy layer of air such that WA =  KT10.
Given that the conditions of Figure 2.5  apply,  the air temperature is 15°C
and the aerosol is at pH = 5.6, then the aqueous rate of SO^  production,
ra (SO^3), is - 2x10   M s"1.  Going to  Figure  2.6, we draw a  verti-
cal line through W^ = 1Q-10, and starting from  the bottom move  upward
along this line until it intercepts the  diagonal line corresponding  to  ra
= 2xlo~6.  From this point, we^move horizontally to the left and find that
the gas-phase equivalent rate rg is 1.8xlQ-  ppbv hr"1.  X can  be  assumed

                                     201

-------
.0
 Q.
 a.
cr
o
Q
o
cr
Q-
LU
X
Q.
 I
CO
LU
     !05
     I04
i*P  IO3
LU
I-
     I02
      10'


     10°
    10
      ,-3
I  io-4
o
    IO
10"
             10"
                    IO
                      rlO
IO
                      r9
icr8    icr7
            LIQUID WATER VOLUME MIXING RATIO
       Figure 2.6   Nomogram relating aqueous reation rates
       M s~^ , to equivalent gas-phase reaction rates ppbv  hr'"*,
       and vice-versa for T = 288K, P = 1  atm and given liquid
       water volume mixing ratio.  Diagonal lines are constant
       aqueous reaction  rates.
                            202

-------
equal to 5 ppbv, and the initial rate of S02 conversion to sulfate  is 0.36%
hr-T.

     Example 2:

     Scott (1982) estimates the rate of S02 to sulfate conversion at 10%
hr"1 for storms over the northeastern United States.  If the S02 vapor
concentration were 5 ppbv, then the equivalent gas-phase rate is 0.5 ppbv
hr"1.  The liquid water volume mixing ratio is typically 10~6 in these
storms.  In Figure 2.6, rg = 0.5, and W£ = 10"6 corresponds to ra =
6xlO"9 M s"1.  From Figure 2.5, with ra = 6xlO~9 M  s'1 and pH from  4 to
5.6, it can be seen that reactions involving 03, H202, HO, and iron-cata-
lyzed 02 are all capable of generating sufficient aqueous sulfate to ra-
tionalize the conversion rates observed by Scott.

     Example 3:

     What minimum aqueous H202 concentration is needed to account for a 1%
hr"1 conversion of S02 to sulfate when the aerosol  pH = 3, liquid water
mixing ratio is 10~u, and the temperature is -5°C?  Analogous to Example
2 above, ra is found to be 2x10"^ M s"1.  At pH = 3, T = -5°C, [H202] =
lxlO~5 M, and ra = 6xlO~8 M s"1 from Figure 2.5.  Because ra is linear
with respect to H202, the required [H202] is 3xlO~2 M.  This aqueous H202
concentration corresponds with a gas-phase concentration of 35 ppbv when
Henry's Law equilibrium is assumed.

     This analysis illustrates the inability of low liquid water content
aerosols to generate significant amounts of sulfate.  Cloud droplets and
hydrometeors, on the other hand, appear able to sustain elevated rates of
sulfate conversion with respect to gas-phase reactions during their life-
times.  H202 and 03 are the principal oxidants under the assumed condi-
tions.  At no time does the uncatalyzed 02 - S(IV)  reaction appear  signi-
ficant, and the catalyzed iron and manganese reaction requires atypical
concentrations of these metals.  The hydroxy and hydroperoxy radical oxi-
dation of S(IV) may be important.  However, substantial research on aque-
ous radical chemistry is needed before a definitive judgment can be made.
If the anomalous rate constant for (79) measured by Oblath et al. (1980) is
correct (e.g., concentrated aerosol solutions), then in low pH solutions
N(III) oxidation of S(IV) may contribute to sulfate production.  This seems
unlikely.

2.2  Acid generation from nitrogen-containing species through gas-particle
     interactions and aqueous chemistry

a.  Features of heterogeneous NOy chemistry:  empirical evidence

     Depending on season and location, 30-60% of the acidity measured in
precipitation in regions of NOX emissions is due to nitric acid.  Since
the gas-phase oxidation of NOX (primarily via OH +  N02 " HN03) is a fair-
ly rapid process, approximately ten times faster than its S02 counterpart,
it has generally been assumed that nitric acid in precipitation results
from scavenging of HNOa vapor by falling droplets.  Except during times of
precipitation or near the ground, HN03 and the major nitrogen oxides (NO,

                                     203

-------
NO2, NO3, and N^OS) have been assumed to exist  in  ratios  determined by
gas-phase kinetics (see Table 2.9 and Section 1 of this chapter),  with HN03
a major contributor to dry acid deposition.

     There is growing evidence, however, which  suggests that  this  picture
of tropospheric odd nitrogen chemistry  is not complete.   For  example,  Laz-
rus et al. (1982) found as part of APEX that nitric  acid  appeared  to form
continuously over the course of a warm  frontal  storm and  suggested that
in-cloud acidification was partly responsible.  Even under  dry  conditions,
the NOX/HN03 ratio is often much higher than predicted by purely  gas-
phase kinetics, and loss to particles is a postulated explanation.  This
phenomenon has been observed in both polluted and  unpolluted  environments
(Kelly et al., 1980; Stedman and West,  1981).

     Heterogeneous processes are implicated by  measurements of  other NOy
species in the troposphere, e.g.: (1) nocturnal N03  levels  in virtually all
measurements made to date are lower than can be explained by  strictly gas-
phase processes (Noxon et al., 1978; Noxon et al.,  1980;  Platt  and Perner,
1980; Platt et al., 1981); (2) HONO builds up at night at rates much faster
than can be explained by gas-phase mechanisms (Platt et al.,  1980).

     The species participating in atmospheric nitrogen oxide  and  oxyacid
chemistry are summarized in Figure 2.7.  To the complement  of nitrogen
oxides described in Section 1 of this chapter have been added N203 and
N20it, which may figure in NOX gas-to-particle conversion  and  condensed-
phase chemistry.  The arrows designate  interconversions among three groups
of NOy compounds:  NOX, higher nitrogen oxides, and  acids.  PAN and
HNO^ nave been grouped with nitric and  nitrous  acids because  they  may con-
tribute to acid formation in the condensed phase (Spicer  et al.,  1981),
although the extent to which this takes place is not certain.  This is
partly because PAN and HNO^, like the compound  oxides N203, N20tt,  and N205,
have varying thermal stability over the range of temperatures typical  of   .
the boundary layer.  The sum of all oxides and  acids is referred  to as
NOy.

     Except for ions which come from acid dissociation in the condensed
phase, Figure 2.7 with different kinetics applies  to both gas and  condensed
phases, with the latter comprising three particle  types:  fog or  cloud
droplets, small aerosols, and rain or snow (hydrometeors).  These  are the
same classifications (II-IV) described  earlier  (Figure 2.2).

     The basic features of homogeneous  NOX to nitric acid conversion were
discussed in Section 1 of this chapter, where it was pointed  out  that the
predominant acidification process is OH + N02 ^ HN03; the rate  of  this
depends critically on [OH], which in turn is largely controlled by atmo-
spheric NOX and hydrocarbon levels (see Section 2.4  of this chapter for a
discussion of heterogeneous effects on  hydrocarbons  and other oxidants).
In addition, HN03 may be incorporated into particles or may form  within
them from oxidation of other NOy species.

     The following two sections review  heterogeneous NOy  chemistry.  The
first focuses on aqueous-phase processes, and the  second  surveys  NOy gas-
particle interactions, attempting to describe the  key processes as they

                                     204

-------
N0x
NO /
NO 2 - ,
^


higher nitrogen oxides
* N03 £
>> N205
NzO*
N203
C
„ . 	 	 - 	 ^
<_ 	 —
acids
3 HN03
. .-^ HONO
PAN (?)
HNOj,
N0"2 (condensed
phase only)
NOs

Figure 2.7   Major tropospheric NOy species and schematic inter-
conversion pathways.
                                 205

-------
have been identified by experimental evidence and modeling treatments  to
date.

b.  Condensed-phase kinetics

     A major part of the condensed-phase chemistry of NOy has  been  tho-
roughly reviewed recently (Schwartz and White, 1981).  In terms  of  nitrogen
acidification in precipitation, cloudwater, or other particles,  the  crit-
ical equilibria are the ionic dissociations of nitrous and nitric acids:

                         HN03(a)  *  H+(a) + M03-(a)

                         HONO(a)  :  H+(a) + N02-(a)
The position of the HN03 equilibrium lies strongly to the  right  {Keq  =
15.4; Davis and De Bruin, 1964), and dissociation is expected to  be com-
plete in all but the most acidic particles.  Nitrous acid  is weak  (pKa  =
3.3) so that if it forms to any degree in particles with pH < 4,  a signi-
ficant fraction of it will  be present as undissociated HONO.

     In addition to the thermodynamic and kinetic characteristics of
aqueous NOy chemistry, Schwartz and White (1981) reviewed  the solubility
equilibria of the nitrogen oxides to determine the potential for  mixed-
phase N0x-to-acid conversion; i.e., the nitrogen analog to aqueous S(IV)
acidification.  The primary contributors,

                                    (H20)
                      N02(g) + N0(g)  £  2H+(a) + 2N02-

and

                              (H20)
               N20(g) + N02(g)  J  2H+(a) + N02'(a) + N03-{a),

have equilibria that lie to the right, but Lee and Schwartz (1981) demon
strated that low NO and N02 solubilities inhibit the oxidations  and prob
ably have little effect on aqueous S(IV) oxidation which is highly pH-
dependent.  Direct N02 - S(IV) reaction may, however, oxidize the latter.

     The kinetics for aqueous NOy chemistry are summarized in Table 2.10
(interactions between NQX and SOX are discussed in Section 2.3 of this
chapter).  The list is not exhaustive, but it includes the major  inter-
actions among the NOy species and a number of N03 oxidations.  The pro-
cesses in Table 2.10 may be supplemented by two other types of reactions.
The first are radical -radical interactions, identical to their gas-phase
counterparts, which can interconvert forms of NOy, e.g.,

                            R02 + NO  +  RO + N02

                            H02 + NO  +  M02 + OH

The effects of such reactions on condensed-phase acid formation  are prob

                                     206

-------
Table 2.10.  Liquid-Phase Oxidation of Odd-Nitrogen  to Nitrogen  Oxyacids
Reaction1'
NO + N02 * 2HONO

w
NO + N02 " M2U3

N203 1 2HONO
N02 + N02 2 MONO + HN03

N02 * M02 + N20^
N20,, » HONO + HN03
N02 + N03 " 2HN03
N20; • 2HNO,
N03 + ? - N03- + ?
N03 + Cl- * N03* + C1
NO, * F." . N03- * Fe-
N03 + N02" » M03~ •*• N02
Rate Constant Comment
7.4xl06 M-1 s"1
IxlO8 M-1 s'1
l.lxio9 M-1 s-1
2xl07 M-1 s-1
S.3xl02 s'1 pH <^ 5
10s M-1 s-1
1.7x10* M-1 s-1
3xl07-9xl08 M-1 s"1
Ixl03-6xl0* s-1
7
> 10s s-1
(7. 59*0.21 )x!03 s-1 add
9.5x10^ add
9.7»102 2.8
8xl03 add
3x10" pH « 7
l.SxlO5 natural
IxlO8 M-1 s-1
(8.0Tl.6)xlOs M-1 s-1 acid
1.2xi09 M-1 s-1 pH » 7
Reference
Gratzel et al.-
(1970)
Treinin and
Hayon (1970)
Ross and Neta
(1979)
Epstein et al.
(1982)
Ross and Neta
(1979)
Lee and Schwartz
( 1981 )
Epstein et al .
(1982)
Ross and Neta
(1979)
Ross and Neta
(1979)


Ross and Neta
(1979)
Ross and Neta
(1979)
Ross and Neta
(1979)
Ross and Neta
(1979)
                                  207

-------
Table 2.10.  Liquid-Phase Oxidation  of Odd-Nitrogen  to  Nitrogen  Oxyacids
                              (continued)
Reaction1
N03 i
i- CH3COOH * ?
N03 + HCOOH » ?
H03 i
NO 3 H
M02-
N02-
HONO
HO +
HO +
C03-
Fe"
i- CH3OH » ?
>• CH3CH2OH * 7
+ 03 - M03- + 02
+ H202 « N03- + H20
+ H202 « H+
+ N03- + H20
NO 2 * H02NO
NO * N02- * H*
+ N02 « C02 + M03-
+ N02 l*Fe*** + HOMO
Rate Constant Comwnt
(4.6*0.4)xiO* M-1 s-1
2.06xl05 M-1 s-1
IxlO6 M-1 s-1 acid
2.2xl06-3.9xlOs add
200 [H*]-1 M-1 s-1 pH • 0-3; T - 25»C
4.6»103[H+] M-1 S'1 pH • 0-3; T « 2S'C
2.5xl02 exp(-7650T-M pH * 0.8-3.1;
T « 20-30*C;
x (1 + 7.8 I) M-1 s-1 fonic strength, I
- 0-0.08 M
1.3xl09 M-1 s-1 pH » 9; T » 20-25*C
1010 N-1 s-1 pH » 7; T » 20-2S°C
1x10* M-1 s-1 pH • - 11;
3.1x10* M-1 s-1
Reference
Ross and Neta
(1979)
Ross and Neta
(1979)
Ross and Neta
(1979)
Ross and Neta
(1979)
Martin et al.
(1981a)
Martin et al.
(198U)
Lee and L1nd
(1983, personal
connunl cation)
Farhatazlz
and Ross (1977)
Farhatazlz
and Ross (1977)
Ross and Neta
(1979)
Epstei n et al .
(1982)
                                   208

-------
ably secondary, influencing oxidant levels,  S02 conversion,  and  nitrate
formation.  A second group of reactions stimulating  acid  formation  may  be
oxidations of N02 and N03 by ions  (especially  organic)  other than  those
illustrated:
                               N02
                                       R0<
A full range of subprocesses must be part of a  realistic  aqueous-phase ki-
netic scheme.

     From Table 2.10, it is apparent that there are  a  number of  routes for
effective conversion of aqueous N03 to N03~.  Since  N03 appears  to be read-
ily scavengeable by particles  (see following section),  these reactions may
be major contributors to condensed-phase acidification.   The contributions
of PAN and HNOt,. to aqueous nitrate formation have  not  been  established.
PAN in particular has been proposed as a mid-troposphere  NOX reservoir
(Singh and Hanst, 1981).  Both PAN and HNO^ decompose  upon  dissolution.
PAN may decompose to form N02~ (Mudd, 1966; Nicksic  et  al.,  1967)  or N03~
(Spicer et al., 1981); the products are apparently pH-dependent.   Nitrite
is in equilibrium with HONO, which because of its  relatively low  solubility
(Schwartz and White, 1981) could be desorbed from  the  aqueous phase.  The
compound oxides N20H and N203 also form N02~ in solution.   Thus,  the ox-
ides, PAN, and/or HNOi+ all appear to be potential  HONO  sources.   If so,
the sequence of reactions:
N203
PAN(?)
HNOlf(?)
                        gas
                                   N02-,
                                       •H

                                     HONO
                                                 HONO
                                                     gas
                                     aqueous
could represent a heterogeneous  source  for  tropospheric  HONO  (Heikes  and
Thompson, 1982). .

     The rates of nitrate and nitrite production  through homogeneous  so-
lution phase reactions involving NO, N02, and  N02~  can be calculated  and
qualitatively compared with the  rates from  gas-phase  and heterogeneous
reactions (Section 1 of this chapter).  For these calculations,  the
following conditions are assumed:

                            -,.10
T = 25°C, p(HONO) = 10-1(J a tin, [HONO]  = K(3) P(HONO),
[N02-] = K(3) K(24) P(HONO)  [H+]'1,  [Fe++]  = 10'5  or  10'7  M,
      [H202] = 10-  M, P{03) = 5xlO-8  atm,  [03]  = K(ll)  P(03),
      [NO] = K(16) P(NO), [N02]  = K(17)  P(N02),  and  [HO] = SxlO"13
                                                              M.
The partial pressures of NO and N02 are  allowed  to  vary  from 10"12  to 10~5
atm and span values found typically in pristine  air and  moderately  dilute
plumes.  Solution pH is allowed to range  from  0  to  7.  r(HONO)  and  r(HN03)
through reactions 67, 68, 72, 73, 80, 81, and  82 (Table  2.8)  are  shown in
Figure 2.8.  The rate constants used  to  calculate r(HONO)  and r(HN03) are
listed in Table 2.10.  It can be seen that N(III) oxidation  is  dominated by
H202 at pH < 2.7 and by 03 at pH > 2.7.   The surprising  result  in Figure
                                     209

-------
     icr6
     10
 r8
O
-w
    io
o

o   io-'6
X
     IO-I8
    10
r20
          - Aqueous Rotes of Nitrite or Nitrate Production-
  ,0
   -I2
                             3     4


                               pH

                             i	I
              ,0-l!  ,0-IO  |0-9   |0-8   |0-7   ,0-6




            P(NO),P(N02)OR  [p(NO)xP(N02)f,atm
       Figure 2.8   Aqueous rate of HONO or  HON03 formation as a

       function of pH or NO and N02 partial  pressure at  25° C

       (see figure key on following page).
                               210

-------
                                      Figure 2.8

                                      Figure Key
     Label
     Mechani sm
Rate Constant Reference
                     NO,- + 0, * NO,- + Or
                                     Martin et al. (19815)
       b  '
N02- + H202 + N03~ + H20


   [H202] = ID'5 M

         H20
N02 + N02 + MONO + HN03

        H20
NO + N02 + 2 HONO
Martin et al. (19815)
                                                          Lee and Schwartz  (1981)
                                                          Lee and Schwartz  (1981)
                     N02 + Fe^ + N02- -»

                        [Fe**] » 10-5 M


                     N02 + Fe++ * N02-

                        [Fe+*] = 10-7 M


                     NO + HO * HONO

                        [HO] = 5xlO-i3


                     N02 •*• HO * HN03

                        [HO] = 5xlO-13
                                     Epstein et al. (1982)
                                     Epstein et al.  (1982)
                                     Farhataziz and Ross (1977)
                                     Farhataziz and Ross  (1977)
[03] is calculated assuming Henry's Law and a gas-phase 03 partial pressure of
5x10"8 atra.  [NO] and [N02J are also calculated assuming Henry's Law and NO or N02
partial pressures given the lower a5scissa.  [N02~] is calculated assuming Henry's
Law and  HONO partial pressure of 10-10 atm.
                                          211

-------
2.8 is r(HN03) through 81.  The oxidation  of  N02  by  Fe++  exceeds 80 as a
HN03 source up to NO? partial pressures of 4xlQ-9 atm  (for  [Pe"1"1"]  = 10-' M)
and 5xlO-7 atm (for [Fe++] = 10"5 M).  The HO,  liquid  phase oxidation of NO
and N02 does not appear to be a significant source of  HONO  or  HN03.

     Figures 2.6 and 2.8 can be used together to  compare  the aqueous sour-
ces of HONO and HNQ3 with heterogeneous and gas-phase  mechanisms.   If we
further assume that the rates of HONO and  HN03  must  exceed  0.1  and 1.0 ppbv
hr  , respectively, to be relevant  to atmospheric chemistry, then  minimum
conditions for the aqueous mechanism can be established.  Maximum  liquid
water contents for aerosols are near 10_ °.   From Figure  2.6,  it can be
seen that ra must exceed 105 M s~l  for rg  > 0.1 ppbv hr"1,  and  from
Figure 2.8 it is obvious that none  of the  reactions  shown for  HONO can
produce the required amount.  Similarly, it can be shown  that  none of the
aqueous HN03 reactions considered is capable  of generating  1.0  ppbv hr"1.
Liquid water contents for clouds are near  10" , and  _from  Figure 2.6 it can
be seen that ra must exceed 10~9 M  s"1 in  order for  rg >  10"1  ppbv
hr"1.  Using this value for ra and  Figure  2.8,  it can  be  shown  that the
partial pressure of N02 must exceed 5x10   atm  (• 500  ppbv)  or  [P(NO)»
P(N02)]~/2 must exceed 6xlO~7 atm  before  aqueous reactions can be a
significant source of HONO.  Such conditions  are  uncommon for  the  tropo-
sphere, but might be found within a condensing  power plant  plume.   Again,
in an analogous manner, it can be shown that  for  r(HN03)  >.  1 ppbv  hr"1,
then ra >. 10"8 Ms"1.  Only the 03  - N02"  (67)  and the N02  - N02 (81)
aqueous reactions are able to sustain such a  rate (Figure 2.8),  and even
then the pH must be greater than 5.2 and P(N02) must be greater than 2000
ppbv.

     The above analysis suggests that, for the  purposes of  tropospheric
HONO and HN03 chemistry, homogeneous solution-phase  reactions  are  negli-
gible under all but the most extreme conditions.

c.  NOy gas-particle interactions

     The partitioning of trace species between  the particulate  and gas
phases determines the chemical composition of precipitation, and ultimately
the relative amounts of wet and dry deposition.   The greater the fraction
of a given species in suspended particles, the  smaller is the  amount di-
rectly deposited at the Earth's surface.   Hence,  during periods of low
particle density conditions, nearly all gas deposition is dry.

     In principle, nitric acid formation in the atmosphere  may  occur as a
consequence of either homogeneous or heterogeneous reactions.   In  the for-
mer case, HN03 is formed in the gas phase. It  may be  removed  by dry depo-
sition or absorbed onto particles.  In the latter case, an  acid precursor
(NOX or a higher oxide) is adsorbed and then  oxidized  within or on a par-
ticle surface.  Thus, to evaluate HN03 deposition mechanisms,  it is ne-
cessary to determine both the gas-particle partitioning of  HN03 and the
degree to which HN03 precursors rather than HN03  itself are involved in
deposition processes.

     Although ten neutral and two ionic forms of  NOy distributed among
four modes (gas phase and three particulate types (Figure 2.2)) would

                                     212

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require solution of 46 continuity equations, considerable  simplification  of
NOy kinetics is usually possible.  To begin with, within a given  phase
there is usually a rapidly achieved steady state  between NO and N02  and
among the compound oxides N204 and N203, NOX, and the  acids.   Under  some
conditions, N03 and N205 can also be assumed to be  in  a steady-state equi-
librium (Heikes and Thompson, 1982).  We have also  seen that  condensed-
phase conversion of NOX and N02~ to nitrate is negligible  under normal
tropospheric conditions.  Furthermore,  it is usually assumed  that,  because
of their low solubilities, NO and NQ2 are not absorbed by  particles.  (This
would not be true if there were significant reaction between  N02  and an
organic compound on the particle surface.)

     It is convenient to consider two important cases  of heterogeneous
NOy chemistry.  The first is the small  particle which  has  a pronounced
composition-size dependence at equilibrium and which can be thought  of  as
starting nuclei for chemical and physical evolution.   Although the  growth
dynamics of such particles are usually  linked to  sulfuric  acid, the  amount
of dissolved HN03 influences pH and the S(IV) - S(VI)  chemistry (Chapter  V,
Section 2).  A second class of heterogeneous processes involves interac-
tions between gases and particles in which the collecting  (and evaporation)
properties of the latter are unaffected by gas absorption.  In between  the
two extremes, particles change composition as they  grow or shrink until
they deposit at the surface (see Chapter VI, Section 5) or are scavenged  by
cloud droplets or precipitation (Scott, 1982).

     Gas-particle interaction coefficients of the type kc(I,J) have  been
given for NOy species by a number of investigators  (Luther and Peters,
1982; Levine and Schwartz, 1982; Heikes and Thompson,  1982).   They  follow
Fuchs1 and Sutugin's (1970) formulation of the gas-to-particle diffusion
rate in which the most critical parameter is the  sticking  coefficient,  the
probability that a gas diffusing to a droplet will  stick upon encountering
it.  Particle removal coefficients corresponding  to number densities of  ty-
pical aerosol, cloud, and raindrop distributions  are given in Table  2.11.
They were calculated for HN03 and other NOy species, but values for  most
reactive gases and radicals are similar (Cnameides  and Davis  (1982); kc
(I,J) for OH and H02).  Figure 2.9 shows an approximate altitude  dependence
of kc for typical atmospheric conditions, i.e., particle distributions
corresponding to aerosols, fog, and a non-precipitating cloud. For  each
entry in Table 2.11, the number in parentheses is k~1=x, the  characteristic
removal time for the process.  The most rapid removal  is calculated  for
cloud or fog conditions in which the liquid water content  is  high.

     The particle removal constants for a cloud (.03 -.16  s"1, depending  on
the sticking coefficient) are well within the lifetime of  a typical  cloud
drop (10 min.).  Hence, a cloud in contact with a stable air  mass will
gradually deplete the air of HN03, and  possibly N03 and N205. NO and N02,
because of their low solubilities, will be relatively  unaffected  (Lee and
Schwartz, 1981).  Since HN03, N03, and  N205 scavenging are essentially
irreversible (conversion of the latter  two species  is  assumed to  form N03~
instantaneously), return of these species to the  gas phase occurs only  by
particle evaporation.  However, scavenged N03 is  likely to be returned to
the gas phase as HN03 so that particles have acted  as  heterogeneous  acid
sources.  If we assume that a steady-state exists between  particle  removal,

                                     213

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                               Table 2.11
                   k(Gas.Part)  for HN03,  N03,  and  N205
                                (in s-1)
  Sticking Coefficient   k(Gas,Aerosol)
          (a)
k(Gas,Cloud   k(Gas,Raindrop)
   Droplet)
1.0
0.1
0.01
0.001
3.46 x 10-3
(289)
9.58 x 10-"
(1040)
1.21 x 10-*
(8260)
1.26 x 10-5
(79400)
1.65 x 10-1
(6.06)
1.57 x 10-1
(6.37)
1.08 x 10- *
(9.26)
2.99 x 10-2
(33.4)
4.67 x 10-"
(2140)
4.67 x 10-"
(2140)
4.61 x 10-"
(2170)
4.17 x 10-"
(2400)
Heikes and Thompson (1982).
                                   214

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      10
i    «
UJ
Q
r>
     0.1
     .01
I   I  I II III|     I  I I  I I INj    I   I I I I III
              i   i  i i  i nil    i  i  i  i i nil    i   i  r«j 11 nl     i  i  i  i i n
         10-4
10-3
          10-2
10-1
I
                                            max
                                   part
         Figure 2.9   Vertical profiles of normalized first order particle
         removal  coefficients, kpartApirt -kc  (J«J) 1
-------
kc(I,J), and particle breakup, ke(J,I),
        /

         0  =  k (I,J) {[HN03] + [N205] + [N03]} - k  (J,I)  [N03-],
                w                                   tr

the ratio of gas phase acid and precursors to dissolved  nitrate  is  given  by
the ratio of the condensation (removal) and evaporation  coefficients:

                            [N03-]            k (I,J)
                                           _   v*
                      JHND3 +1T205 + N037     ke(J,I)

     A more detailed steady-state treatment of heterogeneous NOy  chemis-
try has been carried out by Heikes and Thompson  (1982).  Observations  of
low nighttime N03 can be accounted for by aerosol removal of the  latter,
although olefin scavenging of N03 or a NO + N03  reaction could  also  explain
the measured levels (Platt et a!., 1980; Platt et al., 1981).   Richards
(1982) has discussed the contributions of NQ3 removal to aerosol  nitrate
formation in Los Angeles.  Heikes and Thompson (1982) have also calculated
the dependence of cloudwater HN03 acidification  on kc(I,III), NOX and
03, photolysis rates, and other physical parameters.  For example, Figure
2.10 shows the HN03 formation rate, r(HN03), as  a function of kc(I,III).
The dotted line represents a gas-phase equivalent rate of 1 ppbv  hr"1
(T = 288K, P = 1 atm).  At low values of kc(I,J), the primary mechanism
of in-cloud nitrate formation is the reaction OH + N02 •*• HN03,  followed by
particle removal of the latter.  This pathway would not be operative at
night when OH production ceases.  At higher values of kc(I,J),  cloud re-
moval of N03 and N20s is fast enough to compete  with photolysis and  could
produce appreciable HN03 in clouds both day and  night.  From Figure .2.10,
it can be seen that a 1 ppbv hr"1 HN03 formation rate requires  minimum
values:  kc(I,J) » 10-3 s"L, NOX = 10 ppbv, and  50-100 ppbv 03.   Heikes
and Thompson (1982) have also analyzed the role  of NOy and particle/water
vapor interactions in heterogeneous nitric acid  formation for fixed  levels
of NOX and 03.  The results are presented in Figure 2.11.

     Other examples of model studies of heterogeneous NOy removal  include
one-dimensional calculations of below-cloud HN03 washout (Thompson and
Cicerone, 1982; Turco et al., 1982; Stewart et al., 1982).  Durham et  al.
(1981) have investigated HN03 scavenging by falling raindrops.  Cloud  drops
which begin at pH = 5.5 are acidified first by HN03, then by S02  adsorp-
tion; those which start at pH = 4 only add HN03.  Although scavenging  is
very effective in cleansing the atmosphere of HN03 (Huebert, personal  com-
munication, 1981), the implication from the APEX study is that  in-cloud
HN03 formation may be an important source of acid precipitation in polluted
environments.

