PA-650/3-73-002
ecember 1973
Ecological  Research Series



vXvX//X;XvXvXyX;X;>XvXvX;X

vX'X'X'X'X'X'XvX'X'X'X'X'X-X'X'X'X'X'X'X'XvX'X'X'X-;



                                                                           >i'X'Xv!*!*!*""!"~"~"~*"
                                                  :;:!:!$;:•   I
                                                  in   \


                                                   WS8&                   llflllllt
                                                   iii^^^^^^^^^^^^^iiwiiiisliii:!^
                   .V.'.V-V

-------
                                 EPA-650/3-73-002
           DETERMINATION
         OF  THE  FORMATION
MECHANISMS AND  COMPOSITION
 OF  PHOTOCHEMICAL AEROSOLS
                    by

           W. C. Kocmond, D. B. Kittelson,
           J. Y. Yang and K. L. Demerjian

               Calspan Corporation
                 P.O. Box 235
               4455 Genesee Street
             Buffalo, New York 14221
             Contract No. 68-02-0557
            Program Element No. 1A1008
               ROAP No. 21AKB-02
         EPA Project Officer: Marijon Bufalini

          Chemistry and Physics Laboratory
         National Environmental Research Center
       Research Triangle Park, North Carolina 27711
                 Prepared for

        OFFICE OF RESEARCH AND DEVELOPMENT
       U.S. ENVIRONMENTAL PROTECTION AGENCY
             WASHINGTON, B.C.  20460

                December 1973

-------
This report has been reviewed by the Environmental Protection Agency and




approved for publication. Approval does not signify that the contents




necessarily reflect the views and policies of the Agency, nor does




mention of  trade names or commercial products constitute endorsement




or recommendation for use.

-------
                            TABLE OF CONTENTS
Section                                                              Page Nc
   I.       INTRODUCTION .....................................      1
   II.       DESCRIPTION OF EXPERIMENTAL FACILITIES .......      3
            A.  The Calspan Chamber ............................      3
            B.  The University of Minnesota Smog Chamber ........      9
  III.       CHAMBER CHARACTERIZATION TESTS  - CALSPAN
            SMOG CHAMBER ....................................     19
            A.  Background Reactivity ...........................     19
            B.  Chamber  Light Intensity Studies ...................     21
  IV.       RESULTS AND DISCUSSION . .........................     2 3
            A.  Summary Experiments - Joint Workshop at Calspan
               March 1973 ......................................     23
            B.  Summary of Experiments  - University  of Minnesota. .     3 S
            C.  General  Behavior of the SO , -Moist Air System ......     if)
            D.  A General Correlation ............................     SB
            E.  Observed Rates of Photooxidation of Sulfur Dioxide . .     S9
            F.  The Propylene-NO  System .......................     62
            G.  Chamber Effects on Aerosol  Behavior ..............     71
                1 .  Coagulation Experiments ......................     72
                2.  Linear Aerosol  Volumetric Growth Curves ......     93
                3.  Chamber Reactivity Tests .....................     97
   V.        SUMMARY AND CONCLUSIONS .......................     99
            REFERENCES .......................................   101
                                    111

-------
                               LIST OF TABLES


Table No.                                                            Page N.

     I      Dimensions of Teflon Reactant Contaminant Bags ........   11

    II      Measured Ultraviolet Radiation Intensity on Chamber
            Centerline for  Various  Numbers of Lamps ......... 0 . . . .   15

   III      Calibration Constants for Whitby Aerosol Analy/.er
            and Data Analysis Format .............................   17

    IV      Summary of Photooxidation Experiments Performed
            During Calspan/U. of M. Workshop - March 1973 . . . „ . „ . „   ZS
     V      Summary of SO ,  Photooxidation Experiments -
            University of Minnesota. . . ...................... ......   37

    VI      Summary of NO -Propylene Photooxidation. Expo r iments . .   64

   VII      Coagulation Rate Constants for U. of M.  Runs ...........   73

  VIII      Coagulation Rate Constants for Several Experiments
            Performed in Calspan Chamber ....................... „   74

    IX      Experiments to  Determine the  Length of  the Linear
            Volume Production Period ...................... „ ......   96

    X      Chamber Reactivity Experiments ..................... „ .  98
                                     IV

-------
                              LIST OF FIGURES
Figure No.                                                         Page No.
      1      Inside View of Calspan's 600 m  Photochemical
            Aerosol Chamber	    5
      2      Inside View of Top Area of Calspan's 600 m  Photo-
            chemical Aerosol Chamber	. .     6
      5      View of Air Circulation System Containing  Ductwork
            and Charcoal Filtering Beds	°	 .     7
      4      Schematic Diagram of the University of Minnesota
            Photochemical Reaction Chamber and Related
            Facilities.	    10
      5      Interior View of Lighting System with Bag Fully
            Inflated	   12
      6      Interior View of Lighting System Showing Collapsed
            Large Bag	......    12
      7      Schematics of the Whitby Aerosol Analyzer	   IS
      8      Effect of Charcoal Filtering  on Photochemical Aerosol
            Formation  in Rural Air	   20
      9      SO , Aerosol Deca y Experiment	   26
     1 0      SO , Aerosol Growth Experiment	   26
     1 1      SO } Aerosol Growth and De cay Expe riment	 .   27
     12     SO , Aerosol Background and Growth Experiment	 •   2
   I1} 21
               ,
     1 3      SO , Aerosol Growth Experiment	   28
   14, 15    SO , Aerosol Growth and Decay Experiment .............   28, 29
     16      SO , Aerosol Decay	   29
     17      SO , Aerosol Growth	 .   50
     18     SO , Aerosol Decay With and Without Stirring	   50
     19     SO , Aerosol Growth in Particle Free Clean Air	   51
           Aerosol Growth in theNO2 Propylene-Clean Air System. .•
   22,23   SO , Aerosol Growth Expe rime nt	   52,
     24     SO  Aerosol Growth After  Chamber Wash	   55
     2 5     SO , Aerosol Growth and Decay Experiment . „	   54
     26     Aerosol Development with  Time for Run  54	   58
     27     Aerosol Development with  Time for Run  5 5  	   59

-------
                           List of Figures  (Cont'cl)
Figure  No.                                                              Page No.
    28       Aerosol Development with Time for Run 36 ..............    39
    29       Aerosol Development with Time for Run 40 ..............    40
    30       Aerosol Development with Time for Run 41 ..............    40
    51       Aerosol Development with Time for Run 42 ..............    41
    52       Aerosol Development with Time for Run 43 ..............    41
    5 5       Aerosol Development with Time for Run 47 ..............    42
    54       Aerosol Development with Time for Run 48 ............ „ .    42
    55       Aerosol Development with Time for Run 49 ..............    45
    56       Aerosol Development with Time for Run 50 ..............    45
    57       Aerosol Development with Time for Run SI ........... , . ,    44
    58       Aerosol Development with Time for Run 52 ..............    44
    59       Aerosol Development with Time for Run 55 .......... . . . .    45
    40       Aerosol Development with Time for Run 54 ..............    45
    41       Aerosol Development with Time for Run 5^ . . „ . . . . „ .  . . 0 . .    46
    42       Aerosol Development with Time for Run 56 ..............     4(>
    45       Ae rosol Development with Time for Run 57 ..............    47
    44       Aerosol Development with Time for Run 58 . . „ ......  .....    47
    45       Aerosol Development with Time for Run 59 ..............    48
    46       Aerosol Development with Time for Run 60 .........  „ . . . .    48
    47       Aerosol Development with Time for Run 61 ........ ......    49
    48       Aerosol Development with Time for Run (> 2 ............. „    4 ')
    4<»       Ae rosol Development with Time for Run h 5 ..............    50
    50       .Aerosol Development with Time for Run f>4 ..............    50
    51       Ae rosol Development w ith Time for Run b 5 ..............    51
    52       Time Histories of Number Concentration for Four
             Different Particle Sixes Observed with the Aerosol
             Analyser (Run 15) .............. „ .................. ....     55
   55,54     Percentage of Volume Accounted for by Particles
             Smaller than the Diameter  D    vs D .   . . . „ „ . . ....... . . .    56
                                          V O     V Cj
             Variation of the Apparent Equilibrium Surface  Area With
             Volumetric Conversion Rate. „ ....................... „ . .    58
                                       VI

-------
                           List of Figures  (Cont'd)

Figure No.                                                           Page No.
    56       SO, Photooxidation Rate vs Relative Humidity	   61
    57       Normalized Volumetric Conversion Rate vs Relative
             Humidity	   63
    58       NO and NO , Concentration with Time for Run 65	   65
    59       NO and NO , Concentration with Time for Run 67	   65
    60       Aerosol Development with Time for  Run 65	  66
    61       Aerosol Development with Time for  Run 67	„	  66
    62       AV/A log D vs D    	  68
   63,64     Experimental fk Modeled Results for the Propylene-NO
             System	* . . .  70
    65       Aerosol Coagulation - U. of M. Run 49	„  75
    66       Ac- rosol Coagulation - U. of M. Run 50	  75
    67       Aerosol Coagulation - U. of M. Run 51	0 0  76
    68       Aerosol Coagulation - U. of M. Run 52	  76
    69       Aerosol Coagulation - U. of M. Run 55	 .  77
    70       Aerosol Coagulation - U. of M. Run 56	  77
    71       Aerosol Coagulation - U. of M. Run 57	  78
    72       Aerosol Coagulation - U. of M. Run 59	  78
    73       Aerosol Coagulation - U. of M . Run 60	  79
    74       Aerosol Coagulation - U. of M. Run 61	  79
    75       Ae ros o 1 Coagulation - U . of M . Run 62	  80
    76       A e ro sol Coagulation - U. of M. Run 6 3	  80
    77       Aerosol Coagulation - U. of M. Run 64	  81
             A e rosol Coagulation - U. of M . Run 65	  81
             Aerosol Coagulation - U. of M. Run 66	  82
             Aerosol Coagulation SO ,-Air System without Stirring -
             Calspan	„	„	  82
   81,82     Aerosol Coagulation SO >- Air System without Stirring -
             Calspan	. .	  83
   83,84     Aerosol Coagulation SO,-Air System With Stirring -
             Calspan	„	  84
                                     VII

-------
                               List of Figures (Cont'd)


P^igure No.                                                            Page No.