     Zero- or one-dimensional model calculations may be able to treat  cer-
tain case studies, but they are probably poor representations of  long-term
averages since many episodes of varying precipitation intensity and  compo-
sition determine mean wet deposition.  In places where the composition is
not highly variable, it is important to use properly chosen steady-state
wet removal coefficients Ypart to estimate wet removal (Rodhe and Gran-
dell, 1972).  One approach to estimating TTpart is to average episode-
integrated removal over a representative period  of time:

                                     216

-------
10s
I08
«   I07

 o
  *

 c?
 I  ,o6
             I         I

       NOX, 03
   IC
           100, 50
          10,10
          1.0, 50
          0.1,50
                ic
               5
I0
'4
       I0
                                    "3
IO
                     -2
10'
IOC

    Figure 2.10   Effect of NOX and 03 (in ppbv)  on HN03 formation
    rate, r(HN03),  as a function of kpart ['cc(J'1) in text]. Values
    for other parameters are:  T=288K;  P=l  atm;  OH=106 cm-3.
    Photolysis rates used in calculations are for cloudy conditions,
    Dashed line reoresents an HN03 production rate of 1.0 ppbv hr-1
    (Heikes and Thompson, 1982).
                            217

-------
  10
                                               IOC
Figure 2.11   In-cloud HN03 formation rate r(HN03),
calculated as a function of kpart [kc(I,J) in text]
for various production pathways.  Solid curves are
for daylight conditions and dashed curves are for
nocturnal conditions.  E's represent total formation
rates.  Curve labels refer to the following reactions:
R19, N02 + OH + M -»• HNOs + M; .R29, N205 + N£0 •»• 2HN03;
R37, N03 + wp ->• HNOs;  R39, N204 H- wp -*• HONO + HN03;
R40, ^305 + wp -»• 2HN03.  Assumed conditions are:
T = 283 K,  P =0.9 atm, NOX = 10 ppbv, 03 = 50 ppbv,
100% relative humidity,  OH = 106 cm~3 daytime;
OH = 0 niqht.  Nocturnal formation rates are not shown
at kpart < 10~2s_i because steady-state model assumptions
are not valid.
                         218

-------
                     kpart(z)
 cond
k    (x,y,z,t)dt
     / dt
where the instantaneous  removal  coefficient kpart(x,y,z,t)  has been writ-
ten to emphasize  its spatial  dependence  (Levine and Schwartz,  1982: Thomp-
son and Cicerone, 1982).  Thus,  a  single  value  of l(part»  e.g., 10   s"1,
may represent a continuous  aerosol  removal  or a few hours per  week of fog
or precipitation  deposition.  Depending  on  the  altitude distribution of
£part» t"6 relative amounts of wet and dry  removal  may vary by a factor
or two or more (Thompson  and  Heikes, .1982).

     The examples we have described represent simplifications  of a four-
phase NQy chemistry, as  illustrated in Figure 2.7.   Particle evolutions
and transport have been  neglected,  and heterogeneous processes have in-
cluded primarily  irreversible scavenging  of HN03  and higher nitrogen ox-
ides.  Schematically,  interactions of all  species between two  boxes of the
type shown in Figure 2.7  have been  simplified:
             Gas:  I
NO J higher
oxides
: HMO 3
HONO
             Particle:   11,111,1V
                                             ke  t
  Although this represents a  great  reduction  of  complex  chemical  and micro-
physical processes,  it may describe NOy  chemistry  adequately in many sit-
uations in the troposphere.

2.3  Coupling of NOX - SOX aqueous  and particulate chemistries

     An issue in the modeling of  acid deposition is  the  question of line-
arity.  Linearity usually implies that the  amount  of sulfate and nitrate
received at the earth is directly proportional to  the quantity of sulfur
and odd nitrogen emitted anthropogenically.   The relation of deposition to
emission is highly dependent  upon the spatial  and  temporal  scales over
which linearity is considered.  Clearly,  over the  globe  and on an annual
basis, sulfur or nitrogen deposition is  linear.  Otherwise there would be
a net accumulation or loss of the oxides  of  sulfur and nitogen in the atmo-
sphere.  However, on a regional scale such  as eastern North America, this
question is clouded  by the flux of  material  through  the  lateral  boundaries,
the scales of the deposition  phenomena (e.g.,  precipitation extent and du-
ration), and the chemical mechanisms of  acid  formation.   A point central  to
the latter effect is the degree to  which  the  primary acids (HN03 and H2S04)
and their precursors (MOX and SOX)  interact.

                                     219

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     Rodhe et al (1981) demonstrated theoretically  that  for  their  highly
simplified chemistry and environmental conditions,  the production  of  sul-
fate in the atmosphere and its deposition are  strongly influenced  by  odd
nitrogen emissions.  The link between sulfate  and nitrate  in  their model
is the competition between S02 and NOX for gas-phase oxidant  (OH)  and
aqueous oxidant (H202).  Our discussion of aqueous  and heterogeneous  SOX
and NOX chemistries has described at least five potentially  significant
areas of interaction:  gas-phase oxidant competition, aqueous  oxidant
competition, acid inhibition, S02 oxidation by NOy, and  volatization  of
weak and comparatively insoluble acids.  We will consider  each  of  these
briefly.

a.   Gas-phase oxidant competition

     In the gas-phase homogeneous chemistry section (Section  1  of  this
chapter), it was shown that the principal acidification  reactions  were:

                          N02 + HO + M + HN03  + M                        (1)

                    S02 + HO + M + HS03 + M —>  H2$Q>*>                  W

with the reaction (2) being either an HOX radical termination  reaction or
more likely an HOX radical chain propagation reaction.   In either  case,
there remains the competition for OH with the  rate  constant  for (1) being
approximatly one order of magnitude faster than the rate constant  for (2).
If one molecule of NOX is emitted with one molecule of S02,  as  state-wide
emission inventories would suggest, then initially  there will  be a ten-to-
one production ratio of HN03 to H^O^ in the gas phase.  Consequently, on
the basis of HO chemistry, sulfate production  and possibly its  deposition
will lag significantly behind that of nitrate.

b.   Aqueous oxidant competition

     In aqueous solutions, the question of oxidant  competition  is  more
clouded.  The concentration of S(IY) and its speciation  are  shown  to  be
pH-dependent, and the solubility and speciation of  N(III)  are  as well.
The rate constants for S(IV) reaction with 02, 03,  H202, N02~  are  pH  de-
pendent (see Tables 2.2 - 2.6), as are the rate constants  for  N(III)  reac-
tion with 03 and H202 (Table 2.10).  The speculated aqueous  HOX reactions
leading to S(VI) and N(V) formation compete with each other  for HOX and
with almost all other dissolved species as well.  The complexities of rate
constants and solution composition do not permit us to conclude on the ba-
sis of oxidant competition whether sulfate oxidation will  inhibit  nitrate
production or whether nitrate production will  inhibit sulfate  production.

c.   Acid inhibition

     It was shown earlier that acidification of aqueous  particles  will
reduce the S(IV) concentration and, depending  upon  the oxidant mechanism,
significantly reduce the rate of sulfate production.  The  production  of
S(VI) from S(IV) is in and of itself inhibiting, since one molecule of H+
is released for each molecule of HS03~ which is oxidized at  the normal pH'
encountered in cloud and precipitation water.  The  incorporation of HN03

                                     220

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either through gaseous absorption or aqueous production will  also  acidify
the particle.  Therefore, HN03 and/or other acids can influence the  atmo-
spheric production rate of sulfate (Durham et al., 1981).  Conversely,  the
absorption of ammonia will act to neutralize the solution and promote  sul-
fate formation (McKay, 1971).

d.   S02 oxidation by NOy

     Oxides of nitrogen may directly oxidize S(IV) or catalyze other
oxidation mechanisms.  Nash (1979) indicates that N02 will oxidize bi-
sulfite to sulfate.  However, at his N02 concentrations (80 ppmv), the
reactions


                             2N02{g) * N204(g)

                              N02(g) $ N02(a)

                        2N02(a) * HONO(a) + HN03(a)

                                * HONO(a) + HN03(a)
can lead to significant MONO formation, and  he could  have  been  observing
the reaction

                     2NUII) + 2S(IV) * N20 + 2S(VI).                    (3)

Rate constants for (3) are reported by Oblath et al.  (1980)  and Martin  et
al . (1981b).  Reaction (3) was shown earlier to be  negligible under  typical
cloud and rain conditions (Figure 2.5).  Another possible  way for  NOX  to
oxidize S(IV) in solution is the diffusion of N03 to  particles  followed by
a direct N03 - S(IV) reaction or the production of  aqueous radicals  which
then oxidize S(IV) (as discussed in Section  2.2 of  this  chapter).  It  is
premature to assess the significance of this mechanism in  sulfate  produc-
tion.  Lastly, it appears that N02 can catalyze the conversion  of  S02  to
sulfate on dry soot particles (Cofer et al., 1981), although this  would be
of negligible importance under all but the most extreme  atmospheric  condi-
tions.

e.   Volatilization of weak and comparatively insoluble  acids

     The last interaction between NOX - SOX  to be discussed involves
the volatization of weak and relatively insoluble acids.   The desorption  of
S(IV) as pH decreases has already been discussed as part of the acid inhi-
bition effects.  Along with S(IV), there will also  be a  loss of HONO as the
pH falls.  Perhaps most important is the loss of HC1  from  NaCl -containing
particles on which HN03 and H2SUi+ are incorporated, and  the loss of  HN03
from particles upon which ^SO^ has absorbed or been  produced.  These
effects are all amplified if the wet particle is undergoing evaporation.
The HC1 loss mechanism was proposed by Erickson (1959, 1960) and Yui et
al . (1976) as a source of gaseous chlorine compounds, and  has been observed
by Martens et al. (1973), Duce et al . (1965), and Hitchcock et  al . (1980).

                                     221

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The volatization of HN03 is thought to be observed  in  the  anticorrelation
between aerosol N03" and SOi^ (Harker et al., 1977) and  the  fact  that  in
the northeastern United States little if any aerosol nitrate  is observed.
Theoretical studies (e.g., see Tang (1980), Middleton  and  Kiang (1979), and
Peterson and Seinfeld (1979)) also indicate that the incorporation  of  sul-
fate on aerosol causes HN03 desorption.  The net effect  of acid volatiliza-
tion is to reduce aerosol acidity, while at the same time  increasing the
concentration of acidic vapors and reducing aqueous rates  of  SQ^~ and
N03~ formation as the precursors S02 and HONO are lost.  In  the development
of realistic acid deposition models, the chemical mechanisms  employed
should be capable of treating the various interactions.

2.4  The role of hydrocarbons and organic oxidants  in  heterogeneous
     atmospheric processes

a.  Introduction

     All  of the atmospheric organic molecules and radicals participate to
some degree in heterogeneous processes.  Many species  are  found in  preci-
pitation (e.g., Galloway et al., 1976; Klippel and Warneck,  1978; Thompson,
1980; Meyers and Kites, 1982), and organic compounds of  all  classes  are
found in aerosols (Grosjean et al., 1976; Hahn, 1980;  Ketseridis  and Eich-
mann, 1978; Simoneit and Mazurek, 1981).

     Organic compounds in particles may be important to  acid  evolution in
two respects.  First, organic acids will partly determine  pH, and organic
neutral molecules and radicals will play a counterpart to  their gas  phase
role in determining dissolved oxidant levels, especially OH  and H02.   In
addition, a critical uncertainty in acidic particle evolution is  the degree
to which organics concentrate on the outer surface  of  aerosols  (Ripperton
et al., 1972; Graedel et al., 1982).  A densely-packed organic  layer would
inhibit exchange of volatile material between the condensed  and vapor
phases (Chang and Hill, 1981).

b.  Model treatments and condensed-phase chemistry

     Zero-dimensional models which treat organic and inorganic  chemistry  in
detail (e.g., Calvert and Stockwell, 1982; Atkinson et al.,  1982) for  the
most part neglect heterogeneous interreactions and  condensed-phase  chem-
istry.  In one-dimensional models which treat a limited  number  of organic
species (Chameides, 1978; Liu, 1977; Hov, 1982; Thompson and  Cicerone,
1982; Turco et al., 1982), it is conventional to include a first-order
removal constant kc(I,J) for the most soluble ones, e.g.,  peroxides,
aldehydes.  Many organic acids, alcohols, and nitrates are probably  suffi-
ciently soluble to be removed to particles with rates  on the  order  of  kc
(I,part) = (- IQ-^-lQ-1 s'1) for HN03.  Like their  inorganic  analogs OH
and H02, radicals of the type RO, R02 are also probably  scavengeable from
the gas phase (Luther and Peters, 1982).

     Reviews of aqueous organic chemistry pertaining to  atmospheric  systems
have been given by Mill  (1980) and Graedel and Weschler  (1981).   In  gen-
eral, the reactions proceed as in the gas phase, with  the  first step con-
sisting of oxidation by OH or 03,  followed by 02 addition  to  form a peroxy

                                     222

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radical  R02.  Subsequent reactions propagate radical  generation  and  even-
tually form peroxides, alcohols, acids, etc.:

                                              /aldehydes")
                    OH,03  02       NO,H02    Jketones   /
                RH    >  R -»•   R02    *       (alcohols  >
                                     etc.     I peroxidesi
                                              vacids     /

At all stages of reaction, there is a possibility of  material exchange
between gas and condensed phases.  For example, particle incorporation  of
atmospheric acids and alcohols, lower aldehydes, and  peroxides may enhance
significantly the aqueous phase concentrations of these  species.

     Published aqueous-phase radical kinetics  models  (Chameides  and  Davis,
1982; Turco et a!., 1982) do not include the organic  molecule contribu-
tions, although these must be included for correct  characterization  of  OH,
H02, RO, R02, and H202.  This is an area requiring  much  additional re-
search.  Given the abundance of tropospheric organic  species, a  reasonable
approach to calculating them in a condensed-phase kinetics model would  be
to group them in various ways (as is proposed  in the  treatment of  gas-phase
hydrocarbons) and to determine the effects on  aqueous OH, RO, and  other
radicals and peroxides.  Some of the kinetic information needed  to do  this,
including numerous organic reactions with OH and H02, is available from NBS
reviews (e.g., Fahrataziz and Ross, 1977; Ross and  Neta, 1979).  Hoigne and
Bader (1975) have studied ozone reactions in natural  waters.

2.5  The possible coupling of chemistry and meteorology

     An issue which requires consideration at  some  point is  the  decoupling
between a meteorological model and chemical models.   It  is accepted  that
the meteorological process controls species concentrations,  reaction,  and
deposition.  However, the effect of chemistry  on the  meteorological  vari-
ables is less well-known, and is assumed to be negligible by most  research-
ers.  The latter phenomenon, tentatively called inadvertent  weather  modifi-
cation, may be important under some as yet unknown  conditions.   The  major
pathway for chemical effects on meteorology is through heterogeneous pro-
cesses.  The chemical evolution of aerosol directly influences its growth
characteristics and consequently the number and activity of  cloud  conden-
sation nuclei (Hung and Liau, 1981) and ice nuclei  (Saxena and Hendler,
1982), which in turn determine cloud development (Ochs and Semonin,  1979)
and the onset of precipitation (inferred from  Lee et  al., 1980).   Visibil-
ity degradation in humid and polluted air is one example of  aerosol  modi-
fication (see Atmospheric Environment, 1981, Vol. 15, 10-12).  Cloud forma-
tion and enhancement are observed downwind of  Chicago along  the  Michigan-
Lake Michigan shoreline.  Also, power plant plumes  are observed  to develop
clouds or augment cloudiness in humid air (Koenig,  1981).  The St. Louis
urban plume is thought to increase precipitation amounts (through  cloud
seeding), but this remains statistically unproven (Chagnon,  1979).   The
possibility also exists that pollution may actually decrease precipitation
(over-seeding).

     Changes in aerosol characteristics and cloudiness directly  affect  the

                                     223

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short- and long-wave radiative properties of the  air  and,  indirectly,  the
heating and cooling of the earth's surface—or, in other words,  the  driving
forces of the atmospheric motions.  The extent of this  is  unknown,  and is
probably of negligible importance to current modeling.  It  is,  however,  at
the heart of aerosol-climate studies.

2.6  Summary of the chemical reactions important  for  acid  generation
     in the troposphere

     In the preceding discussions in Sections 1 and 2 of the  current  chap-
ter of this review, we have learned that there is a great  diversity  and
seeming complexity of the reaction channels in the troposphere  which  con-
vert S02 and NOX into H^Oi, and HN03, respectively.   Obviously,  all  of
these many reactions are not required in any acid generation  and preci-
pitation model  to insure some reasonable accuracy for the  chemical  trans-
formations leading to acids.  Sensitivity studies allow one to  arrive  at
some minimum set of reactions for use with any given  model which will
provide the desired level of accuracy.  Our current review  and  evaluation
gives some guidance in this choice.  The following reactions  are judged to
be of primary importance for acid generation for  tropospheric conditions
which are commonly encountered:

        Gas Phase:     HO + S02 (+M) + HOS02 (+M)	•»• H2SO^          (1)

                       HO + N02 (+M) -» HN03 (+M)                         (6)

        Liquid Phase:  S(IV) + H202 * H2S04 +  ...                       (61)

                       S(IV) + 03 •»• H2S04 + ...                         (60)

                       S(IV) + HO •*• H2S04 + ...                         (62)

                       S(IV + H02(02") + H^...                    (63,64)

                       S(IV) + N03 + H2S04...                           (65)

                       N205 + H20 > 2HN03                               (78)

     The gas phase reactions (1) and (6) appear to be major acid forming
steps in the troposphere.  Thus, for a moderately polluted  troposphere
during relatively cloud-free daylight hours, the  theoretical  rates  of  S02
and N02 transformation through (1) and (6) in  summertime amount to  about
16% and 150%, respectively, per 24 hr period.  In wintertime, significantly
lower rates are expected:  about 3 and 25% per 24-hr  period,  respectively.
Reactions of S02 with 0(3P), CH202 (and other Criegee intermediates),
CH302, etc., may also contribute to the acid generation, but  the conditions
necessary for their significant occurrence are probably rare.

     When gaseous S02 encounters cloud water,  fog, or rain  water, it dis-
solves in part to form S(1V) species (S02-H20, HS03-, SOH=, and H?0+).
The reactions of these species with various water soluble,  oxidizing
impurities in the water can occur and lead to  acids.  Thus, reactions  (61)
and (60) of the S(IV) with H202 and 03 are expected to  be  very  important

                                     224

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acid-forming processes in the liquid water-containing  air  masses.   Rates  of
these can be as high as several hundred percent per  hour for  pH  and reac-
tant concentrations which are not uncommon  in  the  troposphere (see  Figures
2.5 and 2.6).  The reactions (62)-(65) and  (78) involve gas-phase-gener-
ated, transient species which are transported  to and captured by the water
particles.  If the fraction of the species  captured  per collision  is suf-
ficiently high (greater than about Ixio   )  and their competitive reactions
with other impurities are unimportant, then  these  reactions appear  in the-
ory to be very significant to acid generation  in clouds; state-of-the-art
models of acid generation and transport should include them.   Further work
on the experimental evaluation of the  capture  coefficients will  be  neces-
sary to quantify the estimates of the  rates  of these processes within the
troposphere.  In addition, the reactions  of other  oxidizing agents  such as
PAN (peroxyacetylnitrate), H02N02 (peroxynitric acid), CH302H (methyl hy-
droperoxide), etc. may be important, although  further  experimental  work
will be necessary to define better these  possibilities.  State-of-the-art
models should include these reactions  if  and when  they are shown to be
important.  For certain relatively uncommon  conditions encountered  in
highly-polluted atmospheres (e.g., urban  fogs), the  Fe3"1",  Mn2+,  and the
graphitic carbon-catalyzed reactions of S(IV)  with 02  can  be  significant
sources of acid in theory; provision for  their inclusion for  these  cases
should be made.

     The homogeneous gas-phase chemistry  typical of  the reactions  in smog
must be included in model development  to  generate  in a realistic fashion
the concentration-time profiles for the reactive species (HO, 03, H202,
N03, N205, H02, etc.) which are responsible for the  acid production in the
above reactions.  Two somewhat sophisticated "smog"  models developed and
tested by Atkinson et al. (1982b) and  Whitten  et al. (1982) are  available
to modelers today.  These mechanisms contain relatively large numbers of
reactions (80 and 75, respectively) and chemical species (about  53  and 39,
respectively).  Some simplification of these schemes appears  to  be  possible
with sacrifice of chemical detail.  However, it is clear that a  state-of-
the-art description of the chemistry of acid development is not  a  trivial
exercise; a very large number of reactions  and equilibria  must be  employed
to achieve an accuracy comparable to those  obtainable  in the  transport and
dry deposition portions of sophisticated  regional  transport models.  A mod-
ular approach to the treatment of chemistry  is recommended to those who
plan to develop future models; this will  allow a suitable  updating  of the
mechanism as knowledge of acid-forming processes grows without serious
perturbation of the transport and other computer packages  in  the model.


3.  PHOTODISSOCIATIVE PROCESSES IN CHEMICAL  MODELING

3.1  Introduction

     Accurate modeling of tropospheric photochemistry  requires photolysis
rates based on a radiation field which includes ozone  absorption and mo-
lecular scattering.  Photolysis rates  also  depend  on cloud cover,  aerosol
loading, and surface reflection, so that  a  close connection exists  between
meteorological conditions and trace gas distributions. Since clouds and
aerosols may change over a short period of  time and  surface reflection

                                     225

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varies with location and solar angle, it  is necessary to  have  a  rapid  means
of calculating radiation in a regional-scale model.

     The photolysis rate of a molecule A  by fragmentation  pathway  I,
js"1), is an integrated product of  three wavelength-dependent  terms:
                            f


                             dxFtotal(x)oA{x'THA(x'T)
                                                                         (1)
where a.(x,T)) = the absorption cross-section (cm2) of molecule A  at wave-
                 length X and temperature T,

       $A(x,T) = quantum yield or probability that molecule A  decomposes
                 by pathway I on absorbing radiation of wavelength  X,  and

     Ft .  -,(x) = the solar flux (cnr2), wavelength x, at x,y,z.

     For tropospheric J^'s, it is appropriate to integrate in  the  wave-
length range Xx, X2 - 280, 730 nm, because stratospheric 02 and 03  block
out most of the uv radiation and because no photochemistry of  interest
takes place beyond the Chappuis band of ozone.  In practice, the inte-
gration is carried out by summing over wavelength intervals of 10-20 nm:
                    ,1
                         AX. F(x.
                                 total
                                         (xi,T)
(2)
In
the
the near uv (295-325 nm), refined resolution is required for calculating
 rate of the photolysis of ozone:  03 n¥  0(1D) + 0?.
     For many of the species which photodecompose  in  the  troposphere,  ab-
sorption cross-sections and quantum yields have been  measured  in  the  lab-
oratory; some have been determined over the appropriate temperature  range
(220-300 K).  Tabulations of these quantities and  the extraterrestrial
solar flux are available in a convenient form for  use in  model  calculations
(NASA, 1982; WMO, 1981).  Hence, the problem of calculating photolysis
rates in a photochemical transport model reduces to calculation  of  the  near
uv-visible solar flux under a variety of atmospheric  conditions.

     There is an enormous body of radiation literature (see, for  example,
the review by Coulson and Fraser (1975)), most of  it  dealing with highly
accurate methods of solving the radiative transfer equation.   They  are
prohibitively costly, even in a one-dimensional model, and they  would not
guarantee highly accurate photolysis rates since absorption cross-sections
and quantum yields are  rarely determined to better than 20% (NASA,  1982).
Thus, a few percent accuracy in calculating the solar flux is  probably
sufficient for computing JA*  (This can be compared to gas-phase  bimo-
lecular rate constants  which can be uncertain to factors  of 2  or  3  for
certain complex reactions.)
                                     226

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3.2  Flux calculations and photolysis rates

a.  Clear sky values:  effects of multiple scattering and surface reflec-
    tion

     The total solar flux (cnr2) can be expressed as a sum of direct and
diffuse radiation:

                      Ftotal  =  Fdirect + Fdiffuse

Calculation of direct flux at a point in the atmosphere is straightforward.
In the wavelength range A = 280-730 nm, the extraterrestrial solar flux
F0U) is absorbed somewhat by ozone in its Muggins band and to a lesser
extent in the Chappuis band.  (In very polluted situations, absorption by
N02 can also attenuate Fg(x) near the surface, and an additional term,
a N02^°2^k,k+l» is required in the equations which follow.  See Figure
3.1).  In a'plane-parallel atmosphere between grid points k and k+1 (Fig-
ure 3.2), the direct beam (solar zenith angle 60) is attenuated by 03 ab-
sorption along the path it traverses:


             FdirectU)  '  Fdirect'x)


i.e., [03]u fc+i = sec SotOslkfk+l' where [03]fce£+i is the column
depth (cm  ) along the normal"between k and k+I.  The direct flux at k
in turn is given by


           FdirectU)  =  Fo(A) exp <>sec 9° °03(X'T)

where [O^0 a  represents the entire overhead 03 column (top of the
atmosphere along a normal to level k).  The direct flux at 0 and 15 km,
calculated assuming a typical midlatitude 03 profile (0.36 cm-atm overhead
column), appears in Figure 3.3.  03 absorption is strongest in the near-uv,
and there is attenuation between 15 and 0 km only at X < 330 nm.

     The diffuse flux includes contributions from molecular and aerosol
scattering and radiation reflected from the surface and clouds.  Since
radiation is scattered out of the level between k and k+1 and is also
received from the surroundings,

              Fk+l      _  pk+1              Fk+l                       {6)
               diffuse      scattered in      scattered out '

^diffuse ls positive or negative depending on the balance between in-
coming and outgoing scattered fluxes.  Since molecules and aerosols are
concentrated near the surface and^cloud depths and levels are variable,
the degree of scattering, hence Fdiffuse, is strongly altitude-dependent.

     In molecular or Rayleigh scattering, all molecules absorb and scatter
radiation with a cross-section which is strongly wavelength-dependent,

                                     227

-------
    lO'16
CVJ
 E
 o  10"

 I
       17
z     ift
g  I0"18

o
LJ     ,Q
CO  10"l9

CO
CO
O  in-20
tr  iu
o


o  io-21
|  icr22

CO
CD

    IO'23
                                    NO-
I
                                     I
                                             I
           200     300   400    500    600

                       WAVELENGTH -nm
                                                   700
        Figure 3.1  Absorption cross-sections for 03 and N0£ in the
        uv and visible regions of the spectrum  (Luther and Gelinas,
                            228

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                              Direct  Solar  Beam
Figure 3.2
angle 0
      0
 Transmission of direct solar beam, incident
between two  levels of plane-parallel atmosphere
                     229

-------
      10
        16
CJ
 I
 E
 o
 c
 o
2.   I015  i
 o

 OL
 a:
 o
 CO
 o
 LJ
 CE

 O
      I014
      10
        13
            300
                                                                     700
             Figure 3.3   Direct  solar flux at 0 and  15 km as a function

             of wavelength,  X;  0.36 cm-atm total  overhead ozone column.

             Calculations based on extra-terrestrial  solar flux from

             WHO  (1981).
                                    230

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        « X'1*, and is significant only at \ < 450 nm.  Figure  3.4  shows
the Rayleigh scattering optical depth or extinction
for 1 and 15 km thicknesses and at ground  (Valley,  1965).  [M]+i  is
the normal molecular depth (cm~2) between  k and k+1.  Also given  are the
03 optical density at 15 km and ground and a typical aerosol attenuation
near ground.

     In molecular scattering, half of the  scattered radiation  goes  in the
forward direction; half goes backward.  Since TRay  per  km is   greatest
near the surface, Rayleigh scattering gives a net loss  of flux  near  the
ground relative to the flux calculated assuming only 03  absorption
(^direct)'  Away ^rom the surface, backscattered radiation enhances  the
flux beyond the pure absorption value.  This can be seen in Figure  3.5,
which shows fluxes calculated with multiple scattering  and 03  absorption.
Results are given for 60° solar angle and  are qualitatively similar  for
other angles.  Ground albedo is assumed to be zero  in these examples for
all wavelengths so that the flux  shows the effect of molecular scattering
alone.  Although only altitudes to 15 km are shown  in Figure 3.5a,  the
diffuse radiation from Rayleigh scattering reaches  a maximum at 20-30 km
and decreases with increasing altitude (Luther and  Gelinas, 1976).   When
surface albedo is greater than zero, the diffuse flux includes  a  substan-
tial contribution from reflection of both  scattered and direct  radiation,
An example appears in Figure 3.5b, where the flux at 15 km is  shown  as
calculated with molecular scattering and three values of albedo.
     Table 3.1 lists some of the major photodissociating  species  in  the
urban atmosphere.  Photolysis rates calculated  from  Eg.  (2)  (solar  angle
= 60°) are illustrated for two photolyses  of  ozone,  Jo3,  which  produces
O^D), and JQ , which. gives 0(3P)  (Figure  3.6).  Surface  and scattering
effects on JQ  and JQ  illustrate  different sensitivities of a  uv and
visible absorber since the absorption maximum to produce  O^D)  is at 290  nm
and that of 03 •»• 0( P) is at 600 nm (Figure 3.3).  For example, looking at
the zero-albedo curves in Figure 3.6, it is clear  that ozone absorption and
molecular scattering in the near uv produces  a  stronger altitude  gradient
in Jo3 relative to JQ  (cf. the altitude pattern of  the  direct  flux  in
Figure 3.3).  The effect of surface reflection  is  also different  for J(j3
and jQ3, and is consistent with the flux pattern of  Figure 3.5a.  Surface
albedo is much more effective for  Jg^ than for  JQ  ,  because  the Chap-
puis absorption is located where the atmosphere il nearly transparent
(A > 400 nm, Figure 3.1), and the  reflected flux is  transmitted upward with
little loss of intensity.  The choice of Luther and  Gelinas1  (1976)  calcu-
lation of Jg3 to illustrate the sensitivities of a uv absorber  has  been
made for convenience.  In fact, a  temperature-dependent quantum yield  for
the 03 -»• Ql1^) photolysis (NASA, 1981) increases JQ  at the  ground  rela-
tive to Jg3 at 15 km.  Molecular scattering is  discussed  more fully  by
Luther and Gelinas (1976)," and its effects on trace  gas chemistry are
described by Luther et al. (1978).  The latter  paper emphasizes strato-
spheric chemistry.  Two recent studies of  chemical effects of multiple
scattering and surface albedo discuss tropospheric chemistry more ex-

                                     231

-------
a.
UJ
o
o
h-
Q.
O
                                     14,15 km
                                	0,  I km
           300
350
400
450
                         X(nm)
     Figure 3.4   Optical depth (per km) versus wave-
     length, X, due to  63 absorption and Rayleigh
     extinction in the  upper troposphere (14-15 km)
     and  in the lowest  km.  Also shown  is the optical
     density due to aerosols near the ground,  Optical
     depths taken from  Valley  (1965).
                        232

-------
o
o.
V)


X
ID
-I
U_
      300    400   500    600
                    X(nm)
700      400    500   600    700
                X(nm)
       Figures 3.5a and 3.5b   Effects of molecular  scattering and surface
       albedo on fluxes calculated for solar zenith  angle 60° and wavelength
       A.  Fluxes are presented as a ratio of fluxes calculated with scattering,
       surface reflectance and 03 absorption flux  (ms) relative to fluxes
       calculated with 03 absorption flux (pa)  only:
       (a) Flux at four levels in the troposphere  with ground albedo equal
       to zero shows the effect of scattering only;
       (b) Flux at 15 km for three values of surface albedo (alb) shows
       the effect of surface reflectance  (Thompson, 198Qb).
                                   233

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           Table  3.1
Major Photodissociating  Species
    in the Urban  Atmosphere
      03 + hv * 0(1D)  + 02

      03 + hv > 0(3P)  + 02

       N02 + hv •»• NO  + 0

      HN03 + hv * N02  + OH

        H202 + hv -»• 2  OH

       N03 + hv ->• NO  + 02

       N03 + hv -»• N02  + 0

      H2CO + hv -»- H + CHO

      H2CO + hv * H2  + CO

      HONO + hv -»• NO  + OH

    CH3CHO + hv -»• CH3  + HCO

      HNOi+ + hv ->• products

  (CH3)2CO + hv * CH3  -H CH3CO

    CH3OOH + hv * CH30 + OH

     N205 + hv •»• NO2  + NO3
                234

-------An error occurred while trying to OCR this image.

-------
tensively (Demerjian et al., 1980; Augustsson  and  Levine,  1982).

     Uv-visible differences are also apparent  in the  diurnal  variation  of
photolysis rates.  Figure 3.7a,b  (from Demerjian et al.,  1980)  shows  JMQ?
and Jg3 calculated as a function  of local .solar time.  Because  03  extinc-
tion increases rapidly with solar angle, OQ  is more  sharply  peaked  about
the noontime maximum than is JNQ..

b.  Aerosol  and cloud effects

Aerosol s

     Flux calculations which include aerosol scattering are more compli-
cated than Rayleigh scattering because the flux from  aerosol  scattering
(i.e.,  the phase angle distribution of scattered radiation and  the inten-
sity integrated over all angles)  depends on the shape  and  size  of  the
aerosols.  If the scattering is mostly peaked  forward, then the principal
effect of an aerosol  layer close  to the surface is absorption  (i.e.,  simple
attenuation of incident radiation and not much backscattering).  This be-
havior characterizes background tropospheric aerosols  (Logan  et al.,  1981).

     For a moderately to highly polluted aerosol situation, however,  Demer-
jian et al.  (1980) find that approximately 9Q% of  the  total extinction  is
due to scattering.  The Demerjian et al. (1980) calculations  also  show  that
when aerosols are present at concentrations typical of high pollution sit-
uations, 3-5% less visible radiation and 15-20% less  uv radiation  reaches
the surface than when no aerosols are present.

Clouds

     Clouds represent the major cause of perturbation  to  the  tropospheric
radiation field, and their effects must be included in the calculation  of
photolysis rates.  These effects  are highly variable,  depending on cloud
height, thickness, type, number of layers, and zenith  angle.  This can  be
seen in Figure 3.8, which shows cloud reflectance  as  a function of h/L  for
a cloud of thickness h, where L is the mean free path  of  a light ray, i.e.,
a measure of cloud density.

     It is convenient to think of cloud effects in three  categories:  (1)
above cloud, (2) below cloud, and (3) within cloud.   Above a  dense cloud
layer,  radiation can be calculated as in a clear sky  with  the cloud  as  a
reflecting surface instead of the earth.

     Below-cloud radiation can be approximated (Demerjian  et  al.,  1980) by
multiplying the clear-sky flux by a semi-empirical correction factor.  At-
water and Brown's (1974) formulation can be used:


                           n [1 - f, (1 - T.)]                           (8)
                          1 =1      1       ]

where n = the number of cloud layers, f^ = the amount (coverage) in  the
ith layer, and T-j = transmission  of the layer, a function  of  cloud type.

                                     236

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10.0
                            10      12      14

                              TIME, hrs L.S.T.
16
18
20
      Figure  3.7a    Diurnal  variation of the photolytic rate constant
      for  the formation  of 0(^0)  for 63 in Los Angeles on 21 June at
      the  earth's  surface  and  at  three levels above the surface
      (Demerjian et al., 1980).
                                  237

-------
    14.0
=  12.0
o
4-
O
o
CJ
cc
     10.0
 ~    8.0
o
      6.0
      4.0
      2.0
      0.0
                                 10      12      14

                                    TIME, hrs L.S.T.
16
13
20
          Figure  3.7b   Diurnal variation of the  photolytic rate constant
          for  the formation of 0(3p) from N0£  in  Los  Angeles on 21 June
          at the  earth's surface and at three  levels  above the surface
          (Demerjian et al.5 1980).
                                      238

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-------
Haurwitz's (1948) transmission functions are usually  used  for  T-j.   At-
water and Brown  (1974) have demonstrated consistency  of  their  calculations
with both measurements and more exact calculations of  surface  radiation,
although Demerjian et al. (1980) point out potential  inaccuracies  in  apply-
ing Eq. (8).  One problem is lack of wavelength discrimination  in  Haur-
witz's (1948) functions.  Calculations of surface  radiation  by  Spinhirne
and Green (1978) as well as field measurements of  solar  fluxes  and photo-
lysis rates (Dickerson et al., 1980) reveal that clouds  block out  uv  20-30%
less effectively than visible radiation.  Thompson (1980)  has  incorporated
this distinction into a simplified cloud radiation calculation.  Thompson's
treatment also accounts for cloud reduction of surface albedo  to a very low
value independent of surface type and zenith angle.

     Examples of above- and below-cloud radiation  effects  are  shown in
Figure 3.9.  Fluxes (actually the ratio Fluxcloud/Fluxno cloud)  nave  been
calculated assuming that a single dense cloud layer exists in  the  mid-tro-
posphere.  As in the case of molecular scattering  and  surface  reflection
calculations (Figure 3.6), above-cloud flux enhancement  is greater in the
visible than in  the uv.  This alters the mid-to-upper  troposphere  ratio,
JNQ/JQO (Figure 3.10), and may have an appreciable effect on  above-
cloud chemistry  (Thompson and Cicerone, 1982).

     The simplest treatment of fluxes within a cloud  or  among  cloud layers
is to interpolate between cloud-top and cloud-base values, although in  some
cases internal reflections can actually enhance uv radiation above the
cloud-top values (Schmetz et al., 1981; Twomey, 1972).   To a first approx-
imation, these fluxes could serve to calculate photolysis  rates  for gases
dissolved in cloud droplets.  Graedel and Weschler (1981)  have  reviewed
aqueous-phase absorption spectra and quantum yields for  a  number of species
of atmospheric interest.  In general, aqueous absorption spectra are  simi-
lar to the gas-phase, but solvent cage effects typically cause  dissociation
quantum yields to be only 10~3 to 10   of their gas-phase  counterparts.

3.3  Photodissociation calculations in a regional-scale  model

     A regional-scale model must supply photolysis rates for chemical kine-
tics calculations at all daylight times and at every  point in  the  spatial
domain.  All the basic components of radiation vary in a regular way  with
solar zenith angle, while 03, aerosol, and cloud attenuation vary  irregu-
larly in space and time as meteorology changes.  For  some  species, the  ab-
sorption cross-section and/or quantum yields are temperature-dependent.
Thus, the potential computational problem is enormous; e.g., a  50  x 50  x  10
grid requires calculation of 2500 photolysis rates for each  species.   For-
tunately, some simplifications immediately suggest themselves,  and others
can be investigated fairly easily with existing models.

     The first simplification is that a fixed ozone and  N02  pattern can  be
assumed over the entire region.  Even in photochemical smog  situations,  the
principal local  perturbation to radiation is likely to come  from aerosols
or clouds rather than from tropospherically-produced  03  which  is only a
small part of the total overhead ozone column.  (Exceptions  to  this would
present a subgrid-scale problem and could be studied  with  a  one-dimensional
photochemical model.)  This means that chemical feedback on  the uv-visible

                                     240

-------
TJ

I 2.0
x  1 5
ID  ]'D
-J
LL
>^
"g  1.0

u

§ 0.5

u_

   0.0
SZA=30°                 . .
Cloud Reflectance{oejuvj
Ground Albedo-0.0
                                       ble)
              'Above Cloud (10 km)
                     Below Cloud (Okm)
            300
                            350            400
                                X (nm)
                                                  450
        Figure 3.9   Flux above and below cloud (as  a function of wave-
        length X) expressed relative to no-cloud conditions with zero
        surface albedo  in both cases.  Cloud  is represented as a single
        dense layer between 5 and 6 km with reflectance 0.8 in the
        visible and 0.6 in the uv.  Solar zenith angle is 30° (Thompson,
        1980b).
                              241

-------
 e
J£
o
 10
O
 CVJ
O
      0 Ground
         albedo'
— No cloud
— 0.8 Cloud  albedo

~ Ql(UV)}Cloudalbedo
                     1
                    20°             40°

                    SOLAR  ZENITH  ANGLE
                                  60*
     Figure 3.10   The effect of cloud reflectance on above-cloud ratio
     of photolysis rates: JNQ9/  jjjv  at 10 km.  Two cloud cases are shown.
     One assumes uniform reflectance (0.8) for all wavelengths;  the other
     assumes 0.8 reflectance in  the visible and 0.6 in the uv.  Surface
     albedo is  zero in both cases.  Cloud is assumed to be dense layer
     between 5  and 6 km, but result is similar if it is assumed to be
     located anywhere in the lower troposphere (Thompson, 1980b).
                               242

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radiation field can be neglected, and meteorological  variables  alone  can  be
used to compute fluxes.  The meteorology of a given  synoptic  situation  (in
terms that can be used to specify aerosol distribution  and  clouds)  can  be
used to calculate photolysis rates once and for all.  Thus, photochemical
processes can be driven with stored photolysis rates.

     Depending on the time resolution employed in  the regional  dynamic
model, another reduction in computation could come from interpolation of
photolysis rates at various times of day as is common practice  in  general
circulation models.  The interpolation might employ  a functional relation
derived from more exact temporally-resolved calculations  (e.g.,  Luther  and
Gelinas, 1976, or Demerjian et a!., 1980).

     Interpolation is only practical for clear sky conditions.   Even  then,
molecular scattering and surface reflection must be  included  in  those flux-
es which are actually calculated.  Highly accurate methods  (e.g.,  Luther
and Gelinas, 1976; Anderson and Meier, 1979; Demerjian  et al.,  1980)  are
too costly to use, but two rapid approximation methods  (Isaksen  et al.,
1977; Luther, 1980) are available.

     The inclusion of clouds and aerosols on a large scale  is more prob-
lematic because these phenomena can produce intense,  rapid, and  widespread
changes in the radiation field.  One approach would  be  to develop  a parame-
terization based on Coakley et al.'s (1983) treatment of  tropospheric aero-
sols.  An extension of Coakley's method (Charlock  and Ramanathan,  1983)
could be used to treat clouds.  The only required  meteorological input
would be total liquid water content.  Coakley's technique,  which is based
on direct and diffuse adding with the 6-Eddington  approximation  (Joseph et
al., 1976), would give sufficiently accurate radiation  fluxes for  photodis-
sociation rates.  However, we expect that the parameterization  adopted  for
use in a regional-scale model could be developed from calculations made at
a few key wavelengths, and the final choice of technique  would  strike a
good balance between accuracy and computational economy.

     Clouds and aerosols also raise the question of  subgrid-scale  radiation
effects.  Fog, haze, and low clouds which form over  a limited region  can
give rise to a rapid oxidation of S02 and N02 through solution  phase  chem-
istry.  There is a concomitant effect on radiation which  is important to
calculate correctly.
                                     243

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                                CHAPTER SIX

                   DEVELOPMENT OF ACID DEPOSITION MODELS
     In this chapter, we take a more forward-looking  view  toward  develop-
ment of a new generation of acid deposition models.   Based largely  on  the
topics reviewed in earlier chapters, we focus on essential  components  and
practical issues involved in developing a comprehensive model,  with extra
emphasis on topics needing great improvement or omitted in present  models.
Specifically, this chapter discusses needed emissions data;  salient fea-
tures of long-range transport of pollutants; features and  mechanisms of
acid rain chemistry that are necessary to embody in a credible, compre-
hensive model; cloud types, processes, and scales  involved in  pollutant
transfer and chemical transformations; and the mechanics and overall  phe-
nomenology of dry deposition.  Further, we enumerate  key issues and guiding
principles on model resolution, pertinent numerical methods, and  strategies
for model validation and sensftivity analysis.
1.  EMISSIONS

1.1  Introduction

     Before defining specifically which emissions  are  central  to the acid
rain problem and what kind of data are needed,  let  us  recognize  the  need
for specific and detailed information.  Regardless  of  whether  one sees the
acid deposition model as an assessment tool  for  regulatory  policy or as a
purely scientific construction without intended  practical  utility,  it is
clear that the acid rain phenomenon originates with  ground-level  (or near)
emissions.  While it is true that there are  upper  atmosphere  sources of
acidic gases, e.g., NOX produced by lightning, we  know that these are not
often significant compared to other more obvious sources,  e.g.,  S02  from
coal burning and NOX from internal-combustion engines.

     For modeling purposes, very detailed  information  is  required for a
number of chemical species.  An inventory  of emissions with suitably re-
fined spatial and temporal resolution is required  as input  to  a  regional
acid deposition model before any serious investigation of  the  principal
sources of deposited acids can be mounted.   At  present, major  unresolved
scientific questions include the relative  importance of local  and distant
sources, the contributions of mobile and stationary  sources,  the influence
of natural emissions, and the significance of other directly  emitted pol-
lutants which affect the conversion of acid  precursors to  acids.  In this
section, the type of information required  to address these  questions is
discussed and the adequacy of existing data  bases  to meet  these  require-
ments is reviewed.

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1.2  Needed data for an emissions inventory

a.  Chemical species

     Because the principal acids in North American precipitation  are  sul-
furic and nitric, it is quite clear that accurate estimates of  regional  S02
and NOX influxes into the atmosphere are required.  Although S02  and  NOX
are the major acid precursors, a spectrum of other species significantly
influences or contributes directly to acid formation.  These include  the
volatile organic carbons (VOC) and carbon monoxide, because of  their  role
in the oxidation process; ammonia (NH3), because of its  role as a buffering
agent in cloud chemistry processes; and several reduced  sulfur  species,  be-
cause of their potential importance as naturally emitted precursors to  acid
rain.  In addition, sulfate aerosols are thought to contribute  significant-
ly to the overall sulfuric acid budget.

     Other direct sources of acidity must also be considered.   In certain
regions, hydrochloric acid and occasionally hydrofluoric acid vapors  can be
incorporated into clouds and precipitation in non-negligible amounts.   Di-
rect contributions to acidity from organic acids are possible,  although
some data from Los Angeles suggest a minor role (Lil jestrand, 1980).  By
contrast, Keene et al. (1983) and Galloway et al. (1982)  have found direct
and indirect evidence of major contributions to total  precipitation acidity
from weak organic acids.  Their data are from remote sites (Australia and
Venezuela); the organic acids might arise from biomass burning.   While  not
likely to be ubiquitous or regular in North American precipitation, the or-
ganic acid possibility needs attention.  Finally, in some localized areas,
sea-salt particles or coarse aerosols (those with diameters greater than
2.5 jjm) can be important to acid production.
     Less directly, but important in chemical transformation  pathways,  are
those substances that affect oxidant production.  As  discussed  in Chapter
V, oxidants like 03) H202, and organic peroxides play key  roles  in  acid
production.  Thus, emissions of species like reactive hydrocarbons  and
nitrogen oxides are important as sources of oxidants.

     The buffering aerosol species  (the alkaline dusts)  and the  aerosol
components important to catalytic conversions in aqueous reactions  (e.g.,
soot, iron, and manganese) are also important in determining  precipitation
acidity; their emissions are difficult to quantify, as an  important com-
ponent is wind-driven and natural.

     Ammonia emissions deserve special note.  As a  potentially  important
buffering gas, emissions inventories are needed.  Though often  thought  to
be naturally produced by microbes in soils and waters, one must  also real-
ize that much NH3 emission is stimulated by man's activities  in  localized
areas— although biogenic, ammonia release to the atmosphere is  not  wholly
natural.  The localization of fixed-nitrogen application (fertilized
fields) and waste collection (cattle feedlots and municipal waste plants)
makes it possible to estimate regional ammonia emissions.
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b.  Classification of sources

     The total emissions of many of these  pollutants  are  dominated by  man-
made sources.  For VOC's, NH3, and the  reduced  sulfur  species,  as  well  as
some of the aerosol components, and possibly NOX,  natural  source  inven-
tories are needed for a complete emissions  inventory.

     Man-made sources are comprised of  point and  area  sources.  Point  and
stationary area sources can be classified  as industrial,  commercial,  insti-
tutional, and residential sources.  Associated  with each  source is a  dif-
ferent mix of pollutants.  Because of these different  mixes,  it is impor-
tant to subdivide the mobile source into light  and heavy-duty  vehicles,
using either gasoline or diesel fuels.

     Natural  emissions result mostly from  soils,  vegetation  and animal
wastes, inland water such as marshlands, and, for  NOX,  from  lightning.

c.  Spatial scales

     Significant sections of the United States  and Canada must  be  included
in any acid deposition study.  Thus, comparable emissions data  are required
for both countries.  The appropriate subdivision  of such  a large  region is
still a matter of debate.  It is currently  thought that area  sources  can be
averaged over grids that are on the order  of 20 x  20  km.   Large point  sour-
ces, however, need to be considered individually  because  of  their  impact on
chemical and physical phenomena on a smaller scale (Lamb,  1982).   In  addi-
tion, the impact of a specific power plant  cannot  be  addressed  unless  each
major plant is considered individually  in  an inventory.

d.  Temporal  scales

     For many stationary sources, seasonal  averages or even  annual averages
are an adequate representation of the temporal  variations of  the  sources.
For some stationary sources such as home heating  and  for  mobile sources,
diurnal patterns are required for sufficient description  of  the temporal
variations of the emissions.  For these sources,  a representative  week/
weekend day diurnal pattern (hour by hour)  for  each season is  adequate.
Some natural  sources such as those controlled by  sunlight are  also defined
on seasonal and representative diurnal  scales.

e.  Number of inventories

     Typically, emissions inventories are  created for a base year. To ob-
tain an assessment of the effect of emissions changes  on  acid  deposition,
it would be very useful to have emissions  inventories  for two  different
years for which quantitative differences in emissions  exist  for at least
part of the model region.  The availability of  two emissions  inventories
would provide an opportunity to test a  model's  ability to predict  the  ef-
fect of emissions changes {see model validation section in Section 8  of
this chapter for discussion).
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1.3  Adequacy of existing data

     The major man-made emissions data  bases  are  described  in  Table 1.1.
Some sources of additional data for the development  of  a  natural  source
inventory are listed in Table 1.2.  Since  the available man-made  data  bases
are reasonably comprehensive for at least  the major  acid  precursors S02 and
NOX, more attention is given to a critique of the  less  well-documented
natural sources.

     It has been concluded (Galloway  and Whelpdale,  1980) that anthropo-
genic emissions of S02 exceed natural emissions of gaseous  sulfur compounds
by at least a factor of ten in eastern  North  America,  and a similar conclu-
sion has been reached for Europe (Semb, 1978).  This strong regional  domi-
nance of man-made sulfur  sources over natural  ones is  probably correct, but
the array of uncertainties that appears when  one  attempts a critical  review
of the actual data does not inspire great  confidence.   In the  case of  sul-
fur, there has been one systematic and  high-quality  field survey  of natural
gaseous sulfur sources (Adams et al., 1980).   Because  of  the remaining
problems cited below, estimates of the  natural S  emission rates for eastern
North America can be improved only at appreciable  cost.  Quantitative  com-
parisons of anthropogenic and natural sources of  NH3,  hydrocarbons, NOX,
and CO must await field measurements  of natural sources.  Presently,  only
gross estimates or spot measurements  of actual field emissions are avail-
able.

     Natural sulfur sources are known to be very  patchy spatially and  var-
iable with season; less well-known is the  fact that  the release of S-con-
taining gases from shallow coastal and  inland waters is strongly  dependent
on sunlight and pH, details of the microbial  ecology,  and,  of  course,  time
of day (Jorgensen et al., 1979; Hansen  et  al., 1978).   Further, the iden-
tity of the principal S-bearing compound,  usually  a  reduced-sulfur species,
that escapes these important environments  into the air  also varies with
time of day, largely because these shallow-water  sites  can  change from an-
oxic to oxygenated with time of day.  The  only serious  attempt to consider
most or all of these factors in a multi-site  field measurement program fo-
cused on natural sulfur sources (that of Adams et  al.), measured  H2S,  COS,
CH3SH, (CH3)2S, CS2, and  (CH3)2S2 emissions at about twenty sites, and
documented the soil types and related variables at each site.   Carefully-
controlled analytical methods also appear  to  have  been  used.  Extension of
the Adams et al. research with emphasis on more detailed  diurnal  and sea-
sonal variations and extension to Gulf  Coast  locations  seems advisable.
Also, as is common in all such work,  improvements  to flux-measurement
methods are needed (see below).

     Similar comments can be made about the effort at  measuring natural hy-
drocarbon emission rates  that was mounted  by  Zimmerman  in 1977 (see Table
1.2).  The number of distinct hydrocarbons that were analyzed  and the  anal-
ytical methodology are impressive.  Further,  the  vegetation and soil-typing
were performed systematically.  Extension  of  this  kind  of field program to
much larger areas and to  longer periods of observation  seems necessary.  To
be able to compare properly the natural hydrocarbon  and anthropogenic  emis-
sions, the full range of  variation of the  latter  needs  better  documenta-
tion.  For example, the temperature dependence of  the  evaporative loss from

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     Table 1.1  Major Currently Available Man-Made Emissions Data Bases
                                (EPA, 1982).
1.  National  Emissions Data System (OAQPS)

    Pollutants:  SOX, NOX, HC, CO, particulates
     Geography:  National, coordinate location for significant point -
                 sources country level  aggregation of all  remaining sources
       Sources:  All area and point-source categories
    Time Frame:  1972-1980
2.  Eastern U.S. SOX Emissions Inventory (ORD-MITRE)

    Pollutants:  SOX
     Geography:  Eastern 32 states, state level  totals
       Sources:  All except electric utilities aggregated into nine source
                 categories
    Time Frame:  1980
3.  Electric Utility Emissions (ORD-E.H.P.A.)

    Pollutants:  SOX and NOX
     Geography:  National, coordinates for all point-sources
       Sources:  All electric utility plants
    Time Frame:  1976-1980
4.  MAP3S (ORD-BNL)

    Pollutants:  SOX, NOX, HC, CO, particulates
     Geography:  National, with Canadian sources.  Coordinates for
                 point-sources and county level area sources
       Sources:  All area and point-source categories
    Time Frame:  1979-1980

(This data base is the NEDS data base with some additions and modifica-
tions. )
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                           Table 1.1  (continued)



5.  U.S.-Canadian Work Group 3B Data  Bases

a.  1978 Data Base

    Pollutants:  SOX only
     Geography:  National, U.S. and Canada--U.S.—major point-sources,
                 county level  area sources in the East, State  areas  sources
                 for Western States.   Canada—major point-sources  and area
                 sources in 127 km grids.
       Sources:  All sources aggregated to 10 categories
    Time Frame:  1978

(The U.S. portion of this data base was constructed from parts of  1  through
4 above to meet immediate needs for atmospheric modeling.)

b.  1980 Data Base

    Pollutants:  SOX and NOX
     Geography:  National—U.S. and Canada—U.S.—State level  totals.
                 Canada—major point-sources and  area sources  in  127 km
                 grids.
       Sources:  All sources aggregated into six  categories.
    Time Frame:  1980

c.  Preliminary Estimates

    Pollutants:  Primary Sulfates, VOC, Trace Metals
     Geography:  U.S. and Canada—U.S.— State level.  Canada—province
                 level.
       Sources:  All sources aggregated into major categories
    Time Frame:  1980
6.  Northeast Corridor Regional  Modeling Project (NECRMP)  Inventory
(OAQPS)

    Pollutants:  NOX, VOC, CO
     Geography:  14 Northeastern States plus D.C.   All  sources allocated to
                 20 x 20 km grid squares.
       Sources:  All area and point-sources
    Time Frame:  1979, 1980 allocated to hourly emissions
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      Table 1.2  Some Currently Available Natural Emissions Data Bases
1.  EPRI-^Washington State University "Biogenic Sulfur Emissions in the SURE
    Region"
    a.  1980 Data Base
        Species:  Gaseous H2S,  COS,  CH3SH,  (CH3)2S, CS2, CH3SSCH3
        Geography:  Eastern U.S.  excluding deep South
        Sources:  Inland waters and  soils (various types)
        Time Frame:  9/77-9/79
    b.  1982 Data Base (not yet available)
        All categories as above,  except that geographical area was to be
        Gulf Coast and field studies were to begin after those listed above
        were completed.
2.  EPA-Washington State University  "Determination of Emission Rates of
    Hydrocarbons from Indigenous  Species of Vegetation in the Tampa-St.
    Petersburg, Florida, Area"
    Species:  CH^, total nonmethane  hydrocarbons, parafins,  olefins,
              aromatics, plus several  other species
    Geography:  Tampa-St. Petersburg,  Florida, area
    Sources:  Most indigenous plant  species
    Time Frame:  6/77-8/77
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liquid reservoirs is potentially important  (Zimmerman,  private  communica-
tion).  Changing emissions-control  strategies also mandates  that  the  com-
bustion source of man-made hydrocarbons be  reviewed  regularly.

     Key gaps in the available data on natural  sources  are  in NH3  emis-
sions, NOX sources and possibly CO emissions, and  in  the  effects  of dis-
tant natural surfur sources (Galloway and Whelpdale,  1980;  Granat,  1978).
There is no NH3 emissions inventory at all  for  the midwestern or  eastern
United States or for Canada, although a state-by-state  survey is  now  being
prepared (R. C. Harriss, private communication).  Also, R.  Husar  (private
communication) is preparing NH3-source, NH^"*"  deposition surveys for Morth
America, and G. Cass (private communication from J.  Seinfeld) has  recently
expanded NH3 sources for the Los Angeles area.  Reliable  field  measurements
of NH3 losses from fertilized fields, animal  pastures,  and  cattle  feedlots
are extremely rare, even though nitrogen-balance studies  imply  that NH3
losses can account for 20-50% of all deposited  fixed  nitrogen (Liu  et al.,
1977).  The midwestern U.S. should be a major source  of gaseous NH3 to the
atmosphere because of the intensive use of  fixed-M fertilizers  there.  Hut-
chinson et al. (1982) very competently measured NH3  and amine losses  from a
Colorado feedlot in 1982, and one or two Australian  publications  exist to
guide our estimates of NH3 sources.