   85       Aerosol Coagulation SO ,-Air System Without
            Stirring - Calspan	   85

   8b       Effect of Stirring on Coagulation  in SO ^  Aerosol
            Decay - Calspan	„	„   85

   87       Aerosol Coagulation SO, System  With and Without
            Stirring - Calspan	   86

   HH       Aerosol Coagulation SO , - Air  System - Calspan	   86

   89       Aerosol Coagulation NO ,-Propylene System With
            Stirring - Calspan	   87

   90       Aerosol Coagulation SO ,- Air System With Stirring -
            Calspan	0	„	   87

   C,H       Aerosol Coagulation NO ,-P ropylene System With
            Stirring - Calspan	^	.....„.„	   88

   9<-'       Aerosol Coagulation SO,-Air System With Stirring -
            Calspan	 „	„ . „	.    88

   '' •)       Ae ros ol Coagulation SO _, - A ir System -  Calspan .,...,...   89

   l,'4       Aerosol Coagulation SO ,-Air System Without Stirring -
            Calspan.....	   89

   ''5       Aerosol Coagulation SO ,-Air System -  Calspan	„ .   90

   ')(>       Aerosol Coagulation SO-, System  With and Without
            Stirring	„..,.,   90

   ()7       Theoretical Volume  Production Curves With and
            Without Wall  Losses	„	   95
                                     Vlll

-------
I.      INTRODUCTION

       One of the most difficult problem areas relating to the degradation
of air quality involves the control of chemical pollutants arising from
non-stationary transportation sources.    The goal for  setting and attain-
ment of national primary air standards has been set forth in the Clean
Air Act of 1970.  The lack  of complete understanding of atmospheric
interactions of a complex variety of air contaminants and physical para-
meters,  however,  has seriously hampered progress in achieving the
desired objectives.  Such difficulties are evidenced by  the series of
extensions and delays which have occurred in the regional implementa-
tion plans as well as in the proposed reconsideration of selected air
pollutant limits.   Both the  federal regulatory agencies and the concerned
industries are cognizant of the need for continuing  improvement in the
understanding  of fundamental  chemical and physical interactions relevant
to the variations of ambient air quality.

       The Calspan-University of Minnesota study for  the determination of
the formation  mechanisms  and composition of photochemical  aerosols  repre-
sents one aspect of a broad range program jointly sponsored  by the Office
of Air Programs,  U_ S.  Environmental Protection Agency and the Coordinating
Research Council of the  U.  S.  vehicle manufacturing arid petroleum industries.
This  report presents an  interim  account  of project accomplishments during
the first  year of program performance.

       The objective of the Calspan-Unive rsity  of Minne sola  study is to
elucidate the complex physical and chemical  processes contributing to the
production of photochemical aerosols in polluted atmospheres.  Even though
major advances in the knowledge of homogeneous gas phase reactions
involved in the- formation of photochemical smog have  been gained during
recent years,  the important chemical and physical characteristics govern-
ing gas to  particle conversions remain largely unresolved.  Laboratory
experiments have invariably been confronted with physical constraints present
in reaction chambers designed more specifically for investigating homogeneous

-------
gas phase  processes.  One of the main goals  of this program, therefore, is
to establish  suitable experimental facilities for simulating aerosol formation
processes in the atmosphere.

        The ZO,800  ft  Calspan  smog chamber represents the largest photo-
chemical reaction vessel currently available  in the United States.   As part
of this program,  we are systematically evaluating the performance of this
chamber,  as well as the behavior  of aerosols  in vessels of widely different
surface -to-volume  ratio.

        Preliminary test results suggest that  the Calspan chamber  provides
a reasonably long working time of greater than 11 hours for  aerosol examina-
tion free of significant wall effects.  The 600 ft  University  of Minnesota
chamber,  in which  both temperature and  relative humidity can  be  controlled,
gives reproducible  results for periods  of time in excess of six  hours.

        Descriptions of experimental facilities design and implementation
are given in  Section II of this report.  Experimental test systems  and cham-
ber characterisation results are presented in  Section III.  Data analysis
methodology and preliminary results are described in Section IV.   At both
Calspan and  the University of Minnesota, attempts  have been made to
characterise aerosol behavior under varying  environmental  conditions  rather
than examine aerosol formation and dynamics in highly specific reaction
systems.  The capability for close simulation of various atmospheric para-
meters within the chambers is  expected to be  developed during subsequent
years.

-------
II.      DESCRIPTION OF EXPERIMENTAL FACILITIES

        A.  The Calspan Chamber

            The main facility used at Calspan for investigations of photo-
chemical aerosols is the  Z0,800 ft  smog chamber  located near Ashford,
New York.  The chamber, shown in Figures 1 and 2, is 30  feet in diameter
and  30  feet high and is constructed  of 0. 5 inch thick steel walls. Considerable
effort during  the project year was devoted to preparing the  chamber for
photolysis experiments.  The most important modifications included pre-
paration and resurfacing  of the inner chamber walls, design and fabrication
of an efficient air filtration system, installation of  lighting  sources, and
acquisition of  gas analysis instrumentation.  These improvements to the
chamber  design are briefly described below.

            •  Wall resurfacing --  Special attention was given to the testing
and  selection of a wall surface material that was  of lo\\ surface energy and
resistent lu chemical attack.   Several steel  panels were c oated with candidate
mate-rials and placed within a teflon bag where they were irradiated with
light from a 200-watt Hg-arc lamp.   The  materials were also tested for
resistance  to various acids and gases,  as  well as contaminant adhesion  to
surfaces.   Among the materials tested, a  specially formulated  fluoro-epoxy
polymer developed  at the Naval Research Laboratory, Washington, D,  C.,
gave the best results in terms of chemical resistivity,  high reflectivity  and
low  nucleus production when irradiated with ultraviolet light.

               These tests were sufficiently encouraging to warrant prepara-
tion  of a SO m test section of the- chamber.  Scientists from  NRL visited
Calspan to  participate in  the experiments in order to determine if surface
adhesion  was adequate, as well as to establish mixing procedures for pre-
paring large quantities of the special epoxy polymer.  The tests showed that
good adhesion could be expected if the epoxy was  applied to an alurninized
polyurethane   base within 12 hours  after application of the base material.
This procedure was adopted when the entire  chamber surface was later
coated in  mid-winter 197 Z.

-------
            Although this  surface coating was chosen for use in the Calspan
 chamber, only research grade samples of the materials have been produced
 so far.  For this  reason availability of the epoxy is extremely limited and
 the costs are very high.

            •  Chamber Lighting --  Lighting within the chamber is provided
from  a combination of daylight and fluorescent lights installed  inside Z4
lighting modules and arranged in 8 vertical channels attached to the wall
of the  chamber (sec1 Figures 1 and i] .  Each module contains two ^15-watt
F<)(> PG17/D daylight lamps  and  two 8S-watt P7ZT12HO  blacklists.  The
modules are  covered with heat-treated glass  (transparent to most wave-
                          o
lengths greater than 3300A) that is air tight for the purposes of cooling
the lamps during operation.  Although 14.4 kw of power is used to operated
the lamps,  tests show (sec' Section IV, chamber characterisation tests) that
somewhat higher Light intensities would be desirable for certain types  of
photochemical experiments,  particularly those involving the dissociation of
NO,.   At the  present time the lighting configuration is  being altered so that
each of the  £4 module's will  contain two ZlS-watt fluorescent daylight  lamps,
right  8S-watt high output blacklights and two 40-watt W es tinghousc rapid
start  fluorescent sunlamps.  The heat-treated glass is also being replaced
by 1/-1" annealed pyrex panels in order to achieve greater transparency to
light in the Z'^50 to 5 300A wavelength   region.  These modifications will
result  in  a  calculated  increase of k  from  our present 0.04 min   to  ~ 0 . Z •$
  .  -1
m in

            •  Air Purification —  Most photolysis  experiments are performed
by  first purifying  the test air and then introducing known concentrations of
contaminants into the  chamber.  An alternate  procedure  is to use bottled
gases  for the test environment followed by introduction ot the pollutant gases.
For the large chamber the later  procedure is  impractical so special pro-
visions have been made to achieve adequate air purity through filtration
methods.   Particle removal  (total concentration less than 100 nuclei  cm   )
is achieved through the'  use: of two separate1 banks of absolute fillers.  Special
ductwork (see Figure1  5) has  been built into the' system to allow continuous

-------
      , ' *.-' t ,  ">%!;-*
Figure 1  INSIDE VIEW OF CALSPAN'S 590 cm3 PHOTOCHEMICAL AEROSOL CHAMBER

-------
'S 6°°

-------
Figure 3  VIEW OF AIR CIRCULATION SYSTEM CONTAINING DUCTWORK AND
       CHARCOAL FILTERING BEDS

-------
reeireulation of the chamber air  through the purification filters.  Trace
gaseous contaminants in the rural atmosphere are  removed by activated
charcoal beds that are placed just behind the absolute filters.  Experiments
to date indicate  that removal of most gaseous contaminants and nearly all
particulate matter can be achieved in approximately eight to ten hours of
filtration.

            •  Instrumentation --  In addition to the aforementioned modifi-
cations to the chamber itself, gas and particle analysis equipment has
recently been incorporated into the facility.  Equipment used to monitor
gaseous contaminants within  the chamber  include the1 following:

            (1)   Bendix Model 800Z O/.one  Analy/.cr  -- This instrument  is
based  on the principle of photometric detection of c hemiluminescence result-
ing from the reaction of o/.one with ethylene.  The  minimum detectable
sensitivity  is 0.001 ppm.