     For NO and N0£, there are tantalizing  indications  in the literature  c-f
soil science and atmospheric chemistry of soil  sources  of NO and  possibly
of N02, but little if any quantification.   Not  to  be  confused with  dry de-
position to soils and other surfaces as a loss  process  for  atmospheric N02,
these potential soil sources are microbial  nitrification  and denitrifica-
tion, as for N20.  The production of NO and N02 in lightning events is cer-
tain; the actual amounts produced per event and/or annually  are uncertain.
A recent review (Bauer, 1982) estimates that  about 1.5  million  metric tons
(N) are produced annually in the latitude belt  30-50°N, mostly  over conti-
nents.  Electrical storm activity is sporadic.  Accordingly, there  could  be
important NOX contributions from individual events.   Sporadic intrusions
of stratospheric ozone to near ground level have occasionally led  to  03
concentrations above air-quality standards; on  an  event basis,  lightning-
produced NOX and 03 from distant sources might  be  analogous.

     Finally, a number of endemic weaknesses  in all  natural  source  assess-
ments appear when one attempts a critical review.  These  include  inadequate
flux-measurement methods, overreliance on deposition  data and assumed re-
gional or global steady-state elemental cycles  in  the deduction of  source
strengths, too fe* empirical data on diurnal  and seasonal  variations, and
almost no basic understanding of the mechanisms that  drive  the  release of
gaseous sulfur (or gaseous hydrocarbons or  NOX  or  NH3).   For example, in
many field measurements of fluxes, it has been  necessary  to  use closed
chambers that can perturb the system under  study in  many  ways.   Micro-
meteorological ly- and biologically-acceptable methods are not generally
available, often because of a lack of appropriate  analytical chemistry
technology for the species at hand.  Similarly, when  deposition data  are
used (e.g., for SOt^, N03~, or NH.,4"} tc deduce  source strengths,  one  must
carefully include the potential effects of  long-range transport and of dry
deposition (usually characterized poorly),  and  proper spatial coverage and
temporal averaging must be used.  It also appears  that  assessment  of

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ral sources has been performed better  by Europeans  than  by  Americans,  and
often with a global point of view rather than  regional.

     Assuming that natural S sources are negligible  compared to regional
man-made inputs (Whelpdale and Galloway, 1980;  Adams et  a!.,  1980),  then
for an adequate regional acid deposition model  we must still  include spa-
tially-resolved man-made sources (see  below) and  natural  sources for NH3
and possibly NOX (at least the lightning-produced NOX).   Creating
model-compatible source grids and assessing model sensitivities to the
adopted N03 and MOX emissions remains  to be done.

     Source inventories for HC1, HF, and the various aerosol  species are
also inadequate at. this time.  Local measurements exist,  but these have yet
to be assembled into an appropriate regional inventory (NAS,  1979).   Al-
though total suspended particulate inventories  are  available,  these  are
bulk estimates of total aerosol  mass and thus  do  not provide the detailed
information required in the model.

     A brief summary of pollutants and the status of their  inventories is
given in Table 1.3.  Major research efforts are required  for NH3 and the
aerosols.  Careful and appropriate spatial and  temporal  discrimination is
needed for the point and area sources  of all of the  pollutants.  Some tech-
niques (e.g., EPA, 1982) for obtaining these discriminations,  such as the
diurnal  patterns of mobile sources, are available.

     A major concern regarding all of  the existing  data  is  the lack  of un-
certainty estimates.  Such information is crucial to a proper use and eval-
uation of any model.

     The list of species and sources presented  here  should  not be consi-
dered to be complete.  Future research may identify  other important  pollu-
tants.  Thus, flexibility in the emissions data input design is of primary
importance in the development of an acid deposition  emissions inventory.

1.4  Subgrid issues

     Emissions, whether at the surface or from  elevated  sources, tend to  be
subgrid-scale phenomena; that is, the  source is inevitably  smaller than the
grid volume of the numerical model.  Thus, for  the  reasons  discussed later
in this chapter, the model necessarily deals only approximately with the
emissions.  Furthermore, the initial dispersion of  emitted  material  from
both surface and elevated sources depends strongly  on the state of the
PBL.  During the day, when the PBL is  convective, both  vertical and  lateral
dispersion are much larger than at night when  the PBL is  stably stratified.
Thus, the same source can give radically different  concentration distribu-
tions in the first grid volume, depending on the  time of  day.

     The subgrid problems which this creates have not yet been completely
solved.  However, we do know a good deal about dispersion from both  surface
ana elevated sources in the PBL; this  would seem  a  necessary ingredient for
the ultimate solution to the subgrid emissions  problem.   Some new effort
here seems appropriate during the development  of  a  regional  acid deposition
model.

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                   Table 1.3  Summary of Emissions Status
 GASES

Sulfur
  SO 2
  H2S

Nitrogen
  NOX
Carbon
  VOC
  CO

Other
  HC1
  HF
      MAJOR MISSING FEATURES
20 x 20 km
20 x 20 km, some categories
20 x 20 km beyond 14 eastern states
20 x 20 km, some categories
20 x 20 km beyond 14 eastern states
20 x 20 km beyond 14 eastern states
20 x 20 km, some categories
20 x 20 km, some categories
AEROSOLS

Sulfate

Alkaline dust

Catalysts
20 x 20 km, some categories

20 x 20 km, some categories

20 x 20 km, some categories
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2.  LONG-RANGE TRANSPORT OF POLLUTANTS

     It is well known that pollution affects  not  only  people  in  the immedi-
ate vicinity of the source, but also those people  hundreds  to thousands of
kilometers downstream.  For example, sulfur dioxide  emitted in one  country
may lower the pH of rain to a value of 4 or less  in  other countries (Li-
kens, 1976).

     When regional air quality is considered,  the  temporal  and spatial  var-
iation of the meteorological parameters (the  three-dimensional wind compo-
nents, the vertical temperature structure, the  humidity, and  the precipita-
tion) become more important than in localized  air  quality problems.  On the
time scales of many pollutants that affect regional  air  quality  (6  to 48
h), the horizontal winds vary in speed and direction,  the vertical  trans-
port by the mean vertical motions becomes important, and the  height of the
mixed layer may vary considerably.  Furthermore, many  of the  pollutants may
react with other pollutants or be removed through  processes which depend on
the meteorology—particularly the humidity and  precipitation.

     The general goal of an air quality model  is  to  forecast  the concentra-
tion of a contaminant, Q (in dimensions of mass per  volume),  over space and
time, given the initial conditions on the atmospheric  structure  and on the
distribution of Q, and given the boundary conditions.  For  limited  domains,
the boundary conditions generally consist of  the meteorological  and concen-
tration variables on the upwind side of the domain (lateral  boundary condi-
tions); the conditions at the surface, including  surface heat,  moisture,
and momentum fluxes; the emission rates in space  and time over the  domain;
and appropriate upper boundary conditions.  We  then  solve the equation for
the time rate of change of Q(x,y,z,t)
    =-Vu.vQ-w-_ QV-V - Vu  • V' Q1  - -Ir- +  sources  + sinks,  (1)
 3t     ~H          3Z       -    n   ~n        9Z


given Q(x,y,z,t0), the time-dependent mean1  horizontal  and vertical  ve-
locities (YH and WK tne horizontal and  vertical  eddy  fluxes  represented
by VH*VH'Q  anc* 3w'Q'/3z, and the volume sources  (emission rates)  and
sinks fe.g., deposition, rainout, reactions).

     It is obvious from Eq.  (1) that the mean wind  and the turbulent fluxes
play a major role in determining the behavior  of  the concentrations.  Gen-
eral, predictive meteorological models  (discussed in Section 4 of  Chapter
III) contain forecast equations for these  meteorological  processes.   To
understand the acid deposition problem  fully,  it  is necessary  to account
for complex, three-dimensional mesoscale (horizontal  scales of 2.5 km to
2500 km) processes such as cumulus  convection.  For example,  if strong
cumulus convection is present, pollution in  the mixed  layer may be trans-

     :Here the mean refers to averages  over  appropriate space  and  time
scales.  In a grid-point numerical  model,  for  example,  the spatial average
is the average over a single mesh volume;  the  time  average is  over one time
step.

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ported to the upper troposphere  (height  ~ 8  km)  in  a  matter of  minutes;
ordinarily, mixing through this  depth .night  require days.   Furthermore,  the
precipitation associated with the convection may  act  as  a  very  efficient
removal mechanism; approximately 86  percent  of  the  sulfates in  the atmo-
sphere are removed by precipitation  (Kellogg et  al.,  1972).

     When considering a general  acid deposition  model,  it  is convenient  to
break the total model into two major components—a  meteorological  model  (of
the type reviewed in Section 4,  Chapter  III) and a  chemistry model.   The
meteorological model provides the meteorological  variables that affect the
transport, diffusion, and reaction of Q.  These  variables  are then utilized
in the pollutant model to forecast the advection  and  diffusion  of  Q.   If Q
is passive--that is, its behavior does not appreciably  affect the  meteor-
ology—the meteorological and pollutant  models  may  be run  in series.   The
meteorological model is run first; the appropriate  data  are stored and then
used in the subsequent air quality model.

     The importance of utilizing three-dimensional, time-dependent meteoro-
logical models that contain the  relevant physics  on regional-scale air
quality modeling can be seen by  considering  the  variability of  trajectories
on the appropriate time scale of 0-2 days.   Because of  the importance of
vertical motions on the movement of  air  over periods  of  a  day or more, cal-
culation of trajectories on these time scales must  consider the three-di-
mensional atmospheric motions unless the pollutants are  trapped in a  well-
defined mixed layer.  The combination of typical  synoptic-scale vertical
motions (5 cm/s) and moderate vertical wind  shear can lead to significant
differences between horizontal and three-dimensional  trajectories  over
24 h, especially when the wind changes direction  with height.  For example,
let the wind change linearly from west at 10 m/s  at a height of 1  km  to
east at 10 m/s at a height of 3  km.  If  the  vertical  velocity were constant
at 2.3 cm/s during the 24 h period,  the  parcel  would  rise  from  1 km to 3 km
in 24 h.  Its average east/west  velocity during this  period would  be  zero,,
and so its true horizontal displacement  would be  zero.   A  constant-level
trajectory, however, would erroneously place the parcel  864 km  downwind!
Utilizing real data, Danielsen (1961) has found  similar  errors.

     Figure 2.1 illustrates a 24 h trajectory computed  from the three-
dimensional forecast wind field  in a regional numerical  weather prediction
model (Anthes et al., 1982a).  The parcel originated  at  850 mb  over the
Texas-Oklahoma border, flowed horizontally northward  in  a  low-level  jet,
and then rose rapidly in a frontal zone  over Iowa to  a  pressure of 300 mb.
Such trajectories are not unusual in regions of precipitation.

     General meteorological models capable (with  some modifications)  of
providing the necessary meteorological variables  to an  air quality model of
acid deposition are reviewed in  detail in Section 4 of  Chapter  III.   The
operations in these models consist of:   (1)  measuring initial values  of  the
dependent variables, such as winds,  surface  pressure, temperature  and mois-
ture; (2) analyzing these data to produce consistent  three-dimensional ini-
tial fields; (3) applying boundary conditions on  the  edges of the  domain;
(4) modeling important physical  processes such  as advection; turbulent
fluxes of heat, moisture, and TOmentum;  radiation;  and  condensation;  and
(5) solving numerically the finite difference equations  that represent the

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 100
 500
1000
            Figure 2 }    24 h trajectory of air parcel  originating at
            850 mb at 0000 GMT, 25 April 1979 (Anthes et  al .,  1982a)
                               256

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processes in (4).  Each of these complex component  operations  is  discussed
in Chapter V.  As discussed in these sections, considerable  progress  has
been made in developing accurate techniques  and  realistic  physical  param-
eterizations for modeling regional atmospheric flows.   It  is therefore
feasible to develop and test fully such models on the  regional  acid
deposition problem.
3.  ACID RAIN CHEMISTRY

     In the discussions in Sections  1  through  3  of  Chapter  V  of  this  re-
view, we have learned that there is  a  great  diversity  and seeming  complex-
ity of the reaction channels  in the  troposphere  which  convert S02  and NOX
into H2S04 and HN03, respectively.   Obviously, all  of  these many  reactions
are not required in an operative acid  generation  and precipitation model.
Some reasonable accuracy for  the chemical  transformations leading  to  acids
can be maintained with a much simplified  reaction scheme.   Sensitivity
studies allow one to arrive at some  minimum  set  of  reactions  for  use  with
any given model which will provide the  desired level of  accuracy.   Our cur-
rent review and evaluation gives some  guidance in this choice.  The follow-
ing reactions are judged to be of primary  importance for acid generation
for tropospheric conditions which are  commonly encountered:

       Gas Phase:     HO + S02 (+M)  +  HOS02  (+M)  -  - - * H^           (1)

                      HO + N02 (+M)  -»•  HN03 (+M)                          (6)

       Liquid Phase:  S(IV) + H202 * H^O,, + ...                        (60)

                      S(IV) + 03 * H2SOk  + ...                          (59)

                      S(IV) + HO •»• H^Oi,  + ...                          (61)
                      S(IY) + H02(02") + ti2SQ*  •••                   (62,63)

                      S(IY) + N03 + H^  ,..                           (64)

                      N205 + H20 •»• 2HN03                                (77)

     The gas reactions  (1) and  (5) appear  to be major  acid  forming steps  in
the troposphere.  Reactions of  S02 with 0(3P),  CH202  (and other  Criegee in-
termediates), CH302, etc., may  also contribute  to  the  acid  generation,  but
the conditions necessary for their significant  occurrence are  probably
rare.

     When gaseous S02 encounters cloud water, fog,  or  rain  water,  it dis-
solves in part to form  S(IV) species  (S02-H20,  HS03~,  SO,+=,  and  H30+),
The reactions of these  species  with various water-soluble,  oxidizing impur-
ities in the water can  occur and lead to acids.  Thus,  reactions 60 and 59
of the S(IV) with H202  and 03 are expected to be very  important  acid-form-
ing processes in the liquid water-containing air masses.  The  reactions
61-64 and 77 involve gas-phase-generated,  transient species  wnich  are
transported to and captured by  the water particles.   If  the  fraction of

                                      257

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the species captured per collision  is  sufficiently  high  (greater than about
1 x 10~3), then these reactions appear  in  theory  to  be very  important in
clouds; state-of-the-art models of  acid  generation  and transport should
include them,  Further work on the  experimental evaluation of  the capture
coefficients will be necessary to quantify  the  estimates  of  the rates of
these processes within the troposphere.  In addition, the reactions of
other oxidizing agents such as PAN  (peroxyacetylnitrate),  H02N02 (peroxy-
nitric acid), and CH302H (methyl hydroperoxide),  etc., may be  important,
although further experimental work  will  be  necessary  to  define these possi-
bilities better.  State-of-the-art  models  should  include  these reactions if
and when they are shown to be important.   For certain relatively uncommon
conditions encountered in highly polluted  atmospheres (e.g., urban fogs),
the Fe3+, Mn2"1", and the graphic carbon-catalyzed  reactions of  S(IV) with 02
can be significant sources of acid; provision for their  inclusion for these
cases should be made.

     The homogeneous gas phase chemistry typical  of  the  reactions in smog
must be included to generate in a realistic fashion  the  concentration-time
profiles for the reactive species (HO,  03,  H202,  N03, N205,  H02> etc.)
which are responsible for the acid  production in  the  above reactions.  Two
somewhat sophisticated models developed  and tested  by Atkinson et al.
(1982b) and Whitten et al. (1982) are  available to modelers  today.  Both
the reaction scheme of Atkinson et  al.  (1982b)  and  that  of Killus and Whit-
ten have relatively large numbers of  reactions  (80  and 75, respectively,
excluding S02 chemistry) which are  required to  explain the hydrocarbon-
NOX chemistry in the troposphere.   We  feel  that the  formulation of the
chemical module of an acid deposition  model with  either  of these rather
extensive reaction schemes, together with  the very  extensive meteorology,
cloud chemistry, etc. in the other  modules, would lead to a  rather restric-
ted use of the model as a result of its  large demand  for  running time.  As
a consequence, we feel that one should develop  a  somewhat simpler operating
chemical package, hopefully of near equal  accuracy,  to simulate the gas
phase oxidation of S02 and N02.  There  are  two  approaches which could be
used in this development.

     The first approach involves an extension of  the  method  employed pre-
viously by Lavery et al. (1978, 1980).   Isopleths are prepared for the
maximum 03 and HO-radical concentrations as a function of the  hydrocarbon-
MOX ratio using both the Atkinson et  al.  (1982b)  and the  Whitten et al.
(1982) models, updated and expanded to include  the  S02 chemistry as out-
lined previously as a basis for the estimates.  These isopleths are made
for several seasons [summer, fall (or  spring),  and  winter] at  40°N lati-
tude.  These are keyed into a program  which for a given  RH-NOX simulation
mixture at a given time selects the proper HO-max levels. This is atten-
uated by the appropriate sunlight intensity function  to  provide an HO-radi-
cal estimate for the given conditions.   Then  the  products of [HO][S02]k1
and [HQ][N02]k7 are used to derive  the  rate of  H2SOlf  and  HN03  generation in
the reactions 1 and 7, respectively.   Tne  sutf of  the  products  of the [HO]
[RHl-jk-j terms, where RH-j includes all  hydrocarbons  and aldehydes, is
used to develop the rate of H02 and R02  radical formation.   This is to be
used to drive the NO to M02 conversion  through  reactions  50, 53, and 10,
and H202 formation through reaction 58:


                                      253

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                            H02 + H02 * H202                          '  (58)

The rate constant for 58 is [H20] dependent and  is  adjusted  for  this  in the
simulation.  The ozone concentration is estimated from  the [N02]/[NO]  ra-
tio, and the relation 47 from Section 1, Chapter V  is corrected  for  expect-
ed deviations for conditions of low [NO].  The ozone so  evaluated  is  used
to derive the rate of Criegee intermediate formation and alkene loss
through the 03-alkene reactions.  The concentration of  hydrocarbons,  NO,
N02, 03, S02, H202, and aldehydes is updated  continuously as emission  and
loss from chemistry or deposition occur.  This method should allow an  ef-
ficient use of the computer time, since extensive integrations  are not re-
quired.  At every stage of the development of this  system, a check on  the
errors of the approximate methods is made, using the more complete reaction
schemes of Atkinson et al. (1982b) and Whitten et al. (1982), together with
the extensive experimental data of Jeffries et al.  (1982) derived  from the
outdoor smog chamber experiments.

     In the second approach, one attempts to  use a  simplified reaction
scheme which parameterizes the hydrocarbon chemistry.   Three hypothetical
hydrocarbons of different reactivity are used, which represent  the alkanes,
alkenes, and aromatic species.  The rate constants  for  the reactions  of
these species with HO and 03 are calculated as a concentration-weighted
average of the species in the mixture within  a given structural  class  at a
given time.  The reaction of HO-radicals and  03 with these species is  par-
titioned between the various species according to their relative reactivi-
ties, and the composition of the mixture is regularly recalculated.   This
is used to redetermine the new average rate constant, etc.

     The yield of products of the reactions,  namely H02, R02, CH20,  CH3CHO,
etc., is a function of the composition of the mixture at any time, and is
updated regularly from the prepared stoichiometry tables.  Through such an
approach, one can save considerably on the integration  time  required  for
the large number of reactions in most detailed mechanisms.   The  bookkeeping
job of establishing the average rate constants for  the  hydrocarbons  and the
product distribution in the reaction mixture  can be handled  efficiently
through the computer.  A similar simplification  is  envisaged for the  alde-
hyde and ketone product chemistry.  The average  rate of photochemical  gen-
eration of reactive species from the carbonyl compounds  (H02, CH302)  etc.)
and the distribution of these products can be adjusted  through  the use of
the averaging techniques, tables of product distributions, and  the book-
keeping procedures of the computer.


4.  CLOUDS

4.1  The roles of clouds in acid rain

     Clouds have diverse roles in the acid rain  process, as  Figure 4.1
shows.  While several of these processes have been  described in  previous
sections, it is worthwhile to consider them once again  as a  whole.  The
most important processes associated with clouds  appear  to be these:
                                     259

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            EFFECT ON
             J's AND OH
                            TRANSPORT TO
                            UPPER TROPOSPHERE
      CHEMICAL^
      REACT!ON(
    IN DROPLETSy
       AND RAIN f
ORGANIZATION OF SURROUNDING
        MESOSCALE MOTIONS
       TRANSPORT TO
       LOWER TROPOSPHERE
        INJECTION OF
        CLEAN AIR

RAINOUT AND WASHOUT
OF GASES, PARTICLES
                         DILUTION OF   EFFECTS ON VEGETATION
                        RAIN ACIDITY      POLLUTION UPTAKE?
                     (RAINFALL AMOUNT)
    Figure 4.1  Principal effects of clouds on the atmospheric
    chemistry and physics of acid rain deposition.
                             260

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     (a)  rainfall production—Intensity and duration, a major determinant
          of rain pH and total [H"1"] burden

     (b)  effects on large-scale meteorology—through latent heat  release
          to the air and transport of momentum

     (c)  effects on photolysis rates and gas phase OH oxidation rate

     (d)  transport of sulfur and nitrogen species out of  the polluted
          boundary layer to:

            •  the lower free troposphere—away from surface deposition,
               allowing longer-distance transport and deposition

            •  the upper troposphere—likely into a global circulation,
               with deposition beyond North America

            •  the boundary layer once more—possibly chemically-modified

     (e)  chemical reactions  (oxidation) within clouds and rain

     (f)  removal—rainout and washout of gases and particles

     (g)  organization of small mesoscale convergent motions in the
          polluted boundary layer, thus bringing polluted  material to
          cloud base

The first two processes were  discussed in Section 2 of Chapter III,  and  are
clearly quite important factors in determining acid rain.  This section
assesses the transport processes, and suggests that each process should  be
treated simply but in a manner consistent with the others.   (Since the de-
tailed motions of cloud are extremely complex, semi-empirical descriptions
are frequently appropriate, and, consequently, overall consistency may need
to be sacrificed.)

4.2  Boundary-layer venting and clouds

     Perhaps the least well-simulated process occurring in the acid  rain
problem is the process of vertical transport between the boundary  layer  and
the rest of the atmosphere.   It appears that this process  may play a funda-
mental role in transporting acidic material long distances to remote but
environmentally sensitive areas, and perhaps also in transporting  the pol-
lution far away to the clean  atmosphere.  In this section, we will examine
the little available evidence that allows a preliminary evaluation of these
transport effects, and also some possible methods of simulating them.

a.   Observational evidence that cloud transport is important

     Observations show that a large fraction of the sulfur transported out
of the Midwest has passed through clouds.  Data from the four hundred air-
craft spirals made by Meteorology Research Institute and Research  Triangle
Institute during the SURE program give a good climatological view  of the
vertical distribution of S02, NOX, bscat (a measure of light scattering

                                     261

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by aerosols), and CN in the Midwest.  The latter two  serve,  in  combination,
as a reasonable indicator of the concentration of sulfate aerosol  and  its
age.  Figures 4.2 and 4.3 show vertical profiles of median values  of these
variables and an indication of typical high and low values.  Midday mixed-
layer (interpreted as subcloud-layer) heights ranged  from 1000  m to 1500 m
in the summer; these are climatologically typical values.  Substantial
vertical transport of material beyond these heights must be  accompanied  by
condensation over eastern North America.  Further west, deeper  mixing  can
occur without condensation, due to the typically lower  relative humidi-
ties.  However, these regions have much lower S02 emissions.

     Notice that the behavior of S02 and N02 is different from  that of the
particle measurements.  S02 and N02 drop strongly in  concentration above
the 1000 to 1500 meter level, while bscat and CN fall away at higher al-
titudes, around 2500 m.  Many low clouds have tops extending up to this
level.  A reasonable explanation of the different pollutant  distributions
is that sulfur has been carried through low clouds to produce the  aerosol.

     Do the clouds transform S02 to SOi^?  It is not  clear.  It could  be
that these cloud promote S02 reaction to sulfate strongly, or possibly that
S02 simply exhibits a shorter lifetime against transformation-removal, and
only its product remains in significant concentration above  cloud  base.

     Other data from the SURE airplane flights indicates that around 30%
of the sulfur column present at any time is above 1500  m, the height of  the
summertime mixed layer (see Figure 4.4).  The percentage varies from 15%
to 70% (Bornstein and Thompson, 1981), indicating that  a very substantial
amount of the sulfur loading present at any time over industrialized east-
ern North America has passed through cloud.  Since the  region above cloud
base is "better ventilated" with higher winds, an estimate of the  flux of
sulfur towards an acid deposition region above clouds is perhaps nearer
40-50% of the total.  Ferek's (1982) analysis of aerosols during wintertime
(APEX) conditions and in summmertime conditions suggests also a large
amount of sulfate above cloud base; Ferek suggests that his  data support
a large role for cloud-droplet oxidation processes, both in  storm  and  in
fair-weather low clouds.

b.   Previous simulations

     Several authors have made significant contributions to  the interaction
of cloud transport to air chemistry on the synoptic scale.   Ching  (1982)
has shown the potentially great sensitivity of the regional  oxidant buildup
process to cloud venting (net removal of ozone from the mixed layer).
Greenhut et al. (1982) have shown a case study of this  venting  process,  and
find a large effect in the neighborhood of the cloud  system  studied.   The
extension of this study to broader effects of cloud on  pollutants  is diffi-
cult.  Lamb (1982) has shown how to include the effects of low  clouds, es-
sentially those forced by boundary layer dry convection, into a mesoscale
air pollution model, using information derived from thermodynamic  proper-
ties like local surface heat flux.  Scott (1982) has  presented  two cloud
microphysical models, in which individual systems interact with an environ-
ment that is characterized by observed clirnatological pollutant concentra-
tions and meteorological variables.  He presents simulations of summertime

                                     262

-------
                 3000
             v

             U
             o
             D

                 zooo
                 1000
                             Night
                             and
                             Early
                             Morning
Midday
                         ZO
                               40
                                                   ZO
                                                         40
                               CONCENTRATION SO2 (ppb)
                  3000
                  ZOOO
               U
               Q
               H
                  1000
                               Night
                               and
                               Early
                               Morning
                           20    40            0     20

                                 CONCENTRATION NOX (ppb)
                                                          40
Figure 4.2   Concentrations of the primary  acid  rain pollutants, S02  and
nitrogen oxides,  [NO]  + [N02], (below) as a function of altitude during
189 aircraft spirals  above the Midwest made by MRI  during the SURE program.
(Figure from Blumenthal  et al., 1981).  There is a  drop-off in NOx and S02
above 800 m in  the  morning and '!200 m in the afternoon in most instances.
This level reflects the top of the region typically mixed by dry convection.
                                      263

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             3000
                              Night and
                              Early
                              Morning
                           CONDENSATION NUCLEI (103cm"3)
              3000  »"
              2000
          u
          Q
          H
              1000
                                   scat

Figure 4.3   Concentrations of condensation nuclei  (above)  and  bscat (below),
aerosol measurements which serve as a proxy for a continuous  measurement of
sulfate particles (see Blumenthal et al.,  1981),  Notice  that there are high
values of these extending up to 2000-2500  m suggesting  that transport from
below through the mechanism of low clouds  has distributed sulfate through a
deeper layer.  Condensation nuclei counts  provide a  measure of newly-formed
small aerosol; bscat is a measure of the light scattering properties of
submicron size-aerosol.
                                      264

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 S6 -
 22
 28
3 20

'9
                                            II
                                         Su  F  W Sp  So
       Su  F  w  Sp Su
       J— 1977— +— 1978 — j
                                                          F  w S»  Su
                                                            f—1978—j
                 SMU*
                           1978— (
     Figure 4
     sulfate
     in milli
     bar indi
     1500 m 1
     sampled
     base is
     to 1000
     day.
.4   Column-integrated concentrations  of total
over Philo, Ohio  (left) and  the  entire SURE region,
grams per square  meter.  The shaded  portion of the
cates the integrated amount  of sulfur  found above
n aircraft sampling.  The  remaining  portion was
below 1500 m.  Mean mid-afternoon  summertime cloud
around 1.5 km in  this region. Cloud  bases from 500
m are characteristic of other seasons  and times of
m
                                   265

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(convective) and wintertime (stable cyclonic) storms with  simple models  of
updraft and downdraft structure.  Scott's models include many processes,
but the implications and sensitivities remain to be more fully  understood.
Fisher (1982) has shown how some of the essential motions  of a  wintertime
warm-front warm-sector storm can be parameterized in a manner simple  enough
to allow detailed study of scavenging and chemistry.  Hong and  Carmichael
(1982) have begun work describing the interaction of a small cloud's  water
phase chemistry with a predefined advective transport through cloud.