            (<^)   Bendix Model 8101-B Nitrogen Oxides Analy/.er --  Detection
is based on c he mi luminescent reaction between nitric oxide and o/.one.   The
detection limit for each of the nitrogen oxides is  O.OOS ppm.

            ( i)   Bendix Model 8iOO Sulfur  Analy/.er  --  Operation of this
instrument is based on the  photometric detection of sulfur  atoms excited in
a hyd rogen-rich flame.  A  set of filters is used for selective monitoring of
sulfur  dioxide and hydrogen sulfide.  The  minimum detectable sensitivity
is 0. OOS ppm.

            (4)   Hewlett-Packard Model S7SO Gas Chromatogra ph --   The
i liromatog raph is equipped with dual column and  dual flame ioni/.ation
detectors.  Depending on the column in use,  either  total hydrocarbon or
individual components can be  analy/.ed.  Detection  limits of 0.01 ppm are
routinely at hievable.

            In addition to the gas analy/.ers,  a thermal diffusion c loud cham-
ber is  used to measure the concentration of large nuclei exceeding approxi-

-------
 mately  O.OS uin radius.     The thermal diffusion chamber provides a
measure ot the activity of the aerosol in terms  of ha/,e forming nuclei
which grow to at least 1 iim diameter near  saturation.   Two Gardner small
particle detectors are also available for measuring total particle  concen-
tration in the chamber.  These instruments provide a  measure of the con-
centration of all  particles greater than about 0.0025 um diameter with a
range of sensitivity of 200 to 10  particles  cm

             For most of  the SO ,  photooxiclation experiments c onducted on
 this  program, an improved version of the  Whitby Aerosol  Analyser  was
 used to obtain si/.e distribution data.   (A description of this apparatus is
 given in the  next section.)  In addition to these instruments., an integrating
 nephelometer was recently  acquired for snaking visibility measurements
 within the test environment„

             Tin1 a fore-mentioned chamber modifications were  completed
 during December 1972 and early  January 197 J.   Since  that  time' tests have'
 been conducted to  establish chamber background reactivity and later a
 complete set of  SO , photooxiclation  experiments were  performed  as  part of
 the  joint Ca Ispa n-Univer si ty of Minnesota  workshop.   Results of  these tests
 are described in Seclions IV and V.

         B.  The-  University of Minnesota Smog Chamber

             The main features of this c hamber have1 been described  previously
 by Clark (1972).  Figure'  4 shows the- essential  elements of the chamber and
 some of the  associated apparatus.   The reactants are  contained in either  a
 f/)2tS ft   or a 90 ft   bag,  both of which are  of cylindrical shape and arc' fabri-
 cated from  0.01 in Dupont FEF Teflon  film.  Their dimensions are  shown
 in Table' I.

-------
                                    u
                                   LLI
                                   X
                                   o
                                   o
                                   H
                                   o
                                   X
                                   a.
                                   Ui
                                   2


                                   «E
                                   u. uj
                                   O P

                                   > -J

                                   t 5
                                   ~ UJ
                                   UJ
                                      UJ
                                   1 cr

                                   s|
                                   itr
                                      <
                                   Q X
                                   X
                                   a
                                   •<*•
                                    a>
                                    en
                                   iZ
10

-------
                                Table I
           Dimensions of Teflon Reactant Contaminant  Bags
                   Large Bags             Small Bags
   Diameter             10.0 ft                  3. 8 ft
   Height                8.0 ft                   6. 5 ft

                                                        -1
Volume             625.0 ft3                 90 ft3
   Surface/Volume      0.65ft"1                1.47ft

Flexible' bags were used in order to eliminate the necessity of adding air to
make' up for the sample removed by the analysis instruments.  The concen-
trations of the reactants in the chamber were consequently not altered  due
to sampling.  This allowed less  ambiguous interpretation of the results.
Inflated and collapsed large bags are shown in Figures 5 and 6.   Teflon was
chosen  because of its low surface energy, chemical inertness, and trans-
parency to light in the UV range. The bags were supported in the  center of
the illumination system and air was circulated around them to maintain
nearly isothermal conditions.

            • Chamber Lighting --  The illumination system  consists of 72
General Electric  F40BL fluorescent  lamps mounted in  pairs  on  36  evenly
spa cod  vertical supports.  The  supports  formed a 7. 7 ft  diameter  cylindrical
enclosure around the Teflon bags as  shown in Figures 5 and 6.  Aluminum
foil was attached  behind the lamps  to increase the uniformity  and intensity
of the light.   The lamps are wired  so that they could be turned on in  groups
of 18.  This allows the effect of light intensity to be explored.

            The spectral intensity distribution of F40 BL in the  2900 to
3400A light range believed to  be important in the photooxidation of  NC>2 is
similar to that of sunlight.  A chemical actinometer  utilizing  the photo-
isomerization of O-nitrobenzaldehyde to  O-nitrobenzoic acid was used  to
measure light intensities in the  3000 to 4000A region.  This method has been
described in detail by Gordon (1967).  The results of the  measurements are
                                     11

-------
Figure 5  INTERIOR VIEW OF LIGHTING SYSTEM WITH BAG FULLY INFLATED
                                       >»•:
    Figure 6  INTERIOR VIEW OF LIGHTING SYSTEM SHOWING COLLAPSED
           LARGE BAG

                               12

-------
given in Table II.  Intensity values were converted to watts /m" assuming
                                                     o
that the energy was centered at a wavelength of 3500A.  With all lights turned
on the centerline light intensity was  4. 55 x 10   photons/cm  sec.  This
compared with 12.95 x 10   obtained  by  the same method for noon day sun
in mid-August.  The University of Minnesota chamber light intensity is thus
computed to be about 35% of the intensity of natural sunlight.   The light
intensity was also determined  as  a function of radial distance from the
chamber centerline, and was  found to increase gradually such that near  the
walls it was about 1.6 times centerline intensity.
                                  TABLE II
                             (From Clark  1972)
           Measured Ultraviolet  Radiation Intensity  on Chamber
                 Centerline  for  Various  Numbers  of Lamps
                                   Photons     Watts
No.




of Lamps
18
36
48
72

0
2
3
4
CTn<- sec
.93xl015
. 22xl015
.46x1015
. 55xl015
~~in2
5.28
12.6
19.6
25.8
            •  Air Purification System --  The purification system in the
University of Minnes ota's chambers consisted of a 1Z in  x 1Z in absolute
particle  filter,  an activated charcoal scrubber, silica  gel dryer,  humidifier,
and a single  sheet of 8 in x 10 in MSA filter paper which  acted as a final
filter.  Ambient laboratory air  was pumped through the purification system
at approximately 15 cfm.  The gas scrubber  utilized charcoal supplied by
the Barneby  Cheney Co.  and consisted of 1Z Ibs type AC  standard activated
charcoal,  5  Ibs of type CH charcoal treated to remove acid gases, and
6 Ibs  of type CA charcoal treated to remove  ammonia and amines.  At
IS cfm the residence time in the scrubber  is about Z. 84 sec, which is more
than an order of magnitude greater than  that necessary for normal air
                                    13

-------
purification purposes.  After leaving the scrubber, the air may either pass
through the humidification system or through the siLica gel dryer.   In
practice part of the air stream passes through each component and the
humidity of the output air is controlled by blending the two streams.  This
allows the humidity to be varied in the range  10 to  90% relative humidity.
Following  passage through these compartments, a sheet of filter material
is used to  remove any particles introduced  by the scrubbing  or humidification
system.   Air passing through the purification system is  exposed to only
non-reactive  metal,  glass,  and Teflon duct surfaces and the chance of con-
tamination is minimized.

            •  Instrumentation

               (1)  Whitby Aerosol Analyzer
                A  Whitby Aerosol  Analyzer was  used to measure the size dis-
tribution of the photochemical aerosol in the  diameter range 0.004 to 0.4 (im.
The' instrument is a modified version of the Model 3000  Whitby Aerosol
Analyzer described  in detail by Whitby et al (1972).  The unit shown in
Figure 7 consists of a sonic jet,  unipolar diffusion charger, a mobility
analyzer,  and associated electronic and flow components.  Aerosol enters
the instrument at a flow rate of 0. *>i cfm and is charged by rapid mixing
of the particles with negative ions generated  by a corona discharge' in the
charger.  The  aerosol emerges from the charger  carrying a negative charge
and flows  to the electrical mobility analyzer  for analysis.  From the mobility
spectrum  obtained,  the particle size distribution can be inferred.   The opera-
tion of the instrument depends on the fact that the  electrical mobility of a
particle decreases with increasing particle size for particles  smaller than
approximately  1 urn diameter.  In the mobility analyzer, a positive voltage
on the central collection  rod causes all particles with mobilities larger than
a certain critical value to be collected on the rod while those with smaller
mobilities penetrate the precipitating electric field and are collected on an
absolute filter  at the base.  The absolute filter is connected to an electro-
meter which measures the current produced  by discharging the collected
                                      14

-------
                                   3.5 KV (-)
                                                      0-15 KV ( + )
           COMPRESSED
               AIR
UNCHARGED
 AEROSOL
                           MIXING ZONE
                           (AEROSOL & IONS)
                      SIGNAL^

                      1EAD
                      COMMAND

                      EXT. TRIGGER
                                                                               MOBILITY
                                                                              ANALYZER
                                          CURRENT
                                        COLLECTING
                                           FILTER
Figure 7
                      SCHEMATICS OF THE WHITBY AEROSOL ANALYZER

-------
particles.   By measuring the electrometer current as a function of voltage
on the collection rod, the mobility spectrum and the size distribution of
the aerosol can be obtained.  Rod voltages are changed in steps in the range
0 to 13,300 V.  The first voltage step of 65.7 V corresponds to a  nominal
particle  diameter of 0.004 um while the last voltage step of H, 300 V corres-
ponds to 0.4 um.  A total of 18 voltage  steps are sequentially applied to
obtain particle size distribution.  After each step,  from  15 to 40  seconds
are required  for the electrometer current to reach a new steady state value.
Consequently, the total sampling  time necessary to obtain a complete  particle
size distribution is  about six minutes.  Calibration of the instrument has
been performed using artificially generated aerosols and has been described
 by Whitby et  al (197Z).   The resulting calibration constants and the procedure
 for obtaining number surface- and volume distributions arc1 given  in  Table III.

               Si/.e distributions  are obtained by measuring current as a
 function of rod voltage  and differentiating the- resulting data.  Aerosols
 generated in  smog  chambers are often rapidly growing or decaying.  Under
 such circumstances, the current at each rod voltage will be rapidly changing.
 Since up to 40 seconds  pass between current readings, Al values may be
 distorted.  In ortler to  avoid such distortions, current versus  time  data are
 plotted for each collector  rod voltage' and current values at any given time
 are obtained  by interpolation.  Considerable effort lias been expended in
 developing evaluation processes whereby this interpolation is performed
 automatically using a computer.  So far, however, manual plotting  and
 interpolation of the curves has proved  to be1 the  most  reliable.

            (2) Condensation Nuclei Counter
                A General Electric  Condensation Nuclei  Counter  (CNC) was
 used to  measure total particle concentrations.   All particles larger than
 about O.OOZ |j.m should  be  detected.   Details of the instrument  have  been
 given by Skala (1963).  It has a range' of sensitivity from about 50  to 10
 partii le's/cm  .  For this study the instrument was used  primarily on the
 100,000  particles/cm   scale.  This scale was calibrated as described  by
                                     16

-------
_QJ


 CD
CO
e
> n-s
3.

z —
5 "g
 1
cH


a E
Q =L,





CO 00
o o
X X
co en

t- CN in




CO CO CO
o o o
XXX
in «t r-
in o •-
CM «t r^







0 O
CD *t «-
CN co in
r- 0 0
b b o













o o o
in o in
in CM ro
CM CO Tf
in a> co
co in r*
CM CO 'J
000
o o o

O CO CO
CM O CO
co ^j- in
0 O O
o o o





     o
                                                                                                                                                        co    >
                                                                                                                                            Z    to    ">    >
                                                                                                                                            <3   
-------
Clark (1972).   If concentrations greater than 100K were  encountered, diluters
were used in the sampling line.  They could be used to give 594,000 or  1. 5
x 10 particles/cm  full scale deflection.  The diluters have been described
by Whitby et al (1972).

            (3)  Gas Analysis
                The following instruments have  been used for gas analysis:
Scientific Industries Model 65-8 SO-, analyzer, Meloy Model SA160-2 flame
photometric total sulfur analyzer,  Bendix Model 8101-B NO-NO2-NO
analy/.er,  REM model 612B chemiluminescent ozone analyzer, a Hewlett-
Packard Model 5700 gas chromatograph for CO  and methane and non-methane
hydrocarbons, and a Cambridge Instrument model 880 dew point hygrometer
for humidity measurement.

            •  Operation Procedures  - University of Minnesota  -- Before
each experiment, the Teflon bag was filled  and emptied three times  to
remove- gaseous and particulate residue from the previous experiment.
The bag was then filled in the dark at a flow rate of about 15 cfm.  When
the bag was about three-quarters full, a known volume of SO , (or NO and
C.H/)  was injected through a Teflon sleeve  on the  input line- using a  glass
syringe-.   The  filling was  then continued until the bag was full.  In cases
where  the bag humidity was to be oilier than ambient, the humidification
system was adjusted to give the correct humidity during the last filling
process.   After the bag was fully inflated, the lights were turned on and
aerosol formation and growth were  monitored.
            The CNC was visually run on its most sensitive  range (
particles /cm  full scale) until the aerosol started to grow.   It was then
switched to the 100K range and the appropriate diluters were added.  In
order  to avoid serious material  depletion in the bag,  samples  were only
taken for analysis intermittently.  This was particularly important in the;
experiments performed  in small bags because of  the- relatively small quantity
of air  contained in the bag.  Sample requirements for the E-l condensation
nucleus monitor during continuous operation were 3 1/min and for the WAA
approximately 5 1/min.
                                     18

-------
III.     CHAMBER CHARACTERIZATION TESTS - CALSPAN SMOG CHAMBER

        A.  Background Reactivity

            In most  photochemical aerosol studies,  the  usual test procedure-
is to  first purify the sample air and then introduce known concentrations of
pollutants into the chamber.  The sample is then irradiated while observa-
tions  are made of aerosol formation, particle si/.c distributions  and gaseous
behavior (SO-,,  NO  , oxidant).  Achieving adequate air purity prior to the
start  of an experiment is essential since even trace amounts of gaseous
contaminants can lead to unwanted chemical reactions and the formation of
substantial aerosoL

            Initial tests  were performed in the Calspan  chamber to determine
if the reactivity of the fluorinated epoxy chamber surface coating was  satis-
factorily low and to  establish if the efficiency of the air filtration systems
was sufficient to remove trace  contaminants.  Concern  centered around the
possibility that slight out gas sing  of the1 chamber surface could lead to  con-
tamination of chamber air and  interference with test results.

            Experiments were  designed to examine particle production within
the chamber after first purifying the  test air for varying lengths of time by
filtration with absolute and activated  charcoal filters.  In a  typical sequence,
filtration was continued  until the  measured chamber air particle concentration
                                  _ 3
was stabli/.ed to le s s than ^00 cm  ,  which represents a value comparable
to that  found in most clean rooms.  Normally this condition is achieved
after  six to eight hours of filtration.  Gaseous levels of NO  , SO and
ovidants normally fall below detectable  limits after  four hours of charcoal
filtration.  After purification,  the air is irradiated while  particle concen-
tration  and gaseous  contaminant levels are monitored.

            Results  of several  experiments are plotted in Figure 80  The
figure shows  particle concentration as a function of time for several test
configurations.  It is obvious from  these results that without charcoal
filtration gas-to-particle conversion  begins almost immediately  once
                                     19

-------
                                        -j	T     I   	n
                                     PARTICLE FREE RURAL AIR, WITHOUT STIRRING
                                     PARTICLE FREE RURAL AIR. WITH STIRRING
                                     CHARCOAL FILTERED AIR, WITHOUT STIRRING
                                     CHARCOAL FILTERED AIR, WITH STIRRING
                                     CHARCOAL FILTERED AIR, WITHOUT STIRRING
                            50     75    100    125
                            PHOTOLYSIS TIME, minutes
                                                  150
175
        Figure 8  EFFECT OF CHARCOAL FILTERING ON PHOTOCHEMICAL AEROSOL
                 FORMATION IN RURAL AIR
irradiations arc  started.   On the- other hand,  the use of both absolute and
charcoal filters effectively eliminates  photochemical production of nuclei.
The  relatively  high particle  concentration observed  in the December  197
-------
        B.  Chamber Light Intensity Studies

            As part of the chamber characterization tests, experiments were

performed to  determine the light intensity levels within the chamber.  Two

types of experiments were performed:  photometric measurements  using  a

radiometer and NO -, photolysis.


            •  Radiometer Measurements --  A  specially designed radiometer

and filter  holder system were used to measure both the1 solar and integrated

light  intensity within the Calspan chamber.  The light intensity within the

test chamber  was compared  to the solar radiation measured  on a clear,

winter day at  the test site.  The  results show that the intensity within the
                                              •t
test chamber  is on the average a factor of 10 less than that measured on

the outside,,

                        !
                        »
            The photo flux comparisons we're made using a radiometer which

consisted  of a detector, two  orfi
-------
            These data showed that the light flux through a given volume at
the center of the chamber is between 5 and 12 times lower than would be
experienced by  a similar volume exposed to solar radiation on a clear day.
The results were  rechecked and verified later in the program using a radio-
meter of improved design.  NO-,  photolysis methods (described below) were
also used as a measure of light intensity in the chamber.

            • Light Intensity Measurement by NO , Photolysis --  The
available  NO^-active light intensity within the Calspan chamber was monitored
by measuring the  rate constant, k ,, for NO-, photolysis in nitrogen.  A heat-
sealed Teflon FEP Type C film (3 mil thick) bag of about 15 ft  volume was
constructed for  the desired  actinometry measurements.  An inlet tube pro-
vided with a T-type connector was used for reaction sample  preparation.
Prepurified nitrogen was admitted into the bag,  and a measured amount of
nitrogen dioxide was added  with a gas syringe through a septum in the T-
connector  when the bag  was half-filled with nitrogen.  The NO, and NO
concentrations were  monitored through a separate sampling  tube with a
Bendix chemiluminescent oxides  of nitrogen analyzer.

            Actinometric measurements  were made at three different loca-
tions in the chamber: (a) center  of chamber, (b) half-way up adjacent to
the chamber wall,  (c) one-fourth of the way up  in the middle of chamber.
k . computations were made by plotting the logarithmic  decay of NO, as
a function  of irradiation time.  The adjusted values  were derived by correct-
ing for light attenuation by the  Teflon film.  The results of these experiments
support observations made  with the radiometer and  indicate  an average  k
value of 0.053.  This value  represents a light intensity corresponding to
about 10 percent of late  summer noon time solar radiation.

            Because  of  the low light intensity observed in these tests,  plans
were immediately formulated for  increasing the radiation intensity for  future
tests. The design changes  which are currently being implemented in the
large chamber  have been described in Section II of this report.
                                     22

-------
IV.     RESULTS AND DISCUSSION

        In this section the results of both the Calspan and University of
Minnesota chamber experiments are discussed in detail.  Since most of
our effort was directed toward understanding aerosol behavior using the
SO^-air system,  presentation of individual  test data has been combined in
order  to avoid redundancies when describing the general features of aerosol
development.  It should be noted, however, that although the photochemical
production of aerosol was  similar in both chambers, some important differ-
ences  in photooxidation rates, coagulation constants and chamber working
times  did exist and these differences are  treated separately within the text.

        For the most part then,  the acquisition of data  fell under two broad
categories:  (1) the joint Calspan-University of Minnesota Workshop held in
March  1973 and (^) the detailed SO 7 photooxidation studies performed at the
University of Minnesota  throughout most of the year.