     Gidel (1982) has considered the effects of cloud transport on meteor-
ological tracers with prescribed first-order decay rates,  and finds their
inclusion to be of very great importance in the tropospheric nitrogen  and
ozone budgets.  Chatfield (1982) has constructed a model of the tropo-
spheric transport and photochemistry of S02 and other reactive  reduced
sulfur species, and finds vertical distributions of S02 completely differ-
ent from those of diffusion models cited in his work.  He  also  includes  a
highly parameterized trajectory model for washout of S02,  and finds that
the treatment of the washout and reaction processes below  and just above
cloud base is crucial to the transport of S02 through cloud.

4.3  Vertical transport of pollutants—a mathematical framework

     Above the boundary layer, the most important vertical transport  mech-
anism is involved with the action of clouds, either on the synoptic scale
of cyclonic cloud systems or on the smaller mesoscales of  other clouds
(CIAP, 1975; Wallace and Hobbs, 1977).  Indeed, the boundary-layer top is
frequently taken to be at or near cloud base for the relatively humid situ-
ations characteristic of Europe and eastern North America.  Many cloud sys-
tems create temperature inversions at their bases.  Other  mixing processes
such as intermittent clear air turbulence {CIAP, 1975) do  occur.  The
thickness of such cloud-free mixing is limited, however; upward motion over
distances over 1 km is typically accompanied by condensation—cloud—for
relative humidities usually enountered over the region (Ludlam, 1980;
Wallace and Hobbs, 1977).

     The description of transports due to clouds usually involves time and
spatial scales that are smaller than usually handled by air pollution or
meteorological models.  For this reason, the mathematical  treatment needs
to smooth greatly the effects of cloud without, however, missing basic
transport processes.  The transport processes combine

     (a)  direct advective transport of the organized cloud updrafts  and
          downdraft—hundreds of meters wide and hundreds  to many thousands
          of meters deep, and

     (b)  turbulent motions, tending to produce more local mixing at  all
          scales down to the molecular scale.

These transport processes may have very different character.  Acid rain
simulations and most other air chemistry simulations to date have used eddy
diffusion parameterizations, which are demonstrably effective for the smal-
ler scales.


                                     266

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     It is not difficult to provide a mathematical  framework  for  these
transports.  For example, we can provide a  description  using  the  notation
of Eq. (2) in Section 6 of this chapter.  In  this  notation, the ensemble
and spatial mean transport of species due to  cloud and  associated small -
mesoscale motions is

                       9n,
                       -~  due to cloud transport =
                       0 t

               Ta (x,z) = / dx'Q/z toP{f(x,z|x',z') na(x',z')}


where the function f describes the probability  of  subgrid-scale transport
of the concentration of a species a, vertically  and horizontally  (per unit
time and unit volume).  Generally such  horizontal  transport will  be re-
stricted to neighboring grid elements since larger-scale  transport can  be
explicitly resolved, but the vertical transport  may span  the  depth of the
troposphere.  Such probabilities can be evaluated  in  several  ways:

     (a)  From diagnostic case studies  of cloud  motions in different
          synoptic situations.  While most  of these diagnostics describe
          tropical situations (e.g., references  in Houze  and  Betts (1981),
          Chatfield, (1982)), there are descriptions  of mid-latitude
          motions (Johnson, 1976; references  in  UCAR, 1983).

     (b)  From summary statistics derived from models of  individual  cloud
          or cloud systems (e.g, trajectory studies like  those of Miller
          and Betts (1976)).

     (c)  From convective parameter!zations that frequently form  part of
          a meteorological model.

Both diagnostics and parameter!zations, however, give information about on-
ly the averaged transports due to clouds.   Spatial  averaging  over (50 km)
is commonly used, and temporal averages of  1  to  12 hours  are  typically  im-
plicit.  Furthermore, parameterizations can describe  only the most likely
(i.e., ensemble-average) behavior.

     Other mathematical descriptions of cloud transport are possible.  This
one was based on the work of Chatfield  (1982).   Lamb's  (1982) analysis  of
low cloud is more detailed.

4.4  Four time scales associated with cloud

     For an assessment of the effect of cloud transports, both on subcloud
polluted layers and on the material source  for upper  layers,  a few time
scales are useful.

a.   Residence time below cloud base, TSut>  Cld

     One very basic time estimate can be defined for  removal  of pollutants
from the whole boundary layer:


                                     267

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           _ (typical boundary layer concentration)(subcloud layer depth)
   sub eld                         (cloud  base  flux)

We assume that this time scale is  approximately  constant  for all  levels
below cloud base.  This can be thought of as the  time  for  depleting the
mass in the boundary layer by exporting out  through  cloud  bases.   It is
thus a residence time (against this cloud-base transport)  for any  molecule
within the mixed layer.  It must be remembered,  however,  that other proces-
ses, such as reaction or absorption into  rainfall  or onto  the ground,  are
competing with this transport.  A  different  residence  time must be quoted
for each general  type of cloud, since clouds display widely different-
cloud-base vertical velocities and mass fluxes.   To  interpret this time
scale as a residence time, we must also assume that  the cloud field remains
almost unchanged in character for  times longer than  tsub  eld-  Tnis t1me
scale can be used in analyses of air pollution venting from the boundary
layer.  Such time scales could also be used  in parameterizations  in large-
scale acid rain models where explicit vertical transport  due to cloud  is
not included.

b.   Transport-to-cloud time scale, t-^rans

     A related time scale is harder to estimate.   Suppose  we wish  to con-
sider a molecule anywhere in a polluted boundary  layer, under either clear
or cloudy skies.   What is the average time until  the particle reaches  cloud
base?  This involves knowledge of  the transport  to that variety of cloud
field.  This is the definition of  T^rans, and  naturally only a very crude
estimate can be made without reference to complex models.

     This time scale is useful mainly in  general  analyses; the estimated
time scales shown in Table 4.1 suggest that  cloud removal  of sulfur is
important in the sulfur budget of  eastern North  America,  and approaches
the importance of dry deposition and wet  removal.

c.   Transport times through clouds, Tjnsoi  and  TSO]

     Two other time scales provide information about transport through
clouds.  It is frequently useful to have  a rough  estimate  of the expected
time a molecule spends within cloud, so as to  estimate the relevance of
possible aqueous or gaseous phase  reactions.   A  nearly insoluble gas will
have a transport time through cloud like  that  of  the air  between droplets,
and this time we call Tjnso-j.  Highly soluble  gases  (those that apportion
predominantly into the liquid phase) will frequently have  a rather differ-
ent lifetime, since most cloud droplets have an  appreciable fall  velocity
with respect to the moving air.  Time scales for  the residence of soluble
species in cloud must be calculated with  such  considerations taken into
account, using information from textbooks of cloud physics (Ludlam, 1980;
Pruppacher and Klett, 1978).

     Time scales like these are necessary for  estimating  the extent to
which "slow" reactions can proceed within cloud  droplets.   Estimates of
these time scales for a variety of cloud  types can be  found in Table 4.1.
These cloud types will be described in Section 6  of  this  chapter.   Many of
the estimates are based on a simple technique  that we  may  call the "kine-

                                     268

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                                  Table 4.1

                       Comparison of Cloud Time Scales
                              T           T           T           T
     Cloud type                insol       sol         sub cld     transport

 C
 0         .
 N  Cumulus1                   5-20 min   5-25 min    10-30 min     -14 hr
 E    (humulis mediocris)
 C
 T  Cumulonimbus2            15-40 min  15-60 min    15-30 min     -46 hr
 I
 V
 E

 S
 T  Stratocumulus             3-12 hr     3-9 hr       2-7 hr     >30-120 hr
 A    -stratus3
 3
 L  Nimbostratus"'5           5-48 hr     3-48 hr      1-3 hr      35-120 hr
 E
         LeMone (1976, 1980), Betts (1973), Houze and Betts (1981), Ludlam
(1980), and Stull  (1982) and references therein.

    2See Johnson (1976), Anthes et al . (1983), Ogura and Liu (1980), and
Herzech and Hobbs  (1981) and references therein.

    3See Hales et  al .  (1982), Ludlam (1980), and LeMone (1980) and
references therein.

    See Houze et  al .  (1981), Ludlam (1980), Hobbs (1978) and references
therein.
5
    5See also Telegadas and London (1954) for a general reference on cloud
amount.
                                      269

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matic method," which assumes that the subcloud layer  is  sufficiently  mixed
that all molecules have the same probability of incorporation  into  a  cloud
updraft.  For example, an estimate of rsub eld ^ given  by:

                 _          (height of cloud base)        	
        Tsub eld   (typical updraft(local fraction  of  cloud-base  '
                       velocity)        surface with  updrafts)

whereas a simple description appropriate when cloud updrafts are  widely
dispersed (e.g., cumulonimbus, cumulus, and some stratocumulus  clouds)
would be:

                          	Tsub eld	
     transport ~  (fraction of continental area with cloud and amount)  "

Some data is available from Telegadas and London (1954).  More  sophis-
ticated techniques are possible.  For example, Lamb (1982) estimates
Tsub eld f°r shallow cumulii using thermodynamic analyses.  Such  tech-
niques are likely superior for this type of cloud; other specialized
diagnostic techniques should be developed for other types.

4.5  Four representative cloud types

     Four types of clouds, illustrated and described  in  Figures 4.5
through 4.8, demonstrate the range of cloud effects.  These are:

  t  Cumulus clouds, typically the fair-weather cloud cumulus  humilis and
     cumulus mediocris, but including also scattered, relatively  active
     stratocumulus (see Figure 4.5). The main transport  effect  of these
     clouds appears to be to remove sulfur (S02 and sulfate) from the sub-
     cloud boundary layer, and thereby to reduce greatly the possibility
     of deposition onto the ground.  (Recall that dry deposition  is thought
     to be as important a sink of S02 as any.)  There is also  the possi-
     bility of reaction within water droplets, as described in  Chapter V.
     This is a predominant summertime cloud, and may  contribute greatly  to
     the sulfur loading above 1000 meters altitude.

  •  Deep convective storms like cumulus congestus and cumulonimbus (Fig-
     ure 4.6).  Such convection is important both in  air-mass  thunderstorms
     of summertime and in cold-frontal convection of  winter storms  (Herzegh
     and Hobbs, 1981, and references therein).  These may require the most
     sophisticated treatment, since they allow large  deposition of  sulfur
     as acid rain, and also removal of sulfur to the  upper troposphere,
     where it may be input to the global troposphere, and lost  from the
     continental sulfur supply.  This sink may or may not account for the
     apparent imbalance of sulfur sources and sinks,  with wet  deposition
     accounting for only  about one-fourth of industrial  sulfur  emissions
     (see, e.g., Golomb, 1982).  The sulfur that is transported rather than
     scavenged into rain  is likely distributed throughout the  troposphere,
     with greatest detrainment in the upper troposphere. In particular,
     one does not expect  the dropoff with altitude such  as found  in many
     eddy-diffusion calculations (e.g., Rodhe and Isaksen, 1980;  Graven-

                                     270

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Figure 4.5   Cumulus mediocris circulation patterns  shown  for a
marine environment (Lemone, 1976). Note several  important  features
of these clouds that should be incorporated into an  acid  rain model :
(a)  Transport of material  at cloud base is downward between  clouds
and upward transport is almost exclusively through clouds,  implying
different effective transport for species with little reaction in
water phase (i.e., ozone, sulfate) and those with potentially great
reaction (i.e., SO?, HOOH).
(b)  Material  above cloud base is removed from frequent contact
with the surface, greatly reducing dry deposition for materials  like
sulfate aerosol.
(c)  A substantial portion  of the material passing through  these
clouds originates from near the surface, at least during  the  early
part of of the life cycle of each cloud.
                                 271

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Figure 4.6   A particularly active cumulonimbus  cloud  (Ludlam,  1980).
Clouds of this variety cause great deposition  of [H*]  ion  in  a  few
events over summertime in Eastern North America  (Niemann,  1982),  but
may also allow substantial  removal of sulfur from the  region, as  sub-
stantial amounts of water are detrained above  five kilometers,  so that
very-long distance transport is more likely than reentrainment  into a
precipitating system.  The cloud portrayed is  a  severe storm, much more
active than climatologically more typical  cumulonimbus clouds,  but a
variety which has been better characterized due  to its
effects.  Most cumulonimbi
times in their life cycle;
                            destructive
show the features portrayed at various
usually, only the severe storms maintain
Other features important in the simulation
a quasi-steady structure.
of acid rain are:
(a)  Boundary layer air is spread through rather broad  regions  in
the upper troposphere, so  that mean concentrations  of S02  of 0.3 to
0.5 ppb may represent a substantial  removal  flux from the  1  km  boundary
layer.
(b)  Air ventilating the boundary layer in the downdraft may be a
combination of relatively  clean air from above three kilometers and
somewhat polluted air from one to three kilometers  from one  to  three
kilometers.  For an examp-le of such ventilation, see the unusually
low CFC13 concentrations observed on August 1  in sampling  shown in
Figure  6.6 of Chapter VI.
                                    272

-------
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                       273

-------
            «'CM UOUIQ KKftTES CONTENT
            MICH ICE PARTICLE CONCENTRATIONS   ^
Figure 4.8   Nlmbostratus and altostratus characteristic of
cyclonic warm fronts.  These are most frequent in wintertime
and their large horizontal extent and uniformity allows material
transport to be relatively well described.  Note also that
(a) much of the upward motion in these storms occurs in limited
regions with vertical velocities of 10 to 50 cm/sec, so that
material may be lifted from near the surface to two to five
kilometers over times as short as three to ten hours, and
(b) small-scale transport of reacting chemical species: soluble
species like HOOH, may cross the frontal surface under common
conditions, borne within cloud and rain droplets.  Hydrogen
peroxide may be transported within tne warm sector, originating
in sunlit, moist, maritime, tropical air.  Sulfur dioxide may
accumulate to the more northern, stable air ahead of the warm
front in these circumstances.  In summary, even large-scale
cloud systems may exhibit transport effects taking place on the
scale of kilometers.
                              274

-------
     horst et al., 1978).  Figure 4.2 suggests that such concentrations
     are less than about 1 or 2 parts per billion above 3 km.  Data  taken
     over relatively unpolluted regions of western North America  suggest
     that these concentrations are around 0.2 to 0.3 ppb even at  5 km
     altitude (Maroulis et al., 1980).  Much lower concentrations, one
     third as high, are found over ocean regions,  Chatfield (1980)  has
     suggested that such low but non-negligible concentrations may ori-
     ginate from ground-level sources in midlatitudes and tropics, with
     reduced sulfur redistributed in deep convective updrafts.

  •  Stratus and stratocumulus characteristic of cyclonic warm fronts .and
     orographic clouds.  These form large-scale cloud systems and so might
     seem to present the fewest subgrid-scale problems.  Perhaps  the best
     estimate of transport 1S the synoptic time scale of five days  (win-
     ter) to perhaps twice that (summer).  However, in most synoptic situ-
     ations with flow across the Appalachians, orographic stratiform cloud
     is quite likely to affect the sulfur transport and chemistry, giving
     Ttransport mucn smaller than that shown in Table 4.1.

  •  Nimbostratus of warm-frontal systems.  Again, these form broad-scale
     cloud systems, but, as Figure 4.8 shows, there may be significant
     small-scale effects, including vertical motions on the order 20 cm/
     sec, so that there may be fairly rapid transport to the low  and middle
     troposphere on a sporadic basis.  These systems may also contribute to
     removal of sulfur from the continental sulfur budget and into the  hem-
     ispheric budget, as previously described.  Although the large-scale
     features of these cloud systems are well simulated by regional  models,
     a significant amount of vertical transport, precipitation, and  .chemi-
     cal interchange between air masses may occur in small (30-km wide)
     bands (Houze et al., 1981, and references therein).

4.6  Cloud transport as described by large-scale meteorological models

     We have seen that cloud transports of material can both

       •  help preserve sulfur species from ground-level uptake by carry-
          ing a third to a half of sulfur out of the boundary layer  and
          towards regions of rainout, and

       •  help remove sulfur and nitrogen from the subcontinental lower
          tropospheric reservoir that produces acid rain, perhaps account-
          ing for a portion of the "missing sulfur" that is emitted  but not
          deposited.

Let us describe the present state of meteorological parameterizations  in
terms of the general cloud types given above:

  •  Low clouds, such as fair-weather cumulus and stratocumulus,  are es-
     sentially not diagnosed in weather forecast models (see following
     section on cloud modeling and Chapter IV, Section 6), but have  been
     considered in more specialized diagnostics like those of Miller and
     Betts (1975) and Stull (1983).  Stull (1983) has given a review.


                                     275

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  •  Cumulonimbus and related types make sufficient impact on the  energy
     and momentum fields that their effects are usually diagnosed  {see
     following section and Chapter IV, Section 6).  Only a few  parame-
     terizations, such as that of Arakawa and Schubert (1974) and  its
     successors, can be interpreted explicitly as describing from  which
     level sulfur molecules are removed and to which levels they are trans-
     ported.  However, such models may or may not give a good description
     of the effects on energy, moisture, and momentum fields within a me-
     teorological model (see comparison studies listed in Chapter  IV,
     Section 6).  Many parameterizations are based on considering  a single
     cloud which detrains material only in the top ten percent  of  the-cal-
     culated cloud depth, and so simulate very high removal of  sulfur com-
     pounds from the lower atmosphere.

  t  Large cloud systems, including warm-frontal and orographic nimbo-
     stratus and stratocumulus, are not so complex.  However, it may be
     necessary to account for their own slow convective circulations,
     as shown in Figure 4.8.  The larger vertical velocities here
     (- 30 cm/s) may allow escape of material to the upper troposphere,
     while the enhanced rainfall may allow introduction of soluble species
     like HOOH with a warm-sector origin.

     Some concluding remarks provide an overview of the roles of clouds:

       (a)  Clouds have several different important effects in  acid rain
            models, especially in removing sulfur from the mixed layer.

       (b)  Descriptions of vertical transport superior to eddy diffusion
            parameterizations are emerging, but they require a  climato-
            logical data base.

       (c)  Parameterizations of the effects of clouds on horizontal winds,
            vertical transport, and photolytic radiation are separate,  and
            closely consistent, descriptions.

4.7  Cloud Modeling

     The preceding sections have indicated the complexity of cloud proces-
ses and the variety of parameterization procedures, some rather ad hoc,
that have been employed.  More concrete descriptions of these processes  are
contained in cloud-scale models, and this section will describe what we  can
learn from them for acid deposition modeling.

     The nonhydrostatic meso-y scale model (i.e., the cloud-scale  model)
can be extremely useful in the following two major aspects of developing  a
regional-scale Eulerian acid deposition model:

     (1)  understanding the relationship between cloud/precipitation
          processes and chemical/physical processes of pollutants, and
          developing and testing parameterization schemes of cloud chem-
          istry for regional-scale models; and

     (2)  revealing mutual interactions between regional-scale  phenomena

                                     276

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          (which have the potential to carry pollutants  over  a  long
          distance) and associated clouds, i.e., the  interactions  between
          the regional scale (hydrostatic) and  the  cloud scale  (nonhydro-
          static), and parameterizing and testing the  collective  effects
          of clouds for regional-scale models.

     Clouds are the obvious agency for producing wet  acid deposition,  after
chemical species are mixed with water in the clouds.   The relationships be-
tween cloud/precipitation processes and the chemical/physical processes of
pollutants are not clear.  The state of the art at  present allows  detailed
numerical simulations of clouds.  With such a model,  chemical/physical  pro-
cesses of pollutants may be included at least in a  parameterized  fashion.
Thus, investigation of the evolution of pollutants  in  the cloud and  the
surrounding environment becomes possible.  Since the  actual effect of
cloud/precipitation processes on chemical/physical  processes  of pollutants
(or vice versa) occurs via cloud microphysics,  a cloud model  must treat
microphysics in as much detail as possible in order to study  cloud chem-
istry.  The microphysical processes may include nucleation, condensation,
evaporation, deposition, sublimation, stochastic collection and breakup,
and sedimentation, and they may be complicated  further by cloud electri-
fication and radiation processes.

     On the regional scale, cloud and precipitation processes can affect
the transport and deposition of pollutants.  A  more accurate  representation
of the collective effect of cloud and precipitation processes in  a region-
al-scale model is undoubtedly needed.  Obviously, comparing observed data
with the results from a regional-scale model which  includes parameterized
cloud and precipitation processes can show the  merit  of  the parameteriza-
tion schemes.  However, if we can learn more about  the mutual interactions
between the regional and cloud scales, new parameterization schemes  may
provide more accurate prediction of cloud precipitation.  To  gain some
basic knowledge of (1) how convective clouds and precipitation  will  be
initiated and maintained under different regional-scale  settings,  and  (2)
how the convective clouds and precipitation will feed  back on the regional
scale, the ideal method is to develop a time-dependent,  three-dimensional
system with a cloud-scale model nested within a regional-scale  model with
two-way interactions between the scales.  A cloud-scale  model with complete
dynamics (i.e., nonhydrostatic, three-dimensional,  time-dependent) is  re-
quired for this nested system.

     Various cloud-scale models, either steady-state  or  time-dependent and
in one, two, or three space dimensions, are being used in a number of  as-
pects of cloud microphysics/dynamics research.  The complexity  of micro-
physics or dynamics depends on the nature of the research topic and  indi-
vidual interest.  For studies of cloud microphysics with a relaxed dyna-
mical structure, the cloud model can perform detailed  calculations of  the
evolution of particle spectra, including perhaps radiation and  electrical
effects on the spectra.  On the other hand, for cloud  dynamics  research, a
three-dimensional and time-dependent model is necessary  to reveal  the  de-
tailed circulation of the cloud and its environment,  and only a highly
parameterized procedure for the micro-physical  processes may  be afford-
able with present computer resources.


                                     277

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     Excellent reviews of cloud microphysical and dynamical processes  have
been made by Cotton (1975a, 1979) and Schlesinger (1982); the complexities
of cloud microphysics and dynamics have been well described.  The  emphasis
of this section is on the parameterization of microphysical processes  for a
three-dimensional  cloud-scale model, and on the parameterization of  convec-
tive clouds and precipitation for a three-dimensional regional-scale model.

     To consider a complete set of microphysical processes, the range  of
particles may span from 10~2 urn in radius for aerosol particles to 105 pro
for hail.  The conventional method for calculating the evolution of  a  par-
ticle spectrum is to increment the particle radius logarithmically.  In
order to represent such a broad range of particle sizes precisely, a large
number of increments is needed, giving a large number of field equations
for the size classes.  As shown by Silverman and Glass (1973), 45  mass
classes for hydrometeors ranging from 2 to 4040 pm in radius may be  neces-
sary for satisfactory spectral  resolution just for the warm-rain cloud.
(The microphysical processes involved are only condensation/evaporation,
stochastic coalescence, and breakup.)  Gillespie (1975) has suggested  a
Monte Carlo computational algorithm for simulating the evolution of  the
spectrum by stochastic coalescence.  Although the statistical algorithm is
generally satisfactory, it is quite demanding computationally.  To minimize
the artificial spreading of particle distribution, Ochs and Yao (1978)  and
Ochs (1978) have developed a moment-conserving technique to calculate  par-
ticle-spectrum evolution.  As Ochs (1978) indicates, the increase  in accu-
racy obtained with this technique comes with considerable computational
cost.  A distribution function approach put forth by Clark (1974,  1976) and
Clark and Hall (1982) to simulate the evolution of the particle spectrum
has shown a very accurate and computationally efficient solution,  compared
with the solution of the standard finite-difference approach.  There is a
very high potential for applying this new approach to multidimensional
cloud models.

     One-dimensional time-dependent cloud models cannot provide the  com-
plete cloud circulation, but are efficient and effective tools for develop-
ing and testing complex microphysical processes.  The dynamical framework
formulated by Asai and Kasahara (1967) embraced significant cloud  dynamics;
they averaged the fundamental equations about the central axis over  a  fixed
radius by assuming axial symmetry in a cylindrical coordinate, taking  into
consideration both updraft and downdraft areas.  Later this system was sup-
plemented by Holton (1973) to include dynamic pressure calculations, and by
Cotton (1975) to upgrade the formulations of turbulent transport.  The de-
tailed interactions of cloud microphysical and chemical processes  may  be
simulated by using such dynamically simple models.

     Schlesinger (1982) gave an excellent review of the three-dimensional
numerical modeling of convective storms.  First, he established arguments
for the third dimension in cloud models, and showed how complicated  a  cloud
model could be.  Explicit calculations of the evolution of the particle
spectrum by the conventional finite-difference method become  impossible
with present computer resources.  Based in part on a Marshall-Palmer dis-
tribution, the Kessler  (1969) parameterization, with some variations,  has
been adapted most widely for the microphysical processes in three-dimen-
sional cloud models.  Such parameterizations usually divide liquid parti-

                                     278

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cles into two categories:  cloud droplets, which  do  not  have  falling  velo-
cities, and raindrops, which do.  A similar approach  could  be applied to
the ice particles (Koenig and Murray, 1976; Koenig,  1977).  Schlesinger
(1982) then identified some difficulties in the three-dimensional  modeling
study; namely, model initializations, boundary conditions,  numerical  meth-
ods, and verifications.

     Past models have been quite complex, and often  are  the focus  of  large,
autonomous research efforts.  However,  the preceding review suggests  that
enough has been learned to merit the adaptation of cloud models  to simulate
several processes required by acid deposition research.

     A list of cloud models, including  distinguishing characteristics,  can
be found in Table 4.2.  The development of a three-dimensional model  is it-
self a challenging and time-consuming effort.  The most  reasonable approach
appears to be a nested-grid technique allowing a  large regional  model  to
supply boundary conditions for  individual cloud simulations.   Such a  de-
tailed nested-grid model would  be ideal for the comparison  of model  results
with specific air-chemistry observations.  However,  for  studying cloud
chemistry and the interactions  between  cloud and  regional scales,  one can
use an existing cloud model rather than developing a new one. Accurate
representation of chemical/physical processes of  pollutants in clouds and
the cloud/precipitation processes is the primary  emphasis in  regional-scale
acid deposition applications.

     The treatment of cloud microphysics in a cloud  model is  extremely
important, and one of the best  in this  regard is  the three-dimensional  non-
hydrostatic model developed by  Clark (1977).  This model  uses terrain-fol-
lowing coordinates and excellent cloud  microphysical  parameterizations
(Clark, 1979; Clark and Hall, 1979).

     In summary, the utility of nonhydrostatic cloud-scale  models  for re-
gional acid deposition studies  has been stressed.  To investigate  and par-
ameterize the microphysical processes of clouds,  the chemical processes of
pollutants, and their interactions, a simplified  cloud model  can be very
useful.  The dynamical framework of Asai and Kasahara (1967)  with  supple-
mentations is recommended.  Furthermore, to reveal the mutual interactions
between cloud and regional scales and to parameterize the collective  ef-
fects of convective clouds on the regional scale, a  complete  cloud model
with sound microphysics is required.  For this purpose,  the three-dimen-
sional cloud model of Clark (1979) is appropriate.


5.  DRY DEPOSITION

5.1  Introduction

     The role of dry deposition in the  regional acid deposition  problem is
important.  However, the fact that this deposition of atmospheric  acidity
is commonly referred to as "acid rain"  indicates  that dry deposition  has  in
the past been overlooked or considered  as playing only a minor role.   Per-
haps this is because precipitation would seem to  be  the  most  obvious  source
of acid deposition.  Another reason is  the difficulty in actually  measuring

                                     279

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                                 Table 4.2

          Three-Dimensional  Time-Dependent Numerical  Cloud Models
    Model

Blechman (1981)


Clark (1979)



Clark and Hall  (1979)



Cotton and Tripoli
Klemp and Wilhelmson
(1978a, b)
Lipps (1977)


Miller (1978)

Miller and Pearce
Moncrieff and Miller
(1976)

Pastushkov (1975)
Schlesinger (1975)
Schlesinger (1978,
1980)

Simpson and van Helvoirt
(1980)

Simpson, van Helvoirt,
and McCumber (1982)
      Distinguishing Characteristics

Applied model of Schlesinger (1978); nested
grid (two-way)

Terrain-foil owing coordinate; anelastic;
Coriolis parameter included; precipitation
parameterization of Kessler (1969)

Applied model of Clark (1979);  shallow; log-
normal  distribution function parameterization
for cloud microphysics

Height coordinate; elastic; Coriolis parameter
included; moist but no precipitation

Height coordinate; elastic; Coriolis parameter
included; precipitation parameterization of
Kessler (1969)

Height coordinate; incompressible; shallow;
moist but no precipitation

Applied model of Miller and Pearce (1974)

Pressure coordinate; anelastic; Coriolis
parameter included; precipitation parameter-
ization of Kessler (1969)

Applied model of Miller and Pearce (1974)
Height coordinate; anelastic; precipitation
parameterization of Takeda (1966)

Height coordinate; anelastic; moist but no
precipitation; no turbulence

Applied model of Schlesinger (1975); preci-
pitation parameterization of Takeda (1966)

Applied model of Schlesinger (1978)
Applied model of Schlesinger (1978)
                                     280

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                                 Table 4.2
          Three-Dimensional Time-Dependent Numerical Cloud Models
                                (continued)
    Model

Sommeria (1976)


Steiner (1973)
Tag and Rosmond
(1980)

Thorpe and Miller
(1978)

Tripoli and Cotton
(1980)
Turpeinen and Yau
(1981)

Wilhelmson (1974)
Wilhelmson and Klemp
(1978, 1981)

Yau (1980)
Yau and Michand
(1982)
      Pistinguishing Character!'stics

Height coordinate; anelastic; shallow; Coriolis
parameter included; moist but no precipitation

Height coordinate; incompressible; shallow;
moist but no precipitation

Height coordinate; anelastic; moist but no
precipitation; no turbulence

Applied model of Miller (1978)
Applied model of Cotton and Tripoli (1978);
no Coriolis parameter; precipitation para-
meterization of Kessler (1969)

Applied model of Yau  (1980)
Height coordinate; anelastic; precipitation
parameterization of Kessler (1969)

Applied model of Klemp and Wilhelmson (1978a)
Applied model of Steiner (1973); anelastic;
precipitation parameterization of Kessler (1969)

Applied model of Yau (1980)
                                     281

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and defining the dry deposition contribution  {Hicks  et  al.,  1980).