        Data  obtained in these experiments are very briefly summarized in
parts A and B of this section and  then discussed in  substantial detail in
subsequent sections.

        A. Summary Experiments -  Joint Workshop at Calspan -  March 197 ;)

            During a two-week period in March 1973,  scientists from the
University of Minnesota  visited Calspan to participate  in experiments in the
ZO, 800 ft  chamber.  This workshop represented our first joint working
experience in the large smog chamber.  The objectives of the study were
(a) to determine the aerosol volume production rates (dv/dt   ) f°r several
different SO,-clean air systems  and  to  relate these observations to an
understanding of possible chamber effects (primarily stirring vs non-stirring
and wall losses),  (b) to examine  aerosol growth and decay for both the SO ,-
air and NO  -propylene systems and (c)  to determine the influence of stirring
on the  coagulation of aerosols in the  chamber.  Primary emphasis was placed
on studying aerosol growth and decay in SO-, systems,  and only three NO-,-
propylene and one  auto exhaust experiment  were conducted.

-------
            • Photochemical Aerosol Experiments -- The instruments used
in the  study were:  a Whitby Aerosol Analyzer (WAA), Rich Model 100 Con-
densation Nuclei Counter, Gardner Small Particle Detector, cloud nucleus
chamber, total  sulpher monitor, oxidant analyzer and oxides of nitrogen
analyzer.  All equipment remained at the test site for two additional weeks
after the workshop in order to test NO -,-propylene systems and also to
examine the  influence of auto exhaust contamination on the test results.  In
a typical experiment the chamber air was  first filtered for eight to ten hours
to remove all particles and trace  gaseous  contaminants.  The  clean air was
then irradiated  for ZO to 30 minutes to determine if any trace contaminants
were present which could lead to the formation of particles.  If no nuclei
were observed, a specific amount of SO-, or other gas was introduced into
the chamber and irradiated for varying lengths of time.  Tests lasted from
a few minutes to over 12 hours.   A total of 27 experiments were performed
during the experimental period.  A summary of the tests  is given in Table  IV,
showing the type of experiment performed (i.e.,  aerosol  growth and decay),
the concentrations of SO-, or other gases used in the experiment,  the aerosol
volume production rate, volume production rate adjusted  for  SO, concentra-
tion,  equilibrium surface concentration, relative humidity, photooxidation
rate, and mode of stirring.  A  computer routine was developed to process
data from the mobility analyzer in order to obtain time histories  of number,
surface and volume concentrations.   These data are shown for each experi-
ment where available in Figures 9 through 25.

            Runs 12,  15 and 18 (Figures 14,  17,  19) represent relatively long
SO-, aerosol  growth studies.  The aerosol  volume vs time  profiles for these
experiments remains linear, within experimental error,  throughout the
irradiation period.  The somewhat high  degree of scatter in the data at
long reaction time periods when particles  are growing into larger size
regions may be accounted for by the  fact that the mobility  analyzer is sus-
ceptible to greater error in these larger particle size regions. If we assume
that one of the measures of the useful operating time of a smog chamber is
the linearity of  the aerosol volume conversion rate in the'SO-,  system,  then
the observations in run 18  (Figure 19) would suggest  an effective operating

                                     24

-------
    DC
    D
    Q

    Q
LU
QC
UJ
a.
to
        CO
        rs
        en
        f—
        I
        o
        QC
    *  O
    CC  I


1-1  x  cc
 
    O  2
    O  |
    Jr  Q-
    O  w
    i  -J
    Qu  <
    U.  O
    O
    >-
    cc
    D
    C/3








































(N
D












COMMENTS*




cc
C/S

0

- [i i. .
9 ccs?;
X
o
X o
cc ^
CO
UJ U
E
a
a
1 -=
•n fO
"I
O "-•
w o
\
UJ
cc
Ul
u a a
Z E sui
O ^- l"~ "
X Q. Q. O
Ul 2
*£
UJ
cc
Z m
z





in
CM
FH (6SI/DECAY
S
0
cc
a
o*
CO

O
Z



00
s


o>
CM

1



0
CO
rv
^


IV
tO
CO
CM






CO
CO
1-



1-







X
cc
a
0
00
X
i
cc
u
cT
to

0
Z



CO
•-


o
CO

o
CM



^
CO
ta-



en
CM






00
to
o



CO



CC

Q
3
CO
FH (651/DECAY
i
cc
o
to

CO
Ul
^>-



CM
CM
CM


O
CO

o
s



o
CO
CM



CM
CM
CO






in
P-



*







o
to
X
1
cc
o
CM
o
to

to
Ul
>-



s
o


o
CO

1



o

CM



o
•-






to
o



CO







X
cc
d
3
CM
X
o
cc
o
CM
O
CO

o
z



IV
o


o
CO

1



0
CO
r-'



CM
IV
d






o
o



o

X
cc

D

1
i-
FH (1301/DECA'
O
CC
U
CM
O
to

o
z



CO
to
o


o
CO

1



0
CO
^



in
d






CO
o



T-






§
i-
PH (3001/DECA'
O
CC
(3
CM

CO
Ul
>-



CO
CO
o


CM
CO

1



CO
CO
d



CO
d






5
o



CM






O
CO
<
-
O
Ul
Q
o"
to
CO
Ul
O
Z


£
•-





in

















Cn
o



«•






>-
FH (3601/DECA
0
CC
O
CM
0
to

to
UJ
^



IV
O





in



01
CO
d



in
d






3
o



in







8
S
Ul
Q
CM
O
CO
O
Z
CO
Ul
>


s
•-





g



CO
in
d



o
in
d






o
01
o



CO







o
S
>
O
Ul
0
(M
O
to
o
z
UJ
>


g
o























CO
o



IV







g
to
X
i
cc
a
CM
O
to

to
UJ
^



CO
in
o





^



o
•3-
d



~
d






CO
CM
O



CO




„
o
CO
X
H
'YLENE GROW
0
CC
a.
+
CM
O

CO
Ul
^










CM
CO









CM
in
d



in 01
•- <-'


X *M
co O
0 Z

en




_
o
en
X
'YLENE GROW
O
CC
a.
+
CM
O
Z

CO
Ul
>•




















o
01
d



in «-
r^ CM


T CM
co 0
u z

o
CM






o
CO
I
o
cc
o
CM
o
CO

CO
Ul
^



8
•-





s



^__
CO
•tt



en
CM






CO
in
d



,-
M



o
in
X
'YLENE GROW
0
CC
a.
+
CM
O
z

to
Ul
>.










0
CM









o
CM




o in
CM r-'


CO
I fM
co O
u z

OM
CM






§
X
O
cc
u
CM
0
to

to
Ul
>.



in
o
'-'





in
CM



ui
in
CM



CO
•^









O
in
•-'























o
CO
o



CO
CM


UJ
I—
cc
Z
o
to
cc
UJ
z
O
(J
u
cc
1-
UJ
OLUM
to
UJ
1-
O
Z
UJ
Q
•D|-O
to
Ul
I-
O
Z
DECAY IS GIVEN IN PARENTHESIS
Q
Z
I
S
O
cc
o
ROSOL
Ul
CC
o
u.
to
UJ
z
2
Z

UJ
i
*











2
0
1-
O
LU
cc
cc
a
to
ENOTE
Q
X
CC
Q









U
O
in
CM

@i
D
CC
>
_J
-J
2
cc
0
z
WERE
CO
H
co
UJ
1-






-------
  24.0
  20.0
  16.0
=*,.
LU
  12.0
O  8.0
   4.0
   3.0
   2.0
 O
 > 1.0
    0L
          16.0
           2.0
             22
          550

          500

          450

          400
       CO
        | 350

        E 300

        £250
200

150

100

 50

  0
                                                            RUN NO. 1, MARCH 18, 1973
                                                            SO2 = 1.33 ppm
                                                            NO STIRRING
                                                            ^= 23.67 /im3/cm3 hr
                                                   O AEROSOL VOLUME CONC. /im3/cm3
                                                   A AEROSOL SURFACE CONC. /* m2/cm3
                                                   D AEROSOL NUMBER CONC.
                                                          LIGHTS OFF AT 66 mm
                                                                                    1800
                                                                                    1600
                                                                                    1400
                                                                                    1200
                                                                                    1000
                                                                                    800
                                                                                     600
                                                                                    400
                                                                                     200
                                                                                          cc
                                                                                          UJ
                                                                                          ffi
                                                                                          D
                                                                                          Z
                     32
                              42
                                      52
                                   TIME (mini
                                               62
                                                       72      82

                        Figure 9  SO2 AEROSOL DECAY EXPERIMENT
                      RUN NO. 3, MARCH 19, 1973
                      SO2 = 0.68 ppm
                      NO STIRRING
                                                                                    1000
                                                                                    800
                                                                                    600
                                                  O AEROSOL VOLUME CONC. ^rr/cm
                                                  A AEROSOL SURFACE CONC. /im2/cm3
                                                  D AEROSOL NUMBER
                                                         LIGHTS ON AT 0 min
                                                         LIGHTS OFF AT 60 mm
                                                                           400
                                                                                     200
                                                                                         cc
                                                                                         UJ
                                                                                         m
                          11
                                 21      31
                                 TIME (min)
                                                41
                                                       51
                                                              61
                        Figure 10  SO2 AEROSOL GROWTH EXPERIMENT

-------
  5.0 r
  4.0 -
E 3.0
LU
5
_i
O
  2.0
  1.0
   0 L
          600
          500
          400
                O  AEROSOL VOLUME CONC.
                0  AEROSOL SURFACE CONC.//m2/cm3
                D  AEROSOL NUMBER
                                                       RUN NO. 4, MARCH 20, 1973
                                                       SO2 = 1.15 ppm
                                                       STIRRING
                                                       dv
                                                                m /cm hr
                                                            LIGHTS ON AT 10
                                                            LIGHTS OFF AT 65
             0  10  20  30 40  50  60 70  80  90  100 110 120 130
                                 TIME (min)
                 Figure 11  SO2 AEROSOL GROWTH AND DECAY EXPERIMENT
                                                                               1000
                                                                               800
                                                                               600
                                                                               400
                                                                               200
                                                                                   UJ
                                                                                   m
                                                                                   3