     Indications now are that  nonprecipitation-related  deposition of acidic
or potentially-acidic species  is approximately  equivalent  to that directly
related to rain and snowfall (Record  et  al.,  1980).

     Dry deposition refers  to  the  direct transfer  of material  from  the free
atmosphere to the vegetation,  soil, or water  surface where it is  taken up.
In the Eastern United States and Canada,  most of the surfaces exposed to
the atmosphere are not bare soils, rock,  or concrete, but  are the leaves of
growing plants.  In general, dry deposition may be conveniently  separated
into two reasonably distinct aspects.

     The first part involves the transport through the  surface layer to a
laminar surface sublayer.  This is due to the turbulent processes in the
atmosphere and is the aerodynamic  component of  the transport.  It governs
the rate at which atmospheric  species are carried  into  the immediate vicin-
ity of the surface.

     The second part involves  the  transport by  diffusion through  the lami-
nar surface sublayer to the ultimate  absorbing/reacting substrate,  and is
the surface component of the transport.   Although  the laminar surface sub-
layer is typically only - 100  ym in thickness,  the processes operative
within this layer are critically important in establishing the deposition.
The reactivity/solubility/adhesion of atmospheric  species  at the  surface
governs the ultimate rate at which atmospheric  species  are removed, as
nonreactive species such as Ar and He have deposition velocities  of zero.

     Although the mechanism of transport is complex, involving different
scales of turbulence, the overall  result can  be described  simply.  At any
height, the concentration of a species,  C, and  the dry  deposition flux, F
(C-velocity), define a deposition  velocity:

                                Vd -  F/C

     A useful model which has  been developed  to handle  the mathematical
treatment of deposition is  based on the  analogy to electrical flow  through
resistances.  In this convention,  the overall deposition velocity (or con-
ductance) of any atmospheric species  is  defined as the  sum of the various
resistances to the uptake by the surface.

     In a complicated system such  as  a forest,  the resistances to deposi-
tion are complex.  The ultimate uptake/reaction can  take place at the soil,
at the leaf cuticle, at the plant  tissue in the interior of the  leaf via
the stomata, or at the leaf hairs.  Turbulent transport must be  considered
to canopy top leaves, to the understory,  and  to the  soil.   In order to de-
fine the total conductance  of  a trace constituent, all  these resistances
must be considered.

     The analysis of such a resistance network  where seme  are in  series and
some in parallel yields a single equivalent  resistance. However, for dry
deposition, it is most profitable  to  separate the  total resistance  into
an aerodynamic (turbulent flow) resistance,  ra, and  a surface (diffusion

                                      282

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flow) resistance, rs.  Then, the total conductance  (or  deposition  velo-
city) may be expressed as
     The aerodynamic resistance,  ra,  is  an  expression  of  the  turbulent
transport from the free atmosphere to  the surface  laminar sublayer.   The
value of ra is dependent upon atmospheric stability  and upon  surface
roughness.  Micrometeorological research has  as  its  concern the  prediction
and definition of this resistance term for  the boundary layer transport of
heat and momentum.  The additional input required  for  the calculation of
ra within an advanced acid deposition  model  is a parameterized grid  of
surface cover/land use.  Such information is  available and must  also be
utilized in defining rs.

     The surface resistance component, rs,  is more difficult  to  treat.
Because of the difficulties involved  in measuring  chemical deposition
rates, there is not a lot of data available,  much  of what is  available is
unreliable, and even the reliable data is mostly for ideal conditions of
surface cover and weather.

     Various experimental techniques  are used to measure  deposition  velo-
city.  These include:

     (1)  Box methods

     (2)  Profile or gradient analysis

     (3)  Eddy correlation measurements

A fourth method, budget analysis, can  also  be applied  to  either  or both wet
and dry removal.

     The box method basically consists of placing  an enclosure over  a
surface to be tested and measuring the rate of decay of the concentration
within the enclosure, which is presumed  to  be related  to  removal  at  the
surface.  Although the method is  simple  in  concept and requires  only the
measurement of the mean concentration  as a  function  of time,  there are many
assumptions involved in its application.  First, it  is assumed that  the
enclosure does not affect the removal  rate  and that  the results  can  be cor-
rected for the effects of the enclosure.  These  effects include  adsorption
on the enclosure walls, lack of natural  ventilation, and  changes  in  the
solar and infrared radiation balance  which  also  affect the heat  and  water
vapor budgets within the enclosure.   Over water, an  enclosure will  also
modify the waves.  Over forests,  an enclosure covering a  significant area
would be unwieldy, and enclosures covering  a  branch  may not be representa-
tive.  For these reasons, box or  enclosure  methods will probably  never be
entirely satisfactory.

     Measurement of the mean concentration  profile has the advantage of a
minimal disturbance of the surface and the  overlying atmosphere.   However,

                                      283

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accurate concentration differences must be measured  (on  the  order  of  1%  of
the mean concentration or better).  Furthermore, the stability  of  the  lower
atmosphere and a flux-profile relationship must be known.  These require
additional micrometeorological measurements.

     The eddy correlation technique is a direct measurement  of  the turbu-
lent flux at a particular level.  Within the surface layer,  which  is  typi-
cally of order 10 m deep, the flux of species with lifetimes  greater  than a
few minutes is sensibly constant.  Therefore, the downward flux within the
surface layer is a measure of removal at the surface.  The vertical flux of
a species is obtained by averaging the instantaneous product  of the species
and the vertical velocity after removing the mean from each  of  them.   The
average must be taken over a time long enough so that fluctuations in  the
average are not significant.  The sensor time response must  be  short  enough
to resolve all the significant contributions to the  turbulent flux.   For a
fixed site within the surface layer, this requires an instrument of at
least 1 Hz bandwidth; for an aircraft, several Hz bandwidth  are required.
Although accurate absolute measurements are not necessary, small-scale
fluctuations need to be resolved.

     With current technique improvement, it is likely that within  the  next
years much better and more comprehensive estimates of surface resistance,
rs, will become available for different surfaces under different condi-
tions.

     A regional acid deposition model should have ra and rs  for each
grid square.  There is a conceptual problem of establishing  mean values
of ra and rs for 50 km x 50 km grid squares.  For areas  of monoculture
such as the western wheat lands and the midwestern corn  lands,  this  is pos-
sible, but for eastern mixed land use, it is doubtful.   A redeeming factor
is that in the daytime a deposition regime may be established within  dis-
tances comparable to the height of the boundary layer.   Thus, even for grid
squares with inhomogeneous surface cover, an average of  the  different depo-
sition regimes is valid if the individual elements of surface cover have
linear dimensions of several kilometers.  The greatest difficulty  is  in-
volved where the scale of the mix of land use is less than one  kilometer.

5.2  Available model input

a.  Aerodynamic resistance

     The aerodynamic resistance,  ra, is a function of wind velocity,  at-
mospheric stability, and surface  roughness.  These are variable, although
surface roughness normally is associated with vegetative cover  and only
seasonal variations need normally be considered.  Figure 5.1 indicates the
range of Vj max = l/ra for different natural surfaces normalized for  a
constant friction velocity.  Water surfaces represent an interesting  var-
iation as increased wind speed is marked by increased wave activity and
changed surface roughness.

b. Surface resistance

     Deposition velocity measurements for a number of species have been

                                     284

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   1000  =•
                                                    - 1000
100 =•
 £
 a

X
r-
UJ
                                     Displacement
                                     Height
            (required to generate v
             this
                   Friction
                   Velocity
                                   Max Deposition
                                       Velocity  = -
                            Roughness
                            Length
                    -J .£  •* .£ •*  CD Q. _
                    — -c---c---'Oo<2
                               i±| QJ J  X
           Figure 5.1   Maximum deposition  velocity for
           different surfaces normalized  to a constant
           friction velocity.
                                  285

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carried out over the past decade or so.  Several  recent  critical  reviews of
this data have attempted to establish reliability  and  to  link  the observa-
tions to a theoretical basis (Hosker and Lindberg,  1982;  McMahon  and Deni-
son, 1979).

     For trace gases, the surface resistance  is correlated  with  their solu-
bility/reactivity.  Figure 5.2 represents an  attempt to  correlate the solu-
bility/reactivity of different trace gases with their  experimentally-deter-
mined deposition velocities.  By arranging the chemical  species  in this
manner, a generally well-ordered relationship can  be obtained.  However,
such arguments can only be used in a general  fashion,  as  certain  specific
effects may sometimes dominate.  For example, the  specific  takeup mechan-
isms for 03 and for S02 are different.  Ozone is  an oxidant which reacts
with vegetative tissue primarily via the stomatal  openings;  thus, rs(03)
variation is dependent not only upon vegetation type but  also  upon plant
maturity, photosynthetic activity, moisture stress, and  insolation.   Sulfur
dioxide, on the other hand, is an acid anhydride  which is taken  up by moist
surfaces.  As the pH decreases, a point is reached when  no  more S02  will be
dissolved.  Thus, the variation of rs(S02) is dependent  upon a  different
set of factors.

     For particles, the situation is much more complex.   Different physical
processes, including gravitational settling,  inertial  impaction,  diffusion
and thermophoresis, molecular diffusion, surface  adhesion,  and  other fac-
tors, dominate in different particle size regions, and so the  surface re-
sistance of an aerosol is a strong function of its  size  distribution even
for ideal particles and uptake surfaces.  For real aerosols and  surfaces,
many more factors come into play.  Figure 5.3 indicates  some of  the  phys-
ical processes involved in defining the deposition  velocities  to  smooth
surfaces and compares an assemblage of laboratory  and  field measurements
taken from a review of experimental data.

     Although surface resistances for different gases  and aerosols are very
difficult to assign precisely, enough is now  known  to  allow reasonable val-
ues to be set for modeling purposes.  As better,  more  comprehensive  mea-
surements are made, the newer values of rs may be  incorporated.

5.3  Suitable models

     The model of Sheih et al. (1979) may be  taken  as  representative of  the
style of dry deposition treatment which may be used to generate  a submodel
for a regional acid deposition model.  Although Sheih  et  al. dealt only
with S02 and so£~, other gases and aerosols may be  treated  similarly.

     In this model, surface cover categories  were  defined for  a  0.5° grid,
using data from USDA land use maps.  The surface  cover field shown in Fig-
ure 5.4 was then used, together with the model-generated  stability class
field, to produce values of ra for each grid  square.   Thus, for  the  cal-
culation of deposition velocities, the surface cover map  is used  both to
define ra by means of surface roughness and to define  rs.
                                     286

-------
          10
   vd
cm sec"
        0.01
-
^
~x
-X

X

-
^
_

—
-
—
—
— „

—


II!!!
x H
x H
x J^ H
X sK y H
x *i H G
| |- ' 'Mr»_ ' rt 1 Mrt 1 DAM' u e'lu o' r>/->
                                     OSNOPAN
                            HNO,
DMS
             Figure 5.2   An assemblage of the available deposition
             velocity data for trace  gases ranked approximately in
             terms of reactivity.
                                   287

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     I02


     10'


     10°
 o
 at  'O
 e
 o
~  io-2
    io-3

    !0-4

    io-5
     I       I       i       I
"DRY DEPOSITION TO SMOOTH SURFACE
 (derived from Slinn,l976)
                   psIatmos

    72.6cms"1, evap/cond = lcm/hr"
                 D(c)
                                      NET Vd
                              (for no evap./cond.)
                G.S./
EXPERIMENTAL DATA FOR VARIOUS  SURFACES
C3 Laboratory
o F' Id
                   McMahon ft Denison (1979)
                  J_
      "3
             IO"    IO"2   IO"1    10°    10'    IO2

                   PARTICLE RADIUS  (/j.m)


Figure 5.3    Experimental data plotted over a format showing the
physical  processes  involved in the dry deposition of particles
(G.S.  = gravitational settling;  II = inertia! impaction;
M.D.  = molecular diffusion; D(e)  = diffusiophoresis, 1  cmhr"^
evaporation;  D(c) = diffusiophoresis, 1 crnhr-1 condensation.)
                              288

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           0 Cropland and Potturt
           1  Crop*ondt Woodland end Grazing Land
           2 Irrigattd Crop
           3 Grazed Fortst and Woodland
           4 Ungraztd Fomt and Woodland
           5 SubJiurmd Grassland and Stmiarid
             Grazing Land
6 Op«n Woodland Grawd
7 Dtstrl Shrubland
A Swomp
B Mainland
C Metropolitan City
F Lake or Octan
                               SURFACE COVER
                               VEGETATION TYPE
Figure  5.4    Example  of a  land  use  map  (from Sheih et al.,
1979) and the conceptual  relationship leading to  the  definition
of  a deposition  velocity  field.
                                  289

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5.4  Phases of complexity

     (1)  Use available surface cover/land  use  maps  to  define a deposition
          velocity field for each species of  interest.

     (2)  Use available surface cover/land  use  maps  to  allow  the model  to
        .  define its own micrometeorology and to  generate  ra  fields which
          change with time.  Define  rs  for  each grid and allow a deposi-
          tion velocity field to be  generated internally.

     (3)  Use (2) for ra, but by parameterizing the  effect of seasonal,
          and diurnal cycles, available moisture,  insolation,  and other
          factors on rs, establish a realistic  variation of rs,  and
          again internally generate  a deposition  velocity  field for each
          species of interest.

     (4)  Improve surface cover/land use maps (treat subgrid  scales) and
          improve the parameterization  of ra  and  rs.


6.  MODEL RESOLUTION

6.1  Introduction

a.  The disparity of spatial scales

     To understand quantitatively the production  of  acid rain, we must
consider processes occurring at very  different  time  and space scales.   The
deposition of sulfate and nitrate takes place primarily over  the eastern
third of the North American subcontinent, controlled by the synoptic mete-
orology of a one-to-two-thousand-kilometer-wide region. Let  us call this
large area the deposition region.  However, the acid material  is derived
from the oxidation of SO 2 and NOX, which are  emitted largely  from concen-
trated sources that form plumes hundreds of kilometers  long but only 1-30
km wide (see Figure 6.1).  Within these plumes, there is frequently a  pat-
tern of suppressed and then enhanced photochemical activity which modulates
the transformation of the emissions  to  the  oxidized,  acidic forms.  How-
ever, a competitive process, uptake  by  the  ground, is also rapid, and this
makes the details and timing of conversion  important.   We  may call this the
primary reaction region, bearing in  mind that continued reaction occurs to
the diluted and partially reacted material  in the  broader  regions between
plumes.  An estimate of the ratio of the areas  of  these regions is

                 Area of Deposition  Region    _  >(inn\2 = in4
              Area of Primary Reaction  Region

based on data presented in this chapter.  This  ratio partially explains why
there have net been large-scale acid rain models  that include a description
of chemistry on other than an extremely empirical  basis.   At  least one grid
point needs to be devoted-to each primary reaction region, and the result-
ing requirement of 1Q1* grid points per  horizontal  plane begins to strain
the resources of the largest computers  used to  date  if  many field variables
are carried.

                                      290

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              100 km-
                           100 km  True Reaction « 0
                                      Computer Simulation
                                      of Reaction
                                          OH, 0,
                                                 True Reaction ^
                                                 Simulated Reaction
Figure 6.1    Resolution  cf reaction between chemical species.  Power
plant plumes  are strong  sources of S02 and city plumes frequently
contain particularly  high concentrations of oxidants such as QS and
HO.   The middle sketch shows  how a regional model with a large grid
spacing must  simulate these plumes -- just as if they were completely
dispersed in   a grid  volume.   Clearly, if the true geometry of the
plumes is like the top sketch, the regional simulation will give a
great over-estimate of the reaction rate.  We will see that if the
source geometry is more  like  the bottom sketch, the computer simu-
lation will  give a great under-estimate.
                                   291

-------
     Eulerian models to date have been restricted to grid meshes  of  50  by
50 or smaller, with only one or two levels in the vertical.  For  an  area of
2000 km in horizontal dimensions, this corresponds to a 40 km grid spacing,
about five to ten times coarser than needed to describe power plant  plumes
during the daytime.  These models have furthermore carried only two  or
three chemical species and a very simply parameterized oxidation.  Regional
air quality models describing oxidant production have been limited to smal-
ler regions with dimensions of up to 800 km, allowing finer grid  resolution
(e.g., Burton and Liu's (1981) work referenced in Hayes (1981)).  Yet reso-
lution down to the spatial  scales appropriate for the first four  daylight
hours after emission appears necessary; otherwise, it will not be possible
to understand the interaction of NOX with S02 and their interactions with
other pollutants.  These interactions determine if the species will  oxidize
or undergo dry deposition near the sources.

b.  The need for fine resolution

     There are two important reasons for computer simulations of  air chem-
istry to have fine spatial  resolution:

       •  Comparison with data:  concentration measurements, made with
          point resolution in time and space, are more easily compared
          with simulations with fine spatial resolution.  The problems
          of relating the results of simple models to observations have
          been noted by those who compare them (e.g., Niemann, 1982).

       •  Averaging of nonlinear chemistry:  if the same photochemical
          and cloud chemistry are simulated with otherwise identical.
          models differing only in spatial resolution, the computed  S02
          and NOX oxidation rates may vary significantly.  This is be-
          cause grid-point modeling implicitly involves spatial averag-
          ing, and the product of averages can be much different  from the
          average of products.  Figure 6.1 shows cases where overestimates
          and underestimates can occur.  We believe that the latter  is  more
          prevalent, and will describe it more fully later in this section.

c.  The advantages of limited-resolution models

     There are also advantages to models with less spatial resolution:

       e  Interpretability:  smaller and simpler models are generally
          easier to examine and interpret than larger, more complex
          models.  It can also be argued that acid rain effects are
          averaged over many events, perhaps many years, so that
          spatially-averaged concentrations are useful.

       t  Computer storage:  the CRAY-1 computer, the largest currently
          available for this problem, can provide for arrays of one-half
          million variables (with 64-bit precision), a number that would  be
          required for the following resolution:

             50    x    50     x    8              25         =   500,000
          latitude x longitude x vertical x chemical species  "   variables

                                     292

-------
          Perhaps two or three times as many  array  elements  may  be  required
          if the integration program is more  complex.

       t  Computer time:  The integration time  required  for  a  species  will
          vary roughly as the inverse square  of the separation of grid
          points.  There are perhaps better uses  for  computer  time  than
          increasing the resolution of the model, e.g.,  validation  runs
          for components of the model, more case  studies  of  transport, and
          tests of the sensitivity of the chemical  and physical  mechanisms
          used.

6.2  Observations of the variability of S02 and NOX concentrations

     Observations made over the past decade indicate  considerable variabil-
ity of pollutant concentrations over tens of  kilometers.   Two  sorts of ob-
servations have proved particularly useful:   simultaneous observations of
many compounds made at fixed surface sites, producing a  time series;  and
airborne observations of a smaller subset of  compounds,  presenting  a  spa-
tial sampling.  Each strategy has particular  advantages,  so  we present a
glimpse of each.

a.   Aircraft observations of variability

     Figure 6.2 is a portrait of the variability  in S02  concentrations
produced in the midwestern United States by the Labadie  and  Kincaid power
plant plumes.  These plumes retain their identity for up  to  400  km  down-
wind, and during daytime they spread to widths  (half-widths) of  10  to  40
km; at night their spread is restricted to 5  km or  so, although  wind  shear
is apt to separate laminae (Gilliani et al.,  1978,  Smith  et  a!.,  1978).
Sometimes these plumes are embedded in an urban plume; the latter are  the
most significant sources of reactive hydrocarbons,  and therefore a  source
of extra photochemical activity in many circumstances.   Beyond the  plume
boundary, S02 becomes undetectable.

     How common are plumes?  Figure 6.3 shows observations made  on  a
cross-country flight during the SURE program  (Blumenthal  et  al.,  1982).
Figure 6.3a shows a region of the Midwest with  many sources  during  an  epi-
sode of regional pollutant buildup.  S02 and  other  compounds show signifi-
cant variability over distances of 25 km or so.   Backgound concentrations
of S02 between the plumes are quite high at this  time, at apparently  6-8
ppb.  Figure 6.3b shows a region with fewer sources during this  same  epi-
sode.  Background S02 concentrations in this  case are typically  a few  ppb,
a level at which S02 measurements may become  unreliable.

     A broader "climatology" of air pollution variability is shown  in  the
cumulative frequency distributions of pollutants  sampled  by  aircraft  during
the SURE program. Figure 6.4.  These cumulative distribution functions of
Figure 6.4 describe the magnitude of pollutant  variations.  The  shaded
areas in each cumulative distribution function  curve  indicate  integrals
that sum to the mean concentration of the species.  In the S02  graph,  the
horizontal lines indicate that approximately  half of  the  area  lies  in  a
thin upper portion of the graph, corresponding  to samples with more than 14
ppb mean S02 in the boundary layer.  That is, one half of the  S02 monitored

                                     293

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Figure 6.2   Horizontal  profiles  of 863 during  selected
constant-altitude aircraft traverses on July 9  and  July
18, 1976.   July 9 traverses are at about 450 m  AGL,  arid
July 18 traverses are at about 750 m AGL.   The  Labadie
plume sections are shaded.  Also  shown  are  backward
trajectories for the Labadie plume  (Gillani  et al ., 1978).
                         294

-------
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                                        DISTANCE (Ian)
Figure  6.3   Spatial  variations of ozone, nitrogen oxides  and participate
scattering within the boundary layer as sampled  by two instrumented aircraft
on flights across portions of the  Midwest.  Both flights were made during a
regional  pollutant build-up episode, 20 July  1978.  The upper figure shows
sharp peaks revealing plumes with  widths of 10  km to 100 km  rising from  back-
ground  levels elevated above normal.  The lower  figure shows  even greater
spatial  variability  in a region with lower background concentrations (figures
from Blumenthal et al.,  1981).
                                          295

-------

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was found in only 10 to 15% of the samples,  those with  concentrations  over
- 14 ppb.  This data and the data time  series  of Figures  6.3  and  6.5  show
the degree to which S02 is found in  intermittent plumes of  high concentra-
tion.  The oxidant chemistry and dry deposition properties  of the restrict-
ed regions containing this sulfur are clearly  quite  important in  evaluating
the total S02 transformation of the Midwest.

     By contrast, one half of the ozone  is contained in a minimum of  35-40%
of the samples.  The behavior of nitrogen oxides is  intermediate  between
sulfur dioxide and ozone, indicating locally great concentrations and  also
a continuous background.  The aerosol parameters, CN and  bscat, are  not
precise measures of sulfate, but the distribution function  for bscat  does
indicate the pervasive distribution  of  sulfate in space and time.

b.   Ground-level measurements of pollutant  variability

     Figure 6.5 shows pollutant variability  from another  viewpoint,  namely
the time series of concentration at a surface  site.   These  measurements
were made near the small town of Glasgow in  southern Illinois, about  100  km
north of Saint Louis (Ellestad, 1980).   The  striking attribute of the  many
pollutants displayed is their variability in time, as the instruments  sense
plumes from a variety of sources, such  as cities, industries,  and power
plants.  While some pairs of species are correlated, others are not  at all:
clearly the photochemistry of the situation  is changing rapidly on a  scale
of three hours or so.  Once again, background  S02 concentrations  frequently
fall below a 1-2 ppb apparent detection  limit. A longer  time series  of se-
lected pollutants is shown in Figure 6.6.  During this  summertime period,
the Midwest undergoes cycles of regional  accumulation of  long-lived  pollu-
tants; summertime cold fronts and possibly associated thunderstorm activity
intermittently sweep into the area,  introducing cleaner air (Chatfield and
Rasmussen, 1977).  The well defined  nature of  urban  plumes  is apparent in
the variation of CFC13, which serves as  an urban tracer.  This accumulation
and cleansing behavior takes place over  large  regions,  and  it must also be
captured in a regional model.

6.3  Physical laws, averaging, and computer  solutions;  the  mathematics of
     subgrid-scale averaging

     The mathematical description of air chemistry reduces  to a simple
equation describing the sources, conservation,  and reactions  of chemical
species.  For each species there is  an  equation of the  following  type:

                9n
                —  =  - v-(un_) + KvV +  Q   + H.                     (1)
                at        -  " a         a    a   a
                                                     Va
                                     297

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                          nsp  "SP

                        +r=l  s=l  k'

where

     n       =  number density of species  a

     nr,ng   =  number density of other  species  (molecules/cm3)

     u       =  velocity of air at each  point

     K       =  molecular diffusivity of air

     k       =  reaction rate coefficient  for  species  a  and  b  to
       '        react and product species  s

     sa      =  stoichoimetric coefficient related  to  k  (e.g.,
      a'a~"r     2 for the reaction HOO + HOO ->- HOOH +  02 when
                a = HOO)

     Q       =  physical sources and sinks of  material  (e.g.,
                pollutant emissions, dry deposition, etc.)

     H       =  cloud and aerosol interactions (likely a complex
                function of many reactive  species)

The character of these equations differs for each constituent.   For very
unreactive species, the equation is essentially  a simple partial  differ-
ential equation of transport with small  sources  and sinks  (which may be,
however, locally concentrated).  For reactive  species,  it  has  more the
character of a highly nonlinear set of ordinary  differential equations.

     These equations are several steps removed from those  equations that
can be solved numerically on a computer.   Lamb (1975,  1982)  has  pointed out
some of these differences, and much of this section follows  his  analysis
technique as applied to the problems of mesoscale air  chemistry.

a.  Averaging and computer simulation

     When we wish to understand the processes  of air pollution  chemistry
using Equation (1), we are faced with two  related facts.  First,  the air
motion fields that are shown in (1) include, in  principle,  every wind gust
and eddy down to the viscous distance and  timescales.  Such  detailed infor-
mation is, of course, not available.  Typically, what  is actually available
is one of two data sets:

 (a) Surface winds recorded by the National Weather Service  stations, typi-
     cally every three hours (at best) for stations separated  by distances
     of 40-200 km, and upper-level winds recorded every  12  hours from ra-
     windsonde stations separated by distances of around 500 km.  Local
     wind gusts not representative of the  whole  area around  the  station


                                     300

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     are registered in these  records.
                       f
 (b) Wind vectors provided by weather  forecast models with grid resolutions
     of approximately 180 km, or  similar  winds from large mesoscale models
     with grid spacing of 40-100  km.   These  are available every 10 to 60
     minutes of simulated time.   These models  must smooth out or ignore any
     wind gusts with wavelengths  smaller  than  twice the grid spacing.

This discrepancy in spatial  resolution must  be addressed before we can
solve the transport equations.

     Nonetheless, the equations of  air chemistry as stated so far are valid
at all points in space. These equations cannot be solved, however, until
they are transformed into a  system  of  difference equations through finite-
difference approximations.  As they  are most commonly stated (e.g., Lapidus
and Finder, 1982), these approximations require that grid points be located
closely enough together so as to  capture  most  of the variation of chemical
concentrations; for example,  that the  concentrations can be reasonably re-
presented by low-order polynomials  (regarded as truncated Taylor series).
This requirement is probably  not  met for  most  photochemical models, whether
describing industrial plumes, cities,  or  mesoscale regions.  Figures 6.2
through 6.6 suggest that 5 or 10  km  resolution would be required to capture
typical variations, and even  finer  resolution  would in fact be necessary in
practice.

     An alternative viewpoint is  that  the finite-difference equations de-
scribe grid-volume averages  of species concentrations.  This viewpoint ap-
pears, usually implicitly, in the construction of virtually all acid rain
and photochemical models, whether Eulerian or  Lagrangian in concept.  We
may define the volume average, represented by  a tilde, like this:


                              "a   '   {  dv  "a  '

where V represents the grid  volume.  The  continuous concentration field may
be represented in terms of means  and deviations,


                              na   =   "a +  na  '

We can make this averaging explicit.   By  averaging Equation (1) over the
grid volume, we can produce  an equation which  may be treated by finite-
difference techniques:
                      a
                    —1   =   -  V.(un)  +  T   +  Q   +  H                      (2)
                    3t         -     a     a    a     a
                                      301

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Here the latter terms represent the interplay of  subgrid-scale  variations
(i.e., sub-grid terms).  We will see that in some cases  they  are  as  impor-
tant as any other terms in the equation  (refer again  to  Figure  6.1).   The
equation is rather removed from the physical and  chemical  laws  described in
Equation (1), but it is solvable on current computers  if the  subgrid terms
are known.