5.0

4.0
T)
E
u
o
^ 3.0
UJ
5
3
1
O 2.0
^


1.0

0
~

40
"E
o
NE
^ 30
UJ
o
U-
- 5 20
C/3


10

L 0
. 0 AEROSOL VOLUME CONC. ju m3/cm3 . RUN NO. 10. MARCH 22, 1973
A AEROSOL SURFACE CONC.yK m2/cm3 SO2 = 0.40 ppm
n AEROSOL NUMBER NO STIRRING
ANALYZER MALFUNCTION
LIGHTS ON AT 50

LIGHTS OFF AT 70
8

a


0


Q
o :!
Q .
£ A . o . ° 0 ,
S S3 * A A
HA







400



300 m
X
X
200 m
g
3
Z
100

n
                  12
                         22
                                            52
                                                   62
                                                          72
                                                                82
                                32     42
                                 TIME (mm)
              Figure 12  SO2 AEROSOL BACKGROUND AND GROWTH EXPERIMENT

-------
  0.80 r
E
4.
UJ
5
O
0.40
              82
                                                   O AEROSOL VOLUME CONC. //m3/cm3
                                                   A AEROSOL SURFACE CONC. jUm2/cm3
                                                   D AEROSOL NUMBER
                                                              LIGHTS ON AT 72 mm
                                                              LIGHTS OFF AT 200 mm
RUN NO. 11, MARCH 22, 1973
SO, = 0.35 ppm
NO STIRRING
-^ = 0.45 yUm3/cm3 hr
                    102
                            122     ^42
                            TIME (mm)
                                         162
                                              182
                          Figure  13  SO2 AEROSOL GROWTH EXPERIMENT
                                                                                      400
                                                                                      300
                                                                                    200
                                                                                      100
                                                                                         CO
                                                                                         5
                                                                                         z
   2.4 r
   2.0
 E 1.6
 u
ro
 54,
 uj 1.2
 5
 D
 S 0.8
   0.4
    0 _
           240
           200
                   O  AEROSOL VOLUME CONC. yt/m3/cm3
                   A  AEROSOL SURFACE CONC. yUm2/cm3
                   D  AEROSOL NUMBER CONC.
                                 LIGHTS ON AT 90 mm
                                 LIGHTS OFF AT 390 mm
                                                         RUN NO. 12, MARCH 23, 1973
                                                         SO2 = 0.44 pm
                                                         STIRRING
                                                           = 0.36 U m3/cm3 hr
              52   92   132   172  212   252   292   332   372   412   452
                                                                                     300
                                                                                     250
                                                                                     200
                                                                                   150
                                                                                     100
                                                                                     50
                                                                                        CO
                                                                                        3
                  Figure 14  SO2 AEROSOL GROWTH AND DECAY EXPERIMENT

-------
   1.4 i-
   1.2
   1.0
   0.8
  N
-  E 160
UJ
5
   06
   0.4
   0.2
    0 L.
          280
           240
          200
           120
            80
           40
                                         3   3
              O AEROSOL VOLUME CONC. jUm /cm
              A AEROSOL SURFACE CONC. /< m2/cm3
              n AEROSOL NUMBER
RUN NO. 13, MARCH 23, 1973
SO, = 0.39 ppm
NO STIRRING
   =  0.27 ,um3/cm3 hr
                                                             LIGHTS ON AT  60
                                                             LIGHTS Off AT 250
             52     72  92 112  132 152 172  192 212 232 252 272 292 312
                                   TIME (mm)
               Figure  15  SO2 AEROSOL  GROWTH AND DECAY EXPERIMENT
                                                                                       300
                                                                                       250
                                                                                       200
                                                                                     CD
                                                                                 150  §
                                                                                     2
                                                                                       100
                                                                                       50
  028
  0.24
  0.20
  014
E
=1
  0.12
O
           140
           120
           100
            80
    LU
    O
h   < 60
    cc
    D
  0.08
  0.04
    0L
         (/>
            40
            20
                                                                          3   3
                                               O AEROSOL VOLUME CONC. JJ.m /cm
                                               A AEROSOL SURFACE CONC. ytim2/cm
                                                 AEROSOL NUMBER
                                                      LIGHTS ON AT 8
                                                      LIGHTS OFF  AT 29
                                                     RUN NO. 14, MARCH 23, 1973
                                                     SO2 = 0.91  ppm
                    12  22  32  42  52  62  72  82  92 102
                                  TIME (mm)
                                                                                       300
                                                                                       200
                                                                                     oc
                                                                                     LLI
                                                                                     CO
                                                                                       100
                                                                                       50
                              Figure 16  SO2 AEROSOL  DECAY

-------
   1.61-    16°
   1.4 -    140
   1.2
   1.0
 I
   0.8
 § 0.6
   0.4
   0.2
                        LIGHTS ON AT 50 min
                        LIGHTS OFF AT 410 min
^ O  AEROSOL VOLUME CONC. ^|m3/cm3
 A  AEROSOL SURFACE CONC. ^im2/cm3
    AEROSOL NUMBER CONC.
           RUN NO. 15, MARCH 25. 1973
           SO2 = 0.38 ppm
           SITRRING
           •^ =  0.15 ,Um3/cm3 hr
                                                                                      200
                                                                                      175
                                                                                      150
                                                                                      125
                                                                                      100
                                                                                      75
                                                                                      50
                                                                                      25
                                           DC
                                           LU
                                           00

                                           Z
              62    102   142   182   222   262   302   342   382  422   462   502
                                            TIME (mm)
                               Figure 17   SO2 AEROSOL GROWTH
  0.32
  0.28
  0.24
  0.20
ui 0.16
  0.12
  0.08
  0.04
          160
                                                                                      400
O  AEROSOL VOLUME CONC. JJm3/cm3
A  AEROSOL SURFACE CONC. am2/cm3
                                                D  AEROSOL NUMBER CONC
                                                             LIGHTS ON AT 20 mm
                                                             LIGHTS OFF AT SO min
                                                          RUN NO. 16, MARCH 26, 1973
                                                          SO- = 0.90 ppm
                                                               0.50A/m~/cm- hr
                           START STIRRING
              36    56    75    96    116   136   156   176
              Figure 18  SO2 AEROSOL DECAY WITH AND WITHOUT STIRRING
                                             30

-------
    1.6
    1.4
    1.2
    1.0
  UJ
  1 0.8
  _i
  O
    0.6
    0.4
    0.2
                                                 O AEROSOL VOLUME CONC. JU m3/cm3
                                                 A AEROSOL SURFACE CONC. JUi m2/cm3
                                                 D AEROSOL NUMBER CONC.
                                                        RUN NO. 18, MARCH 28, 1973
                                                        SO2 = 0.28 ppm
                                                        STIRRING
                                                        -jj* =  0.11 /(m3/cm3 hr

                                                        LIGHTS ON AT 40 min.
                                                        LIGHTS OFF AT 720 min.
               62   122    182   242   302  362   422   482   542   602   662   722
                                           TIME (mm)
              Figure 19  SO2 AEROSOL GROWTH  IN  PARTICLE FREE CLEAN AIR
                                                                                       150
                                                                                        cc
                                                                                        UJ
                                                                                        m
                                                                                      50
   120
100 \-  UJ 0.5
t/i
   80
   60
    40
   20
           0.9
           0.8
           0.7
           0.6
         > 0.4
           0.3
             O  AEROSOL VOLUME CONC. // m3/cm3
             A  AEROSOL SURFACE CONC. (102 ,am2/cm3)
             D  AEROSOL NUMBER CONC. (105/cm3)
                     LIGHTS ON  AT 115 mm
 RUN NO. 19
 3 ppm NO,+1.5 ppm C3Hg
 STIRRING
-j£ = 0.52/X m3/cm3 hr
    o L-     0&
            116   126   136   146   156   166   176   186   196   206
                                                                                    450
                                                                                    400
                                                                                    350
                                                                                    300
                                                                                    250  2
                                                                                      CE
                                                                                      UJ
                                                                                  200  CO
                                                                                      D
                                                                                      Z
                                                                                  150
                                                                                    100
                                                                                    50
       Figure 20  AEROSOL GROWTH  IN THE NO2 PROPYLENE - CLEAN AIR SYSTEM
                                              31

-------
     380
     340
     280
  UJ
  o
  <
  UL
  cc
240
     200
 p>
  'o
  x  160
  oc
  UJ
  CO
  £
  Z
120
      O  AEROSOL VOLUME CONC.//m3/cm3
      A  AEROSOL SURFACE CONC. MO2 ,Um2/cm3)
      Q  AEROSOL NUMBER CONC. (105/cm3)
          LIGHTS ON AT 50 min
          LIGHTS OFF AT 140 mm
                                                      RUN NO. 20
                                                      2.15 ppm NO2 + 2.0 ppm C-Hg
                                                      STIRRING
                                                     •^ = 0.90//m3/cm3 hr
                   72    82
                              92
                                   102    112   132   142    152   162
                                        TIME (min)
                                                                               1.8
                                                                               1.6
                                                                               1.4
                                                                           1.2
                                                                                   en
                                                                               1.0  E
                                                                               Ill
                                                                           0.8  §
                                                                               _i
                                                                               O
                                                                           0.6
                                                                               0.4
                                                                               0.2
   52   62

Figure 21   AEROSOL GROWTH IN THE NO2 PROPYLEIME - CLEAN AIR SYSTEM
  0.9
  0.8
  0.7
  0.6
E 0.5
UJ
§0.4
O
  0.3
  0.2
  0.1
         300
           0
           162
             RUN NO. 23, MARCH 31, 1973
             SO2 = 0.56
             SITRRING
                  SO2 = 0.56 ppm
                                        O AEROSOL VOLUME CONC. Am3/cm3
                                        A AEROSOL SURFACE CONC. ,c/m2/cm3
                                        D AEROSOL NUMBER CONC.
                                              LIGHTS ON AT 150 mm
                                              LIGHTS OFF AT 210 min
                      172
                                  182
                               TIME (mm)
                                             192
                                                    202
                                                                                   900
                                                                                    800
                                                                                    700
                                                                                   600
                                                                               500 x
                                                                                   cc
                                                                                   UJ
                                                                                   m
                                                                               400 S
                                                                                   Z
                                                                                   300
                                                                                   200
                                                                                   100
                       Figure 22  SO2 AEROSOL GROWTH EXPERIMENT
                                           3Z

-------
  1.2
  1.0
I 0.8
5*.
Ill
  0.6
O 0.4
  0.2

   0
         400
         300
         200
       UJ
       CJ
       cc
         100
                   RUN NO. 24, APRIL 2, 1973
                   SO2 = 0.42 ppm          ;
                   NO STIRRING
                   dv          3   ,      '
                   — =  2.60 /am /cm0 hi    .
           56    66    '6    R6    96    106   116   126   136   146   156    166
               ,O AEROSOL VOLUME CONC. jurF/cm3
                A AEROSOL SURFACE CONC. /u.t "
                D AEROSOL NUMBER CONC.

                      LIGHTS ON AT 110 mm
                      LIGHTS Off AT 170 mm
                      Figure 23  SO2 AEROSOL GROWTH EXPERIMENT
  1.2
  1.0
JJ 0.8
  0.6
  0.4
  0.2
   O1-
          300
            92
                   RUN NO. 25, APRIL 4, 1973
                   SO2 = 0.29 ppm
                   NO STIRRING
                     f = 0.67 ^m^cm3 hr
                                                  O AEROSOL VOLUME CONC. ^m/cm
                                                  A AEROSOL SURFACE CONC. jjLm2/cm3
                                                  O AEROSOL NUMBER CONC.
                                                        LIGHTS ON AT 80 mm
                                                        LIGHTS OFF AT 170 mm
                    102
                            112
                                     122      132
                                      TIME (mm)
                                                     142
                                                              152
                                                                      162
                                                                                    600
                                                                                   500
                                                                                   400 co
                                                                                       'O
                                                                                   300
                                                                                   200
                                                                                   100
              Figure 24  SO2 AEROSOL GROWTH AFTER CHAMBER WASH
                                           33

-------
    0.6
    0.5
    0.4
  LU
  5 0.3
    0.2
    0.1
i O AEROSOL VOLUME CONC. ,tim3/cm3
 A AEROSOL SURFACE CONC. ju.mZlcn?
               RUN NO. 27, APRIL 6, 1973
                                            D AEROSOL NUMBER CONC.
                 = 0.44 /im3/cm3 hr
                                                LIGHTS ON AT 85 min
                                                LIGHTS Off AT 145 mm
            12   42    72   102   132  162   192  222  252   282  312   342
                                   TIME (min)
            Figure 25 SO2 AEROSOL GROWTH AND DECAY EXPERIMENT
 time of at least 11 hours for the Calspan chamber.   On the other hand,
 examination of all the test results suggests that other factors beside the
 volume conversion rate must also be considered when defining chamber
 working times.  These factors include particle coagulation rates,  size
 distribution of the aerosol, sources of gaseous and particulate contamination
 and the presence of heteorogeneous  gas  phase reactions.   Most of  these
 considerations are discussed in more detail in part G of this section.
             The I/ |SO2  •  dv/dt values for SC>2 aerosol growth experiments
in Table IV show a gradual decrease going from run 1 through 13 and become
relatively stable  in runs, 15,  16  and 18.  The decrease is probably due to a
'conditionin^'effect of the chamber where as differences in  nearly identical
experiments (e. g. , Nos.  6, 1Z and 13) are probably due to  slight differences
in trace background  contaminants.  Sulfur dioxide aerosol  growth experiments
which were preceded by NO,, -propylene showed somewhat higher aerosol
                                     34

-------
production rates.  It is  interesting to note that all experiments having high
           dv/dt values  (i. e. , >1. 0 u  /cm  /hr   ppm   ) were found to have
i/[so2J
high Aitken counts due to a dark reaction prior to irradiation.

            The effect of stimng/non-stir ring on SO-, aerosol growth
processes does not seem to be a critical parameter in systems with initially
Low Aitken counts.  (See e.g.  Table IV,  1/fSO, "I'd^/i-i values for runs  12, 13,
15 and 18).  Results of coagulation studies reported elsewhere within the
text (part F) confirm  this conclusion. On the other  hand,  during aerosol
decay,  coagulation rates were found to be much higher in the stirred experi-
ments .

            With respect to contamination within the chamber, it was found
that following the NO-, + propylene tests  (runs 19, 20 and 22), a  significant
increase in volumetric  conversion was observed in the SO,-air system.
After thoroughly washing the chamber walls with distilled water, however,
(run 24),  lower volumetric conversion rates  were again observed in the SO -
clean air experiments.  By comparison,  the  introduction of auto  exhaust
(Experiment 26)  did not appear to substantially affect the aerosol conversion
rate in.  subsequent SO ,  experiments (run 27)  using filtered  air.

        B_   Summary of Experiments - University of Minnesota

            Three  classes  of experiments were  performed  at the University
of Minnesota:  photochemical  aerosol growth experiments,  aerosol decay
experiments, and chamber reactivity tests.  In  the growth  experiments the
development of the aerosol was monitored after the  chamber lights were
turned on.  Particle number concentration,  total surface area, and total
volume  were measured as  a function of time.

            During an aerosol decay experiment, after a period with the
lights on, the lights were turned off and the aerosol was monitored.   Under
such circumstances the aerosol number concentration decays through coagu-
lation of particles  and loss of  particles to the chamber walls. Since  the
                                    35

-------
coagulation process is fairly well understood, careful monitoring of this
process allows a great deal to be  inferred about wall losses in the system.

            The third  class of experiments  was the  chamber reactivity
 test.  This category may be broken down into two subclasses; background
reactivity tests and dark reaction tests.    In a background reactivity
test  the chamber is flushed several  times with clean air and then filled with
clean air  at a given humidity.  The lights are then switched on and the con-
densation nuclei count is monitored.  The second type of reactivity test was
a test for dark reactions. Here the  normal experimental procedure  was
followed except that the lights were  not turned on until the elapse of a fixed
period of time.  Any aerosol growth produced in the dark was monitored.

            All experiments for the  SO, photochemical system are listed
in Table V.  The main features  of the experiments  are given in summary
form in these tables.  Immediately following  the  table  of graphs
showing pertinent results for each experiment (Figures 26 through 51).  In
most cases these graphs show the number,  surface, and volume concentrations
plotted against time with zero time set at the point  of turning on  the  lights.
Some of the plots also include illustrations  of the variation of volume mean
diameter  of the aerosol through the  course  of an experiment.  In some  cases
only nuclei concentrations were obtained.  A  number of experiments were
performed in which some major difficulty developed so that no significant
data could be obtained.  In such cases the experiments were assigned numbers
but are not listed in Table V.  The results  of the experiments which are
summarized in this and the preceding section will now be discussed  in detail
from the  point of view of photochemical aerosol production and the effects of
the smog chamber  on this production process.

        C. General Behavior of the  SO^-Moist Air  System
           All of the  SO? photochemical aerosol  systems studied exhibit
the same  general behavior.   After the reactants are introduced into  the
bag  or chamber and mixed (either by stirring or  by the filling process) and
the lights are turned on, an initiation period  follows which ranges in length

                                    36

-------
                                    Table V
 SUMMARY OF SO2 PHOTOOXIDATION EXPERIMENTS - UNIVERSITY OF MINNESOTA

NUMBER
18
19
20
22
24
25
27
28
30
31
33
34
35
36
37
40
41
42
43
44 1
45
47
48
49
50
51
52
53
54
55
56
57 __ .
58 1
59
61 I
62
,
63
64
- 66 1

lso2i
ppm
0097
0 210
0 424
0 851
1 94
2 88
-~0 04
-------
           50
                                            RUN NO. 34
                                            SO2 = 0.19 ppm
                                            R.H. = 40%
                                           •—- = 1.9yum3/cm3 hr
                           O AEROSOL VOLUME CONC. ^ m3/cm3
                           A AEROSOL SURFACE CONC. (102 .um2/cm3)
                           G AEROSOL NUMBER CONC. (10 /cm3)
                        100           150
                            TIME (mint
                                                  200
Figure 26  AEROSOL DEVELOPMENT WITH TIME FOR  RUN 34
                            38

-------
  14
  12
£ io
CO
5
z
LU
S
_
O
   S
 O AEROSOL VOLUME CONC. ^ m3/cm3

 A AEROSOL SURFACE CONC. (102 jj. m2/cm3)

 D AEROSOL NUMBER CONC. (105/cm3)
    2.5
 RUN NO. 35
 SO2 = 0.20 ppm
 R.H. = 36%

•~af = 2 M m3/cm
                                                                 hr
     20     40     60      80     100     120    140    160    180
                          TIME (mm)

Figure 27  AEROSOL DEVELOPMENT WITH TIME FOR RUN 35
                  O  AEROSOL VOLUME CONC. ^m /cm
                  A  AEROSOL SURFACE CONC. (102 /LL m2/cm3)
                  D  AEROSOL NUMBER CONC. (105/cm3)
                                  100
                               TIME (mm)
                                             150
                                                           LIGHTS
                                                           OFF
                                                           160 mm
     Figure 28 AEROSOL DEVELOPMENT WITH TIME FOR RUN  36
                                  39

-------
  12
O  AEROSOL VOLUME CONC. p m3/cm3
A  AEROSOL SURFACE CONC. UO2 JUm2/cm3}
   AEROSOL NUMBER CONC. (105/cm3)
  10
z
u.
IT
5)  6
ui
2