     This alternative viewpoint emerges  naturally from the  finite-element
approach to the solution of partial differential  equations, which is not
based on assumptions of Taylor series approximation to smooth functions.
By using the method of weighted residuals, and the  "subdomain"-method ele-
ments and weighting functions, it appears possible  to  derive  difference
equations that are like the finite-difference equations,  but  with volume-
averaging made explicit (Lapidus and Pinder, 1982).

b.   Why are grid-point simulations often satisfactory?

     For many species in many situations, the right-hand side of  Equation
(2) is dominated by terms other than those describing  subgrid-scale  ef-
fects.  Some reasons for this include:

     (a)  Transport may dominate.  Species like sulfate  aerosol have
          sufficiently slow reaction and deposition processes that
          concentrations are determined  mainly by transport.  In  the
          relatively clean air of the unpopulated,  non-industrial  western
          North America or northern Canada, ozone,  carbon monoxide,  and
          nitrogen oxides may also be primarily determined by transport
          over hundreds and thousands of kilometers,  except within ten
          meters of the surface.

     (b)  Chemical sources and sinks may be uniform.   In the  clean
          atmosphere just described, even hydroxyl  radical  (HO) may  have
          a relatively uniform distribution, even though its  one-tenth-
          second chemical lifetime is very short.   In  this  case,  HO
          production and removal is determined by products  of concen-
          trations of ozone, carbon monoxide, nitric  oxide, and less
          reactive alkanes that are themselves smooth  functions of
          position.  Species with chemical lifetimes  longer than  HO,
          like formaldehyde and hydrogen peroxide,  with  chemical

                                     302

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          timescales of hours, will  not  so  quickly  reach  steady states,
          and can be more affected by  horizontal  and  vertical  transports.

     (c)  Intracell transport may be rapid  compared to  chemical  reaction.
          Lamb (1975) has shown that,  under certain circumstances where
          the source term Qa and chemical reactions are dominant, a
          long chemical reaction timescale  allows complete mixing.

     (d)  No branching of reactions.   There may  be  subgrid-scale terms that
          do not significantly affect  those chemical  species  of most impor-
          tance.  The only  reaction  explicitly  studied  in this context is

                                NO + 03  * N02 +  02

          (Lamb, 1975, 1980; Lamb and  Shu,  1978;  Shu  et al.,  1978).  In
          many circumstances, fresh  emissions of NO may produce substantial
          subgrid effects on small scales;  for  example, a substantial  delay
          in the conversion compared to  calculations  based on volume aver-
          ages.  Luckily, for many questions these  effects are of secondary
          importance:  NO will react with ozone  later,  there  being no  other
          competing reaction producing another  fate.  A delay of 10-20
          minutes in the conversion  of NO to N02 has  apparently little
          consequence for a subsequent reaction,  the  conversion of N02 to
          HN03, which characteristically takes  from 4 to  24 hours.  N02
          does have alternative fates:   deposition  on the ground or con-
          version to nitric acid, so that subgrid processes affecting  one
          rate have important consequences  on the production  of acid aero-
          sol and acid rain.  Similar  considerations  hold for S02.  .

c.  Limits on the magnitude of subgrid-scale effects

     Consider the simplest example of  chemical  reaction

                               a + b * c (products)

where the bimolecular rate coefficient is given  by  k.  Let us compare  the
magnitude of mean and subgrid-scale  contributions to  the  single reaction
term

                 ka,b+c Vb  =  ka,b+c  Vb

Since na and n& are positive definite, /n^> = a  nanb  for  some
factor a between zero and infinity.  The extreme cases  are:

     (a)  a = 0 when na and n^ are non-zero only in different places.
          (For example, each may undergo rapid  chemical decay or be
          transported out of the model volume.)   See  Figure 6.1.

     (b)  a = « when, for example, na  =  xnb (they have  similar sources
          and sinks), and they are very  concentrated  within the model
          volumes (e.g., in very narrow  plumes).  Then:
                                      303

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                                  -  x(nj)  >>   MS,,)*   .   n^.


We can get a rough idea of the way error  depends  on  the  degree  of concen-
tration:  if the chemical species are uniformly  distributed over  a small
volume v, much less than the grid volume  V,

                             v  =  eV,  E «  1,

and zero elsewhere, then it is easy to  show that:


                     ka,b+c  Vb  =  1/e ka,b-H: "aV

If a single power plant plume occupies  one-tenth  of  a 100  x 100 km grid,
and species a and b have^negligible concentrations outside  the  plume,  then
the error in estimating nant, by nan"b is a factor  of  tenl

6.4  Situations in which subgrid effects  are  important

     How can we reach some practical assessment  regarding  the representa-
tion of subgrid effects in the simulation of  localized intense  emissions
within large grid volumes?  What happens  when many nonlinear reactions
interact in time?  Let us focus on one  important  simulation problem,  the
emission of power-plant S02 into a relatively clean  Midwestern  rural  area.
What are the difficulties in simulating the photochemical  reaction of HO
with SO2?

     A useful general guide can be found  in the  summaries  of photochemical
smog reaction provided by the isopleth  description used  in  the  Empirical
Kinetic Modeling Approach (EKMA) to urban ozone  chemistry.   Isopleth  plots
of 03, HO, HOOH, and HN03 are shown in  Figures 6.7 and 6.8.  These species
are portrayed as functions of hydrocarbon and NOX concentration,  but  only
the lower left corner of the diagrams presented  are  applicable  to the situ-
ation of urban and power-plant plumes diluting into  a regional  atmosphere.
These figures, from Bergstrom (1981), are based  on the SAI  Carbon Bond
Mechanism of Whitten and Hogo (1978, 1979).   The  calculation algorithm
constituting this isopleth method and the further assumptions  in  the  EKMA
process are reviewed in Hayes (1981) and  references  therein.

     In brief, the two-dimensional isopleth plots show lines of equal  con-
centration of various secondary pollutants as a  function  of only  two  vari-
ables, assumed initial hydrocarbons and nitrogen  oxides,  the primary  emis-
sions.  The EKMA analysis technique, essentially  an  extension  of  early
city-smog analyses, produces predicted  secondary  pollutant  maxima that oc-
cur during the course of a day as a function  of  primary,  completely unre-
acted emissions whose concentrations are  taken to be early-morning values.
Therefore, this technique crudely calculates  the  history  of the photochem-
istry for at least one day.  However, other parameters,  such as dilution  of
material and photolysis rates, are important, and are crudely  parameterized
in EKMA.  Furthermore, other situations besides  the  morning-through-after-
noon period simulated in EKMA are important to large-scale  transformation
rates.  Nevertheless, the general shapes  of the  contour  plots  are generally

                                     304

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                 0.1
                      0.1
                           0.0
                                0.8
                                     i.o
                                          1.2
                                               1.4
                                                     1.6
                                                          i.a
                                0.8   1.0   1.2   1.4    1.6    l.f
                                   NMHC.PPHC
                     0.4    0.6    0.8    1.0   1.2   1.1   1.6   1.9
                o.z
           "
                0.2
                     0.4
                           0.6
                                0.8
                                     1.0
                                   NMMC.PfHC
                                          1.2
                                               1.4
                                                          1.8
                                                               2.0
Figure 6.7    Contour plots of hydroxyl radical  and ozone concentrations
that are simulated  as resulting from initial  hydrocarbon and NOX concen-
trations.  Point  R  depicts conditions representative of a relatively
unpolluted,  rural Midwest atmosphere.  Point  Pa indicates conditions
generally representative of a power-plant  plume dispersed through the
mixed layer.   Point Pm represents concentrations that would be simulated
by a computer model  with large (roughly  100 km) grid resolution, con-
taining pollutant concentrations from Pa and  R.  Above: HO radical con-
centration,  contours in multiples of 10-6  ppm (roughly 2.3 x 10? molecules
per cm3).  Below: ozone concentrations,  contoured in ppm.
                                      305

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                                                        1.8
                                                        1,8
                                                             2.0
Figure 6.8   Concentrations of hydrogen peroxide and nitric acid simulated
as resulting from the primary pollutant emissions of hydrocarbons and NOx-
Contours in parts per million.  This figure and Figure 6.7 are taken from
Bergstrom et al. (1981).  If these contours were equally spaced parallel
straight lines, secondary pollutants would be linear functions of primary
pollutants, and sub-grid processes would average out appropriately. They
are not,
                                     306

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similar among a variety of simulations with  varying  asumptions  (Hayes,
1981) and are complex enough to demonstrate  the  pervasive  nature  of model -
resolution effects.

     What do these contour plots  suggest  about  resolution  problems in the
case of the HO + S02 reaction?  A crude estimate of  subgrid  effects in  the
simulation of a power plant plume may be  made from Figure  6.7.  Point R
represents a rural atmosphere with 70 ppbC of hydrocarbons and  6  ppb of
NOX.   Point Pa represents the actual concentrations of hydrocarbons (70
ppbC) and NOX (50 ppb) in a power plant plume.   Virtually  all  of  the
NOX and S02 in such a plume comes from the power plant; virtually all of
the hydrocarbons come from the environment.  Assume  our regional  model  has
100-km grid resolution, and assume that this power-plant plume  actually
occupies 10% of a given grid square, which is consistent with  Figures 6.4
through 6.6.  Mass conservation then requires that the  grid-square-averaged
NOX concentration be 0.10 (plume  concentration)  + 0.9 (rural  air  concen-
tration), or, in this case, somewhat more than  0.10  of  the plume  concen-
tration.  This is represented by  point Pm in Figure  6.7.

     Now let us do a calculation  of the S02  conversion  rate  in  two ways:
first, using the actual information on plume geometry and  concentration;
and second, using grid-square-averaged concentrations and  ignoring sub-
grid-scale effects.

     The first calculation proceeds as follows.   In  the plume,  which oc-
cupies 10% of the grid square, NMHC is 70 ppbC;  NOX  is  50  ppb;  S02 is 50
ppb; and HO, from Figure 6.7, is  4xl08 ppm.  From the expression  conversion
rate = k[HO] [S02], the conversion of S02 in the plume  is  3.2xlO~6 ppm  min-
ute'1.  In the rural, non-plume air, which occupies  90% of the  grid square,
NMHC is 70 ppbC; NOX is 5 ppb; S02 is 2.7 ppb;  and HO,  from  Figure 6.7,
is IxlQ-  ppm.  Thus, the non-plume conversion  rate  is  4.3x10   ppm min-
ute  .  Finally, accounting for the S02 masses  in the plume  and in the
rural air gives a total conversion rate over the grid square of 7.1xlO~7
ppm minute  , which is equivalent to 0.57% hr"1.

     The second calculation, which ignores subgrid effects,  proceeds as
follows, where each figure given  is a grid-square average.  NMHC  is 0.1
(70) + 0.9 (70) = 70 ppbC; NOX is 0.1 (50) + 0.9 (5) = 9.5 ppb; S02 is
0.1 (50) + 0.9 (2.7) = 7.4 ppb: and HO, from Figure  6.7, is  1.4xlQ-7 ppm.
The conversion rate is 1.6xlO~6 ppm minute"1, or 1.34%  hr  .

     Clearly, very different rates of reaction  may be calculated  for S02
oxidation, depending on the degree to which  spatial  variations  of pollutant
concentrations are recognized and simulated.  In this case,  the simulated
segregation of most of the S02 from a relatively highly-oxidizing rural air
lowered the simulated reaction rate of S02 by a  factor  of  2.6.  Further-
more, the coarse-grid simulation  would suggest  that  most sulfate  production
was due to a local S02 source, while in fact most sulfate  production was
outside of the plurne.

     The numbers here are not particularly significant, but  the sample
calculation could be applied to other isopleth  diagrams and  other situa-
tions; the shapes of the contour  plots (in particular,  their nonlinearity,

                                     307

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a near-universal feature) suggest that large grid spacing will  give  sub-
stantial inaccuracies (see Figures 6.7 and 6.8).  It  is difficult  to  see
how such inaccuracies will simply "average out" due to the  complexity  of
the chemistry and meteorology; they will more likely  compound  in a confus-
ing way.  (In this case, the cruder model gave a first-order reaction  rate
for S02 nearer the currently accepted large-scale average,  about 1%  hr  ,
but for the wrong reasons.  It does not accurately reflect  the  chemistry  of
the model.)

6.5  Approximate treatments of subgrid processes

     It appears that a naive direct attempt to model  the photochemistry of
the oxidants ozone, hydroxyl radical, and hydrogen peroxide as  they  affect
the transformation of sulfur dioxide and nitric oxide to acids  would  give
results somewhat worse than current "tuned" or empirical models.  Such a
simulation would be reminiscent of the first numerical weather  forecast by
L. F. Richardson (1922)--disastrous results, but very instructive.   (Inci-
dentally,  this forecast eventually led to techniques  for treating  small-
scale phenomena.)

     There are several ways to treat small-scale processes  in  a large  meso-
scale model:

     (a)  Fine-mesh calculations within the mixed layer.  Under certain
          conditions, mesh distances of 20 km or less could be  used  in a
          computer the size of the CRAY-1 (750,000 64-bit words for  storage
          and user program).  Such a mesh could be used to  simulate  two or
          three lower layers which contain urban and  industrial plumes.
          Other layers would require much less resolution.  There  would be
          more programming overhead, possibly including word-packing,  less
          accurate numerical techniques, and a simpler photochemical  reac-
          tion set.  Calculations made using a smaller geographical  domain
          could show the magnitude of any remaining subgrid processes.
          There are problems obtaining geographical data on emissions  down
          to this fine resolution, but the major NOX  and S02 sources  have
          been identified (OTA, 1982), and an assumption that  many hydro-
          carbon emissions are primarily a function of local population
          density appears justified.

     (b)  Adjustment of emissions or concentrations.  This  apparently  has
          been the past procedure.  Hydrocarbon concentrations  have  been
          estimated on the basis of nitrogen oxide concentrations  and
          emissions estimates (Lavery et al., 1980).  Similar  approaches
          could be used to estimate net export of NOX and S02  based  on
          field studies,

     (c)  Lagrangian modeling of plumes can give estimates  of  the  export  of
          material from cities and power plant plumes (Liu  et  al., 1981;
          Durran et al., 1979; Graedel et al., 1981).  Simulations would
          be required for a variety of parameters (time of  day, size  of
          city or power plant, combined city and industrial plant).

     (d)  "Two-fluid" or "three-fluid" modeling of plumes.  It is  possible

                                     308

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         to construct consistent descriptions  of  power  plant plumes,  city
         plumes, and rural air on duplicate  arrays  for  each  species.   The
         same general description of dilution  and dispersion plumes used
         for Lagrangian models can be used to  specify transfers  of ma-
         terial between plume and non-plume  arrays.  There  are potential
         difficulties when plume materials cross  grid-volume boundaries,
         and in treating the aging of plumes.  The  simplest  technique is
         to use separate arrays for fresh and  old plumes, and transfer
         from the first to the second that portion  of material  calculated
         to cross a grid boundary.  Old-plume  air is similarly "trans-
         ported" and diluted back into  rural air.   This sort of  subgrid
         modeling is most advantageous  for larger grid  meshes {- 100  km),
         since the savings in computer  storage and  run  time  are  propor-
         tional to the inverse square of the grid mesh. Much storage is
         freed for the extra arrays required.  Certain  processes very
         difficult to model such as the transport of unreacted S02 and MO
         at night, are better treated with the larger mesh  size.  The
         method is most appropriate in  simulating the general  level  of
         concentration of plume material for non-linear chemistry, and may
         introduce small errors in the  location of  pollutant material in
         the cross-stream direction.  Such errors appear unimportant.
         Emissions inventories are also more suited for this sort of
         analysis than for fine-grid models, since  they are  reported  by
         county or large area.  All power-plant emissions in a single
         model volume need to be lumped into a single collective plume
         with an appropriate dilution rate,  but this should  capture the
         basic features of subgrid chemistry and  physics.

6.6  Boundary-layer transport and the need for fine vertical resolution

     In the preceding sections, we have demonstrated the importance of
horizontal grid resolution in the numerical  modeling of chemical reactions,
sources and sinks.  Here we illustrate  briefly the  need for  good vertical
resolution in describing near-surface chemistry in  a coupled transport-
kinetics model.

     There are two main reasons why fine vertical  resolution is  desirable:
(1) the Earth's surface and inversion base allow  sinks  for  important  com-
pounds, and (2) sources of pollutants often  are concentrated initially into
plumes, and their plume chemistry is affected  by  their  degree of concentra-
tion as seen in Section 6.4.  The effect of  concentrated sources is clear
in recent aircraft data.  Data from the SURE program suggests that vertical
variations in S02, NOX, and presumably  OH can  be  substantial.

     Figure 6.9 shows two closely-spaced aircraft spirals in the Midwest.
One spiral shows little variation below the  top of  the  inversion layer.
The other spiral shows dramatic fluctuations due  to several  plumes.  Smith
et al. (1978) have also shown complex cross-sections of such plumes,  and
Lenschow (1982) has observed the interaction of plumes  and  an inversion
layer in ozone profiles.

     Numerous models exist which solve  the species  continuity equation (2)
with vertical transport only.  Most of  these have been  used  to study  bud-

                                     309

-------
   3000
   2500
   2000
•=•  1500
W
Q
D
H
H

•<
   1000
    500
                                        — Spiral 1 - Upwind

                                           Spiral 2 - Over Station

                                           Spiral 3 - Downwind
                                                                     100
                           CONCENTRATION SO  (ppb)
        Figure 6.9  SOg profiles in the Midwest  (reported  by  Blumenthal
        et al.,  1981)  illustrate the great vertical variation  of  pol-
        lutants  that can be produced by intense  sources.   The  profiles
        with  lower concentrations show air well-mixed  in S02  upwind  of
        a source.  The profiles marked with X's  show the effect of a
        complex  source or complex striations produced  by incomplete
        mixing.  Few models can afford the expense of  simulating  such
        complexity: at least 12 levels below 200m would be required
        in order to resolve all pollutant spikes.
                                   310

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gets of longer-lived trace gases In unpolluted  situations.   The  flux  di-
vergence in those cases is represented by edciy  diffusion:
                               o*.   Z               dZ

In this equation, N(z) is the molecular  density  at  altitude  z,  and
x-(z,t) is the mixing ratio of species i.  An  eddy  diffusivity,  Kz,
typical of those used in one-dimensional  simulations,  appears  in Figure
6.10.  Note that a large diffusivity is  assumed  to  extend  to the ground.
In steady-state calculations appropriate for chemical  budget estimates,
Kz(z) is time-invariant and the  time rate of change of species  concentra-
tion is set equal to zero.

     There can be problems in using a transport  formulation  such as  that
given in Figure 6.10 even in budget calculations of background-level  chem-
istry.  For example, Thompson and Cicerone  (1982) have shown that, when a
rapidly-mixing boundary layer (Kz(z) > 106 cm2 s"1  at  the  surface)  is
replaced by a transport-resistant boundary layer, dry  deposition of  meta-
stable trace gases, e.g., HN03,  aldehydes, peroxides,  is  reduced and these
species can accumulate above the resistant layer.

     More detailed studies (Carney and Fishman,  1982;  Hov,  1982; Graedel
and Schiavone, 1981) also show the importance  of surface  layer  resistance,
although the limited applicability of one-dimensional  eddy  transport to
most meteorological situations must be kept in mind when  interpreting those
model results.  These simulations indicate the need for several  model
levels below 100 m when chemical reactions are rapid,  as  they  are near a
source region.  In some cases, however,  diffusion in the  surface layer may
be treated with an analytic approximation (Chapter  IV, Section  5).   Region-
al models of urban air pollution have also suggested the  need  for multiple
levels for the wind field in the boundary layer  and the importance of sur-
face sinks for N02, S02, and HN03 even in a small distance  scale_(Killus  et
al., 1977).

     An example of a source effect on boundary-layer chemistry  can be seen
in Hov's (1982) simulation of the moderately polluted  lower  troposphere.
Hov's model uses 20 grid points  log-linearly distributed  from  0-2 km and
a time-dependent K2 (Figure 6.11) based  on the diffusion  of  heat. The
depth of the convective boundary layer increases with  heating,  reaching a
maximum height, > 1200 m, by midafternoon and  decreasing  to  100 m by sun-
set.  Dry deposition is also reduced at  night.  Thus,  Hov  finds that,  with
boundary conditions appropriate  for a moderately polluted  atmosphere,  ozone
above the boundary layer is nearly unchanged at  night, even  though its pho-
tochemical formation has ceased.  Within the thin boundary  layer, both de-
position and destruction by reaction with emitted NO cause  ozone to  de-
crease.  In the early morning, increased convection mixes 03-rich air from
above toward the ground just as  03 is starting to be produced  photochemi-
cally.  The result is an increase in 03  throughout  the boundary layer.
Surface deposition slowdown caused by a  diurnally varying  boundary layer
causes other longer-lived gases  to accumulate  in the lower  troposphere,
e.g., HN03, PAN, S02.  Some of these effects can be seen  in  Figure 6.12.

                                     311

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      10
LU
Q

      Ql
    0.01
              I   I  I  I I I I 11     I   I
              1 T^tn |
                        II1 I  Mil
 SBLX
x
                                                NoSBL

                j	I _l_l_LLU	I   I  I  I  I I I I I	II  II  I 1 j
        I02
!0
                   I05
          Figure  6.10  Eddy diffusion coefficients with rapid
          mixing  extending to surface (no surface boundary
          layer^  Ho SBL) and with surface boundary layer (SBL)
          below 100 m  (Thompson and Cicerone,  1932).
                                  312

-------
   15

   13
.2 M
V)
c
I  9
i5
UJ  5
X
    I
    O.I         1.0         10         100
      EDDY  DIFFUSION COEFFICIENT K
                                          1435
                                          1295
                                          1157
                                          1021
                                          886
                                          754
                                          624
                                          499
                                          380
                                          268
                                          170
                                          90.6
                                          38.2
                                          12.8
                                          3.68
                                          1.00
                                                         m
                                                         o
                                                         x
                                                         H
                                      1000
Figure 6.11   Calculated profiles of eddy diffusion
coefficient  K(z,t) for chemical transport at various
times of day (Hov, 1982).
                   313

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                                                         l\W/f  OH
                                                         1 , ^ I I (x 10*)
                                         //
        ii-n-ii-ii irii'irirH'irn ii-ii-n7ij-n'
•q.Braa       \mffm;
 ^ii'ii'ii'ii'iru irii ii'irii'ii'!i-irii
    1E5B-
UJ
o
                                                             HNO,(ppb)
                                        • 11 • fI•11•if•11•u • i i • 11 • II • 11 • i I • 11 • n' 11' 11 ii
                                                       NMHC (ppbC)
                                  TIME OF DAY
          Figure 6.12    Time development of species  in  a moderately
          polluted boundary layer calculated in a  one-dimensional
          model with the time-dependent eddy diffusion  profiles of
          Figure 6.11 .  Note the build-up of material  in the mid-
          boundary layer region during the second  day of simulation.
          Emissions near the lower boundary are distributed over the
          lowest three  grid points:  NCL, : 2 x 10" cnr2 s"1;  S02,
          NMHC (nonmethane hydrocarbons) and CO fluxes  are 1.5,
          1.5 and 10 times the NOX flux  (Hov, 1982).
                                    314

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The variable boundary layer also results  in  a  large  positive  deviation from
the photostat!onary state (Calvert and Stockwell,  1982)  within  the convec-
tive boundary layer and a negative deviation at  the  surface.

     The implications of these  vertical gradients  for  longer-term and
longer-range transport are not  clear.  Some  indication  is  given in a  recent
study (Carney and Fishman, 1982) which focuses on  chemical  exchange between
the boundary layer and the free troposphere.   In this  calculation, a
"burst" of convective transport is simulated with  a  brief  period of intense
upward vertical motion {i.e., high eddy viscosity).  Greenhut et al.  (1981)
have observed and others have modeled an  important role  for such mixed-
layer venting due to clouds (see Chapter  V, Section  4.2).   Hence,  oxidants,
oxidant precursors, and acids may accumulate above the  boundary layer, and
the ratio of hydrocarbons to NOX may have pronounced vertical structure
extending into the free troposphere.

     Vertical gradients may be  partially  offset  by advection.   Graedel and
Schiavone (1981) and Schiavone  and Graedel  (1981)  simulate urban chemistry
in two dimensions for both stagnant and convective conditions.   Vertical
transport is limited to a three-element vertical mesh,  but in the convec-
tive case a simple advection scheme is used  to study horizontal transport
over a 140-km-wide region which includes  a  segment of  intense pollutant
emission.  Graedel and Schiavone (1981) predict  that OH  and H02 (as well  as
03) are small near the source of intense  hydrocarbon and NOX  emissions
and increase with altitude.  Graedel and  Schiavone argue that,  as a conse-
quence of the OH minimum, only  air upwind and  downwind  of  the emissions
center will be rich in oxidants and more  stable  products such as HN03 and
S02.  Thus, unless they are efficiently scavenged  or removed  rapidly
through OH attack or photolysis, these species are available  for transport
into the free troposphere and can travel  far from  a  source region.  For
example, Graedel and Schiavone  (1981) predict  that significant  fractions  of
anthropogenically-emitted C, S, and N compounds  (74% C,  12% N,  and 10% S)
will be transported beyond 100  km of the  source  region  even with dry  depo-
sition and aerosol scavenging of these species.  Since  scavenging is  the
major loss mechanism, these fractions are very sensitive to the treatment
of heterogeneous removal.  It should be pointed  out  that Graedel  and  Schia-
vone's prediction of minimum OH near the  emissions source  is  in disagree-
ment with Hov's (1982).  The reason is that  oxidant  levels are  highly sen-
sitive to the assumed hydrocarbon/NOx ratio  (Chapter V,  Section 1), which
differs in the two studies.

     From this brief summary of model and experimental  studies, it appears
that three or four concentration values in  the vertical  might reproduce
observed pollutant variation.   A larger number would be  required to show
detailed features of the vertical distribution.  Obviously,  in  formulating
a regional-scale model, the need for vertical  resolution must be weighed
against the demands for horizontal accuracy  and  the  number of chemical and
meteorological variables.
                                     315

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7.  NUMERICAL METHODS

7.1  Introduction

     Long-range transport of air pollutants has  received  increasing  atten-
tion during the last decade.  Numerical models have been  utilized  to study
the dispersion, transport, and deposition of pollutants and  to  regulate the
emission of pollutants from various sources.  Such models  employ two funda-
mental but different approaches, the Lagrangian  and Eulerian, which  have
been reviewed by Anthes (1979) and Eliassen (1980) in  detail.   In  order to
include necessary physical and chemical processes which may  be  highly.non-
linear, the Eulerian approach is considered better for regional-scale phe-
nomena.  Detailed justification for this choice  is given  in  Section  1 of
Chapter III.

     In general, models for atmospheric dispersion and transport of  pollu-
tants are "kinematic" models.  In such models, the atmospheric  circulation
itself is not calculated, but the limited information  on  the motion  that is
known from observation is used as a model input.  However, more general
systems can be developed in which the regional-scale dispersion and  trans-
port model of pollutants is driven by a regional meteorological model  which
will be capable of simulating real meteorological events.

     For Eulerian grid computations, the concentrations of pollutants have
to be nonnegative, and when the concentrations have no sources  or  sinks
they must be conserved.  Molenkamp (1968), Crowley (1968), Mahlman and
Sinclair (1977), Long and Pepper (1981), and McRae et  al  (1982) have pre-
pared excellent reviews on different numerical schemes applicable  to a sca-
lar quantity, and comparisons among them also have been made.   Those which
have shown potential for use in a multidimensional transport model  are sum-
marized as follows:

7.2  Particle-in-cell scheme

     In this scheme, pollutant concentrations are represented by Lagrangi-
an-marker particles inside a fixed Eulerian grid.  The transports  of pollu-
tants are obtained from the trajectories of the  particles.   The scheme has
been applied to a photochemical smog model by Sklarew  et  al.  (1972), and to
a tracer model by Lange (1976).  Later it was coupled  with a two-dimension-
al mixed-layer model to study the transport of S02 in  a boundary layer
(Anthes, 1979).  The moment scheme devised by Egan and Mahoney  (1972) may
be regarded as an extension of the original particle-in-cell  concept.  It
is a material-conserving computational procedure involving the  zeroth,
first, and second moments of the concentration distribution  within each
Eulerian grid element.  The accuracy of  the moment scheme has been further
improved by readjusting the second-moment of the distribution with a
width-correction technique (Pedersen and Prahm,  1974;  Prahm  and Pedersen,
1978).

7.3  Pseudo-spectral scheme

     Using globally continuous and orthogonal functions,  the spectral and
pseudo-spectral schemes can produce highly accurate numerical solutions to

                                     316

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the nonlinear advective-diffusive-type equation.  In applying  these
schemes, periodic boundary conditions are necessary.  This  is  recognized  by
Christensen and Prahm (1976), who employed the pseudo-spectral  scheme  in
their pollution model.  In order to expand the pollutant concentration  into
Fourier functions, they have assumed that the concentration  decays exponen-
tially in the two outmost row and column grid points, and that the time-
tendency of concentration vanishes at the boundary.  Such unrealistic  as-
sumptions may quite possibly cause steep gradients of concentration  along
the boundary of a limited-area model.  Other applications of the  pseudo-
spectral scheme to atmospheric advective and diffusion models  are  reported
by Prahm and Christensen (1977), Berkowicz and Prahm (1978), and  Wengle and
Seinfeld (1978).

7.4  Finite-element scheme

     A linear combination of locally-continuous basis functions can  be  cho-
sen to approximate the advective-diffusive equation.  The scheme  requires
that the error between the differential equation  and the approximate equa-
tion be orthogonal to all the basis functions.  Then the coefficients  in
the linear combination of basis functions can be  obtained by solving an
algebraic matrix equation.  Basic principles of the finite  element scheme
can be found in Strang and Fix (1973).  The scheme with simple chapeau
function has been applied to the pollution model  with even  grid spacing by
Pepper and Baker (1974).  The use of the scheme on variable  grid  spacing  is
discussed by Raymond and Gardner (1976) and Pepper et al. (1979).  Recent-
ly, a substantial effort to apply finite-element  schemes with  high-order
basis functions to air pollution models has been  undertaken  by a  research
group at the Lawrence Livermore National Laboratory (Lee et  al.,  1976;  Lee
and Gresho, 1977; Gresho et al. 1979).  Other groups have also been  heavily
engaged in research in this area.  The computational algorithm is  quite in-
volved and complex.

7.5  Upstream-correcting scheme

     To solve the advection equation for a nonnegative scalar, the simplest
numerical scheme is the upstream scheme, which does not generate  numerical
dispersion but suffers from very strong numerical diffusion  (Molenkamp,
1968).  The deficiency of the upstream scheme has been corrected  by  hybrid-
izing with other mass-conserving schemes.  The flux-corrected  transport
scheme (Boris and Book, 1973, 1976; Book et al.,  1975; Zalesak, 1979)  and
the self-adjusting hybrid scheme (Harten, 1978; Marten and  Zwas,  1972)  are
based on a hybrid scheme in which the advective flux is given  as  a weighted
average of the first-order positive definite scheme's flux  and the high-
order mass-conserving scheme's flux.  These methods are used to study
shocks and contact discontinuities, and results are very accurate.   How-
ever, the usage of these schemes is rather limited for atmospheric models
of pollutant transport because of the excessive computational  time re-
quired.  Purnell (1976) has introduced the upstream-interpolation  scheme.
The advection term in the original upstream scheme is approximated by  a
cubic spline instead of a truncated Taylor series with first-order accu-
racy.  This scheme has been applied by Mahrer and Pielke (1978) in their
studies of air flow over a mountain and sea and land breezes.   In  their
study of stochastic condensation theory, Clark and Hall (1979) have  sug-

                                     317

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gested a nonlinear switch in their hybrid  numerical  scheme  of  the  upstream
scheme as a low-order approximation and Crowley's  (1968)  scheme  as a  high-
order approximation, in order to assure positive definiteness  of several
field variables.  This approach is adapted from a  concept by Mahlman  and
Moxim (1978).  The nonlinear switch does not  satisfy  the  sufficient condi-
tions to be a monotone operator which guarantees positive definiteness, as
described by Marten (1978), but the switch does prove  to  be adequate  for
their numerical experiments.  Smolarkiewicz (1982) has  improved  Crowley's
original (1968) scheme by retaining the cross-differential  terms (Leith,
1965) of the numerical approximations in the  multidimensional  flux-form
advection equation.  Smolarkiewicz (1983)  has also proposed a  new  posi-
tive-definite advection scheme which has a simple  form, small  implicit
diffision, and a low computational cost compared with  the previously
mentioned variations of the upstream-correcting scheme.   The implicit
diffusion is first identified in an analytic  form, and  then a  simple  anti-
diffusion procedure is developed to restore the artificial  diffusion  with-
out inducing numerical dispersion, which could generate the negative  scalar
concentration values.

7.6  Numerical  schemes for chemical systems

     From the previous discussions, it is  clear that  almost none of the
existing acid deposition models in the literature  has  included a detailed
description of chemical interactions and transformations  of acid precursors
(Rodhe et a!.,  1981).  The previous chapter (Chapter  V) has described in
detail the wealth of knowledge that is being  ignored  by the simple "percent
per hour" sulfate loss rates that are in common usage.  One virtue of such
a simple chemical model is the avoidance of sophisticated numerical.analy-
ses necessary for dealing with the complex system.  However, if  we are to
understand the chemistry of acid deposition,  then  we  must face the full
complexity as outlined in Chapter V.

     It is well known that differential equations  arising from chemical
kinetics interactions are often difficult  to  solve numerically (Curtiss and
Hirshfelder, 1952; Chang et al., 1974).  This difficulty  is generally de-
scribed as the problem of "stiffness."  A  complex  chemical  system  often
includes many interactions with greatly differing  reaction  rates or time
constants.  This results in a unique computational dilemma  for the mathe-
matical  system:  when the desired solution contains  closely-coupled com-
ponents with greatly differing time constants, in  order to  obtain  the solu-
tion at late times (or great distances), one  must  compute accurately  at all
times the evolution of the already-equilibriated components, which in fact
may contribute very little to the components  of interest.  Many  powerful
and highly-accurate numerical techniques have been developed and used for
stiff ordinary differential equations (Gear,  1971; Lapidus  and Seinfeld,
1971).  However, there are only limited applications  to coupled  transport
and chemical kinetics equationss e.g., systems of  coupled partial  differ-
ential equations (Chang et al., 1974; Edelson and  Schryer,  1978; McRae et
al., 1982).  In general, there are three approaches:   the method of frac-
tional steps, the method of lines, and family grouping.

     The method of fractional steps (Yanenko, 1971),  or the operator  split-
ting technique, at first may appear to be  a natural  method  for this type  of

                                     318

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system of equations.  By splitting  the  transport operator and the chemical
operator and treating each- with  the most  accurate numerical  scheme,  this
method conceivably can deal with  all  the  intrinsic difficulties of this
system.  However, it quickly becomes  evident  that every  time the transport
operator is applied, the chemical system  is  rudely perturbed and a signi-
ficant amount of computing is  then  required  to  smooth the total system
again.  This is very similar to  the basic difficulty  in  computing nonlinear
chemical interactions in a Lagrangian Gaussian  plume  model.   The Lagrangian
transport of Gaussian plume is but  a  special  case of  the split transport
operator for the whole system.  The recent review by  McRae et al. (1982)
provides an excellent detailed summary  of recent findings.

     In the method-of-lines technique,  the transport  operator is first
discretized over an Eulerian grid,  perhaps with one of the previously men-
tioned schemes.  The resulting system of  ordinary differential  equations
can then be solved with an appropriate  stiff  solver.   This approach  is both
accurate and flexible for one-dimensional  models, but already for two-di-
mensional models it is found to  require an inordinate amount of computer
memory and execution time.  For  example,  a 50 by 50 two-dimensional  grid
with 30 chemical species would result in  a system of  75,000  coupled  ordi-
nary differential equations.  Clearly,  this  approach  is  impossible for
three-dimensional models.

     The final alternative, family  grouping,  is less  mathematical and de-
pends heavily on our understanding  of the whole chemical system.  Although
it has seen broad applications both for stratospheric models and air qual-
ity models, there exists no detailed  analysis from the computational  (nu-
merical) viewpoint.  In this approach,  subsets  of closely-coupled chemical
species are first identified, which then  provide a reduced set of equations
to be solved.  At each time step, the families  are then  partitioned  into
their components, which in turn  determine the various rates  of chemical
interactions.  This final partitioning  can only be achieved  with a heavy
dose of physical insight and intuition.  Without these physically-based
constraints, usually in the form  of algebraic relations, the system  of
mathematical equations representing the partitioning  operation is underde-
termined.  The choice of family  groupings is  non-unique  and  often changes
as the initial conditions and  physical  problems change.   In  contrast to the
other two approaches, this tends  to limit the generality of  the solution
scheme.  Much research is still  needed  in this  area,  especially since this
may be the only viable approach  suitable  for  the detailed chemistry  in acid
deposition models.
8.  MODEL VALIDATION AND SENSITIVITY  ANALYSIS

     Hypothesis:  The  long-term-average  distribution of wet and dry deposi-
tion is determined by  highly-variable deposition  patterns that can be re-
lated to distinct synoptic  types.  The deposition associated with these
types is a function of ambient  concentration, wind speed, temperature, and
solar intensity and cloud and precipitation  type  and amount.  Both the am-
bient concentrations and the meteorological  components have predictable and
stochastic components.  Therefore, to understand  the long-term distribution
of total acid deposition, it is necessary  to study and understand both the

                                      319

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predictable and stochastic components of the deposition patterns associated
with each synoptic type.

8.1  Introduction

     Current models of long-range transport and acid deposition are highly
parameterized models of the complex meteorological and chemical processes
that determine acid deposition.  Deterministic (as opposed to statistical)
models, incorporating all relevant meteorological and chemical processes,
are necessary for an understanding of the entire process of acid deposi-
tion, from sources to receptor, an understanding of the relative contribu-
tions to the total process by individual components, and a proper design of
control strategies.

     The current status of acid precipitation models is summarized well by
Dittenhoefer (1982):

    "Considerable improvements in the accuracy of LRT/acid precipitation
     models are needed before they can be applied in the evaluation of  al-
     ternative emission control strategies and in policy and planning
     studies.  The predictive success of LRT models is limited by a lack of
     detailed understanding of the temporally-and spatially-varying proces-
     ses of emission, transport, chemical transformation, and deposition;
     by the constraint of treating these processes in a computationally
     efficient manner; and by the adequacy of input data bases.

     Little consensus of opinion exists among modelers concerning the
     specification of the wind field, and the methods employed all suffer
     from various shortcomings.  These transport mechanisms generally  ig-
     nore vertical motions, wind shears, diurnal mixing depth variations,
     vertical pollutant profiles, atmospheric thermal structure, precipi-
     tating cloud type, and major scavenging mechanisms.  Although these
     factors are important for short-term, episodic analyses, it remains to
     be seen if these limitations seriously affect long-term impact assess-
     ments.

     Most LRT models treat sulfur chemistry only as a highly parameterized,
     linear process, ignoring total acid formation and precipitation neu-
     tralization processes.  Models fail to treat aqueous phase chemistry,
     which may be less than first order with respect to emissions, and
     ambient air quality (i.e., photochemical oxidants), which may limit
     sulfuric and nitric acid formation.  Until a nonlinear, multi-species
     approach is incorporated into these models, accurate estimates of  the
     Tmpact on acid deposition resulting from incremental changes in emis-
     sion are not possible."

     Even when a deterministic model combining meteorology and chemistry
with state-of-the-art components is developed, its use in identifying  and
isolating physical processes, improving understanding, and evaluating  al-
ternative control strategies is not straightforward.  This is because  even
the best deterministic model will always have an uncertainty  (random or
stochastic) component associated with any given prediction or realization
because of inherent uncertainties in the model input data as well as the

                                     320

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model parameter!'zations and numerical approximations.  While a model may  be
"perfect" in the sense that a large number of realizations with  slightly
perturbed initial conditions, physical parameter!'zations, etc. will cluster
around the true solution, any single realization cannot be expected to  co-
incide perfectly with the particular atmospheric evolution.  This  stochas-
tic component undoubtedly varies greatly under different weather regimes
and seasons.  Thus, a careful design of a scheme for evaluating  determin-
istic models is necessary, and this design must explicitly recognize the
stochastic nature of the problem.  A similar strategy must be worked out
for application of the model by policy-makers--for example, to test the
impact of reduced emissions in certain areas of regional acidification.
Without a recognition of the stochastic component, misleading conclusions
regarding the effectiveness of proposed regulatory options could easily
result.

     This fundamental uncertainty problem is schematically illustrated  in
Figure 8.1.  Uncertainties and errors (represented by volumes in n-dimen-
sional space) associated with meteorological data and the numerical and
physical approximations in the numerical model lead to uncertainties in
meteorological solution space.  These uncertainties, together with addi-
tional uncertainties introduced by the emissions inventories, initial chem-
istry data, and the chemistry parameterizations, lead to a final uncertain-
ty in the concentration (or deposition) space.  The problem is to  quantify
how these uncertainties propagate through the entire system, amplifying or
damping in the process.

     This section on validation assumes that a complete deterministic model
with all relevant physical and chemical processes can be developed,.and
that this model is "perfect" in the sense described above.  It outlines a
strategy for testing the hypothesis that the acid deposition model is a
perfect model and for assessing the uncertain, or stochastic, component of
its simulations or predictions under various meteorological conditions.

     An outline of a strategy for validating a complete model is as fol-
1 ows:

1.   Validation of individual components and assessment of uncertainties

     1.1  Meteorological components

          a.  Testing of physical parameterizations, such as PBL processes,
              in one-dimensional models under simplified atmospheric condi-
              tions  (e.g., homogeneous, steady state) against observations
              for special field programs (e.g., SESAME).

          b.  Verification of complete meteorological model using  opera-
              tional and special data sets with various objective  measures
              of skill.

     1.2  Chemistry components

          a.  Testing of chemical parameterizations, such as the aqueous
              phase reaction scheme, in zero-dimensional (box) models using

                                     321

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     SOURCES  OF UNCERTAINTY IN THE
     REGIONAL ACID DEPOSITION MODEL
  MET
  DATA
                MET MODEL
                •PHYSICS
                •NUMERICS
  MET
-**  SOLUTION
       CHEM
       INITIAL
       DATA
EMISSIONS
                  AQM
               TRANSPORT
               DIFFUSION
               TRANSFORMATION
               REMOVAL
                               CONCENTRATION
                                   SPACE
 Figure 8.1   Sources of uncertainty in the regional
 acid deposition model.

-------
              laboratory data.

          b.  Verification of complete chemical model components  (such  as
              the gas phase chemistry submodel) against  results of more
              complex models (e.g., Whitten et al.,  1980; Atkinson et  al.,
              1982), validated against smog chamber  studies  (Jefferies  et
              al., 1982).

          c.  Review of existing field data to determine possible assess-
              ments of chemical components under  simplified  meteorological
              conditions.

2.   Validation of complete acid deposition model

     2.1  Analysis of deposition associated with  each synoptic  type,  sensi-
          tivity tests, Monte Carlo simulations,  tests against  special  data
          sets, verification of "structure" or "climatology" of model.

     2.2  Preparation of climatology of  synoptic  types and integration  over
          expected frequency to obtain monthly, seasonal, or annual  aver-
          ages.  Comparison against long-term average data.

8.2  Discussion of validation strategy

     There are two phases to the validation strategy.  The first  phase  is
to validate each component separately, under simplified  conditions,  to  es-
timate the error (uncertainty) associated with that  component.  The  uncer-
tainty of a particular component is evaluated by  performing  a set of  com-
puter experiments in which input data are varied,  and then comparing  the
results of each experiment to observations.  The  variations  in  input  data
are determined by the uncertainty  in the data.  From the set of compari-
sons, statistical measures such as variance and bias are calculated,  and
significance tests are performed for each model component evaluation.   This
information comprises the estimate of error associated with  each  component.

     An example is the testing of  the physical components of the  meteoro-
logical model, such as radiation or boundary layer physics,  against  special
data sets.  For example, Driedonks (1982) describes  the  performance  of  a
slab model for the evolution of the mixed layer during the day.   Zhang  and
Anthes (1982) tested Blackadar's PBL model under  both day and night  condi-
tions using the SESAME 1979 data set.

     Similar tests must be done for all  components,  including the chemistry
modules.  The data to be used in these tests can  be  obtained from field
studies, laboratory experiments, and more complicated models that have  al-
ready been validated.  For example, assume the gas phase chemistry model  is
based on existing, more complicated models (e.g.,  Whitten et al., 1980)
which are verified with smog chamber data (Jefferies et  al., 1982).   In
this case, the model component is  tested against  existing model results.

     For the component evaluations, a wide range  of  possible conditions can
be tested.  When it is determined  that critical data are inadequate,  addi-
tional field or laboratory studies will  be needed, and the model  components

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can be used to help design the necessary measurements.  However,  we  anti-
cipate that sufficient data already exist for a preliminary  evaluation  of
each component.

     In addition to evaluation of the individual components,  similar eval-
uations can be made with various combinations of components.  For example,
the radiation and turbulent mixing parameter!' zations  can  be  combined and
tested in a one-dimensional model.  Similarly, gas and  aqueous  phase chem-
istry can be combined and evaluated in a zero-dimensional model.   The com-
plete meteorological model can be evaluated separately  from  the chemistry
component, using the various measures of skill discussed  in  Chapter  HI.
Likewise, the chemistry model can be exercised under  simplified meteorolo-
gical conditions such as discussed by Lamb (1982) regarding  the evaluation
of regional oxidant models.

     The testing of a complete acid deposition model  also must  recognize
the stochastic component of the problem.  Since the uncertainties in many
variables must be considered, it is necessary to use  variations of the  Mon-
te-Carlo method to estimate the uncertainties associated  with predictions
under various meteorological  situations.  A complete  Monte Carlo  treatment
--the random varying of all of the sources of model uncertainty — is  not
feasible or required.  Many of the variable uncertainties can be  inves-
tigated using sensitivity studies and/or by grouping  dependent  variables
together into a single examination.  Some aspects of  this approach have
been used in the evaluation of global climate models  (Katz,  1982).

     The first step in the validation of an entire model  is  the identifi-
cation of weather types (Figure 8.2) that contribute  to the  annual depo-
sition.  For example, Niemann et al . (1979) identify  ten  synoptic weather
types that contribute to regional sulfate episodes.   Ladd and Driscoll
(1980) present objective and subjective methods of identifying  weather
types.  The types must be chosen carefully to include dry and wet deposi-
tion patterns associated with nitrogen as well as sulfur  compounds.   Those
types that produce the greatest contribution to the total annual  deposition
should receive the greatest attention.  These types can be identified from
previous observational studies (e.g., Niemann, 1982)  as well  as preliminary
exercises of the complete model.

     Having stratified the meteorology into a reasonable  number (M « 10-20)
of types, where the expected annual frequency f^ of each  type is  known, a
number (N) of modified (as defined above) Monte-Carlo runs can  be made  for
each type.  The number of runs is determined by the number of model  uncer-
tainties that need to be considered.  From these runs,  the mean deposition
DJ and the variance Vj of the deposition can be computed  for each i'th
type (Figure 8.3).  The annual estimate of mean and variance can  be  com-
puted from
                                ,   M
                          U  -  £  ^i S


and


                                     324
                                          f.                             (1)

-------
            All
          Others
             (13)
Figure 8.2   Example of synoptic  types con-
tributing to annual deposition in a given
region.
                     325

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   CANADA
   UNITED
   STATES
Figure 8.3   Illustration of the average (solid line)
and standard deviation  (dashed line) of deposition
obtained  from N Monte Carlo runs under synoptic type M,
                         326

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                                M
The standard deviation, a, is simply /V.

     The model can now be verified  in the climatological  sense  by  comparing
paring Uwith the observed U.  The  standard  deviation  gives  an  estimate of
the uncertainty associated with IT.  The smaller V,  the greater  the predict-
ability.  Verification is done by testing the probability  that  the differ-
ence between the observed and predicted values of D" is significant.   The
estimation of variance, bias, noise, and gross error (Fox, 1981)  is  also
important for assessing the significance of  changes  produced by  variations
in the emissions.  The statistical  significance of  such changes  can  be  es-
timated by standard tests (e.g., F-Tests and T-Tests).

8.3  Synergistic relation of modeling and measurement  programs

     Complete validation of a total model is an evolutionary process.
Appropriate data bases for testing  the model under  some of the  important
conditions exist, but it is likely  that these bases  are incomplete.   Model
simulations and tests can be helpful in identifying  the weaknesses in the
data bases, and can be used in the  design of future  measurements  programs.
A synergistic interaction between modeling and field experiments  can lead
to improvements in both modeling and measurement programs.

     Ideally, one would test a model under different emissions,  since the
ultimate practical use of a model is to assess the  impact  of changes in
emissions.  However, it is unlikely that in  such experiments varying real
emissions will be possible.  Therefore, a model must be used in  much the
same way that climate models are used to assess the  effects  of  C02 in-
creases or changes in sea-surface temperature.  First  the  model  is vali-
dated in a climatological sense, using current emissions;  then  the assump-
tion is made that the changes in deposition  associated with  hypothetical
changes in emissions would be a good estimate of the actual  changes  that
would occur if emissions were changed.

8.4  Sensitivity analysis

     Every model is an approximation of the  existing state of knowledge.
Even if it is validated to the fullest extent possible with  existing data,
its prognostic application, by definition, means projection  into  the un-
known.  The correctness of its fundamental physical  principles  and the
demonstrated validity of its theoretical equations  lend a  significant level
of credibility to model predictions (assessments).   Nevertheless,  it is
perfectly reasonable and often necessary to  ask "How certain are  the pre-
dictions?"  Sensitivity analysis is a technique for  providing some quan-
tifiable answers to this often-posed question.

     All input information to a model contains inherent uncertainties.
These data must then be organized into forms usable  by a model.   Whenever
data are manipulated, additional errors may  creep in.   Given an  estimate of

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the range of uncertainty in the data set, it  is possible  to  derive  the
corresponding range of predictions and some estimate of the  most  likely
results.  Strictly speaking, the initialization procedure for  a meteoro-
logical model (Chapter IV, Section 2) is a well-studied special case  of
model sensitivity analysis.  The need also exists  for  a parallel  procedure
for chemical species.  Unfortunately, no such work  has been  done  except  for
a preliminary report by Dennis et al. (1982).  The  available sensitivity
analysis on uncertainties in source  functions with  Lagrangian  Gaussian
plume models sheds very little light on Eulerian grid  models due  to the
intrinsic linearity of the former type of model.  The  detailed consider-
ation of nonlinear processes presents the most interesting possibilities.

     Sensitivity analyses on model input parameters such  as  chemical  kine-
tics rate coefficients, hydrological submodel parameterizations,  radiative
processes, or even model grid resolutions have only been  done  in  a  limited
sense in stratospheric chemical models and air quality models  (Duewer et
al., 1977; Stolarski et al., 1978; Cukier et  al.,  1973; Schaibly  and  Schu-
ler, 1973; Til den and Seinfeld, 1982).  The techniques range from simple
parametric analysis to full Monte-Carlo simulations.   Although these  tech-
niques are all well established, their pragmatic implementation in  acid
deposition modeling is yet to be studied.
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                               CHAPTER SEVEN

                          SUMMARY AND CONCLUSIONS
     In this report, we have reviewed the existing  numerical  models  for
acid deposition, air quality, and mesoscale meteorology.   We  have not at-
tempted an exhaustive review, but rather a critical  review based  on  analy-
sis of the fundamental physical processes.  After having  examined much of
the relevant, published literature, we have concluded  that a  comprehensive
acid deposition modeling system on an Eulerian  grid can be developed in a
few years by a sufficiently broadly based and closely  coupled research and
development team.

     While most, if not all, past and present models have contributed to
our understanding of acid deposition phenomena,  there  are important  fun-
damental weaknesses in existing models of regional  acid deposition.   The
crude, empirical parameter!zations of major physical processes in these
models severely limits their predictive capability.  The  lack of  proper
upper-air transport and dispersion, omission of  detailed  chemical  reac-
tions, lack of cloud physics, and the absence of terrain  and  surface ef-
fects in existing models are particularly critical.  Chapter  III  has sum-
marized the current status of existing models with  emphasis on the extent
to which they deal with these key physical processes.

     Recent advances in understanding these key  processes,  as discussed in
Chapters IV and V, suggest that major improvements  in  modeling both  the
meteorological and chemical aspects of acid deposition processes  can be
made.  Our reviews of these advances are quite  detailed,  and  motivated by
our desire to highlight the vast untapped scientific resources for acid
deposition modeling.  We devoted considerable space to the procedures for
assessing the so-called "goodness" of mesoscale  numerical  models. There is
an urgent need to extend these concepts to regional  acid  deposition  models.
This is particularly important in view of the potential role  of acid depo-
sition models in regulatory considerations.

     As is well recognized, there is an embarrassing absence  of chemical
details in existing acid deposition models.  Although  there are many rea-
sons for this, the lack of understanding of the  fundamental  chemistry is
certainly not one of them.  The wealth of information  noted in Chapter V
clearly supports the cry for action now.  Although  there  are  gaps in our
understanding of all the transformation and deposition mechanisms in the
acid rain process, without a comprehensive model we cannot utilize the
available scientific knowledge properly and cannot  even reliably  evaluate
the remaining uncertainties.  The chemical system is so complex that, with-
out the proper accounting of the full set of interactions,  it is  difficult
to assess the need for better information on solution  phase chemistry and

                                     329

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heterogeneous processes, for example.

     However, these advances cannot be achieved without  research  and  de-
velopment efforts on all components within the idealized modeling system
concept discussed in Chapter VI.  The essential areas  of model  validation,
initialization, and sensitivity analysis, all critical factors  in the de-
cision-making process, need particular attention.  The development of such
a comprehensive model system requires a clearly focused, multidisciplinary
group effort under strong scientific leadership.  Much potentially useful
work relevant to the design of a comprehensive acid deposition  model  has
already been done, and this work should be used whenever feasible in  the
development of the model system.  Nevertheless, critical reexamination  of
available results in the context of the structural requirements of the  com-
prehensive model system is still required.  Because of the  desire for mod-
ular structure, for ease in incorporating new concepts and  ease of physical
interpretation of modeling results, we judge the Eulerian framework as  most
suitable for representing the essential physical and chemical processes in
regional acid deposition.

     In our companion report, Regional Acid Deposition:  Design and Manage-
ment Plan for a Comprehensive Modeling System, we present a framework for  a
model system incorporating our findings.This companion document also  out-
lines the implementation of this modeling project and  some  details on model
components and system integration, keeping in mind the broad  spectrum of
potential users ranging from research students to regulators.
                                     330

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                               CHAPTER EIGHT

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Kaiser, E. W., and C. H. Wu, 1977:  A kinetic study of the gas-phase forma-
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                                     386

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                                  TECHNICAL REPORT DATA
                           (Please read Instructions on the reverse before completing)
. REPORT NO.
                             2.
                                                          3. RECIPIENT'S ACCESSIOWNO.
 TITLE AND SUBTITLE
 REGIONAL  ACID DEPOSITION:
 PROCESSES
                                                          5. REPORT DATE
MODELS AND PHYSICAL
                             6. PERFORMING ORGANIZATION CODE
. AUTHOR(S)
                                                          8. PERFORMING ORGANIZATION REPORT NO.
The NCAR Acid  Deposition Modeling Project
. PERFORMING ORGANIZATION NAME AND ADDRESS
National  Center for Atmospheric Research
P. 0. Box 3000
Boulder,  Colorado  80307
                                                          10. PROGRAM ELEMENT NO.
                              CCVNIA/01 Task 2295  (FY-84)
                             11. CONTRACT/GRANT NO.
                              Interagency Agreement  No.
                              AD49F2A203
12. SPONSORING AGENCY NAME AND ADDRESS
Environmental  Sciences Research Laboratory  -  RTP,  NC
Office of  Research and Development
U. S. Environmental  Protection Agency
Research Triangle Park,  NC
                             13. TYPE OF REPORT AND PERIOD COVERED
                              Final - 7/1/82-5/31/83	
                             14. SPONSORING AGENCY CODE
                              EPA/600/09
15. SUPPLEMENTARY NOTES
16. ABSTRACT
This  report  represents the results of a  ten-month study on the current status  of
research on  fundamental  concepts and physical  processes relevant to regional acid
deposition modeling.   The role of models  in  environmental  assessment is first  de-
scribed.  This  is  followed by a review of existing models  in a chapter designed more
to establish a  reference framework for the bulk of the report than to provide  a
comprehensive review.   Most, if not all,  of  the principal  concepts in model  con-
struction and evaluation are discussed.   Extensive discussions of state-of-the-art
regional meteorological  modeling and the  chemistry of acid generation in  the tropo-
sphere  are presented  in Chapters IV and  V.   Chapter VI then focuses on the develop-
ment  of a new generation of acid deposition  models.  Based largely on the topics
reviewed in  earlier chapters, the desirable  features of a  comprehensible  model  are
described, with emphasis on topics needing great improvement or omitted in present
models.  These include emissions data, detailed acid rain  chemistry, cloud proces-
ses,  dry deposition,  model validation, and sensitivity analysis.
17.
                               KEY WORDS AND DOCUMENT ANALYSIS
                  DESCRIPTORS
                                             b-IDENTIFIERS/OPEN ENDED TERMS
                                             COSATI Field/Group
13. r,.5Ta.iaunc\ STATEMENT
RELEASE TO PUBLIC
EPA . arm 2220 ' (9-73)
                                              19. SECURITY CL.ASS / fins Report)
                                                 UNCLASSIFIED
                                           21. .MO. OP PAGES
                120. SECURITY CLASS /This page I

                    UNCLASSIFIED
                                                                        22. PRICE

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