O  4
                                         RUN NO. 40
                                         SO2 = 0.27 ppm
                                         R.H. = 40%
                                        -JJ5-- = 7.3 JUm /cm  hr
                                                                      200
        Figure 29  AEROSOL DEVELOPMENT WITH TIME FOR RUN 40
   12
m  10
I
2
uj  8
u
cc
oo
UJ
5

§  4
O  AEROSOL VOLUME CONC. ,
A  AEROSOL SURFACE CONC.
                                          m2/cm3)
             D  AEROSOL NUMBER CONC. (105/cm3)
                                                RUN NO. 41
                                                SO2 = 0.27 ppm
                                                R.H. = 40%
                                                     -
                                                      at
                                                         = 8-3 ttm3/cm3 hr
                     50
                                     100
                                   TIME (mm)
                                                      150
                                                                      200
       Figure 30 AEROSOL DEVELOPMENT WITH TIME  FOR  RUN 41
                                     40

-------
       O AEROSOL VOLUME CONC. /I tn3/cm3
       A AEROSOL SURFACE CONC. CIO2/" m2/cm3)
       D AEROSOL NUMBER CONC. (105/cm3)
                                                     RUN NO. 42
                                                     SO2 = 0.27 ppm
                                                     R.H. = 43%
a.
HI
ca
3
Z
ui
O
  16
  ,~
  12
01
5
          20     40
                        60
                              80    100    120     140     160
                                  TIME (mm)
       Figure 31  AEROSOL DEVELOPMENT WITH TIME FOR RUN 42
   12
 £ 10
 03
 2
 2
 cc
 co 6
 O 4
       O  AEROSOL VOLUME CONC. ^mcm
       A  AEROSOL SURFACE CONC. <102 fd m2/cm3)
       D  AEROSOL NUMBER CONC. (105/cm3)
                                     100
                                  TIME (mm)
                                                           RUN NO. 43
                                                           SO2 = 0.27 ppm
                                                           R.H. = 32%
                                                      150
        Figure 32 AEROSOL DEVELOPMENT WITH TIME FOR RUN 43
                                     41

-------
        O AEROSOL VOLUME CONC. /* m3/cm3
   12
                      .
A  AEROSOL SURFACE CONC. (102 /xr
   AEROSOL
    (1Q2
D  AEROSOL NUMBER CONC. (105/cm3)
   10
IU
to
S
z
LU
o
S   6
UJ
S
O
                             V  '
  RUN NO. 47
  SO2 = 0.20 ppm
  R.H. = 18%
.  -^- = 2.22//m3/cc hr
                  10     15     20      25      30
                                   TIME (min)
         Figure 33 AEROSOL DEVELOPMENT WITH TIME FOR RUN 47
        O AEROSOL VOLUME CONC.//; m3/cm3
        A AEROSOL SURFACE CONC. (102y« m2/cm3)
        V  (1
                                            RUN NO. 48
                                            SO- = 0.20 ppm
                                            R.H. = 24%
                                            -^-= 2.10/am3/cm3 hr
   10
O
2   8
sc
00
UJ
5   6
           10      20     30     40      50      60
                                   TIME (min)
                                                   70
         Figure 34  AEROSOL DEVELOPMENT WITH TIME FOR RUN 48
                                     42

-------
                                       O  AEROSOL VOLUME CONC. ^ m3/cm3
A  AEROSOL SURFACE CONC. (102
                                       D  AEROSOL NUMBER CONC. (105/cm3)
                                                    m)
UJ    fi
CD    6
LU
O
ir
UJ
5
_j
O
                                                                    m2/cm3)
    12
 cc
 UJ
 LU
 O
 _1
 O
                   RUN NO. 49
                   SO2 = 0.27 ppm
                   R.H. = 23%
                                                            =  3.84 p m3/cm3 hr
                                                                            10
                                         n
                                      6   E
            20    40    60   80   100   120   140   160   180
                               TIME (mm)
             Figure 35  AEROSOL DEVELOPMENT WITH TIME FOR RUN 49
O  AEROSOL VOLUME CONC. /Jm3/cm3
A  AEROSOL SURFACE CONC. (102 )JL m2/cm3)
D  AEROSOL NUMBER CONC. (105/cm3)
  < Dy> (10
                                                    m)
                 RUN NO. 50
                 SO, = 0.27 ppm
                 R.H. = 58%
                 ^ = 5.35yum3/cnn3 hr
             20     40     60      80     100     120     140     160     180
                                     TIME (mm)

             Figure 36  AEROSOL  DEVELOPMENT WITH TIME FOR RUN 50
                                        43

-------
cc
UJ
              50
                      100
      150      200


        TIME tmin)
                                             250
       Figure 37  AEROSOL DEVELOPMENT WITH TIME FOR RUN 51
    3 -
 o
 u
 CC
 111
 CD
 5

 z

 -I
 o

 8
 a:
 UJ
                   RUN NO. 52

                   SO_ = 0.23 ppm

                   R.H. = 25%
                                 LIGHTS OFF AT 149 min



                                 I	i	1	i  i i -i	i	L
     -50 SO2 o

            25
                  50
 100    150    200    250    300

TIME (mm)
        Figure 38 AEROSOL DEVELOPMENT WITH TIME FOR RUN 52
                                   44

-------
          SO2 = 0.22 ppm

          R.H. = 30%
O

O
u
cc
LU
co
5

z
_l
o
CO
O
cc
LU
                                   50

                              TIME (mm)
                                                           150
          Figure 39  AEROSOL DEVELOPMENT WITH TIME, RUN 53
                              50

                              TIME (mm)
                                                      150
          Figure 40 AEROSOL DEVELOPMENT WITH TIME, RUN 54
                                45

-------
   14
   12
   10
cc
m
00
2
z
UJ
u
cc
00
UJ
5
_l
o
O  AEROSOL VOLUME CONC./Jt m3/cm3
A  AEROSOL SURFACE CONC. (102>< m2/cm3)
D  AEROSOL NUMBER CONC. (105/cm3)
O   (10"2< m)
     0      20
      5 mm
                         60
                       80     100    120
                           TIME (min)
140
       160
              180
           Figure 41  AEROSOL DEVELOPMENT WITH TIME FOR RUN 55
cc
UJ
m
5
D
u.
cc
tfl
UJ
5
_i
O
          O  AEROSOL VOLUME CONC. fj( m3/cm3
          A  AEROSOL SURFACE CONC. HO2 /J m2/cm3)
          D  AEROSOL NUMBER CONC. U05/cm3)
          O (10"2/um)
                                              RUN NO. 56
                                              SO2 = 0.28 ppm
                                            :  R.H. = 17%
                                                       m3/cm3 hr
               20     40      60     80    100    120
           Figure 42  AEROSOL DEVELOPMENT WITH TIME FOR RUN 56
                                      46

-------
 Ul
 CD
 5
 LU
 3
 O
                                     O AEROSOL VOLUME CONG, ^rt/cm
                                     A AEROSOL SURFACE CONC. (102 >
-------
  12

  11

  10

   9

   8

   7

   6

   5

   4

   3

   2

   1

   0
  O  AEROSOL VOLUME CONC. JUm /cm
  A  AEROSOL SURFACE CONC.
                                    m2/cm3)
           AEROSOL NUMBER CONC. (105/cm3)
RUN NO. 59
SO2 = 0.25 ppm
R.H. = 51%
    0 4    20
    3 min
           40
                                                         m /cm  tu
                         80     100    120
                            TIME (mm)
                                            140
                                                   160
                                                          180
                                                                200
          Figure 45  AEROSOL DEVELOPMENT WITH TIME FOR RUN 59
0*7
O  AEROSOL VOLUME CONC. yUm3/cm3
A  AEROSOL SURFACE CONC. <102 /J. m2/cm3)
D  AEROSOL NUMBER CONC. (105/cm3) '.,
                                                    RUN NO. 60
                                                    SO_ = 0.26 ppm
                                                    R.H. = 38%
         20   40   60    80    100   120   140   160   180   200   220
      Figure 46 AEROSOL  DEVELOPMENT WITH TIME FOR RUN 60
                                     48

-------
                                RUN NO. 61
                                SO_ = 0.21 ppm
                                R.H. = 28%
         80     120    160    200    240    280    320
Figure 47 AEROSOL DEVELOPMENT WITH TIME FOR RUN 61
                                    (^-LIGHTS OFF AT 256 min
               120    160    200    240    280    320    360
Figure 48  AEROSOL DEVELOPMENT WITH TIME FOR RUN 62
                         49

-------
                                ALIGHTS OFF AT 213 mm
                              r	
                                    RUN NO. 63
                                  •  SO_ = 0.34 ppm
                                    R.H, = 26%
            100
                           200
                         TIME (mm)
                                           300
                                                          400
Figure 49 AEROSOL DEVELOPMENT WITH TIME FOR RUN 63
                             RUN NO. 64
                            • SO2 = 0.29 ppm
                             R.H. = 58%
         80
               120    160    200
                   TIME (mm)
240
      280
            320
  Figure 50 AEROSOL DEVELOPMENT WITH TIME, RUN 64
                          50

-------
                  5.63 /Im3/cm3 hr
O AEROSOL VOLUME CONC./< m3/cm3
                                    AEROSOL SURFACE CONC.
                                    AEROSOL NUMBER CONC. 105/cm
                  LIGHT OFF AT
                    185 mm
             40   80  120   160   200  240   280   320  360   400
                                  TIME (mm)
             Figure 51  AEROSOL  DEVELOPMENT WITH TIME FOR RUN 66

from less than a minute to 10 to 15 minutes depending on the lighting and
humidity conditions in  the chamber.  During this initiation period, there  is
no observable production of aerosol, i.e., the nuclei count remains at its
baseline level of approximately 50 particles/cm  and the electrometer
current in the WAA is  essentially zero.  As the partial pressure of sulfuric
acid vapor builds, a critical saturation is reached and rapid homogeneous
nucleation occurs.  The condensation nuclei count suddenly begins to rise
and usually exceeds 10  particles/cm  within a few minutes.   Almost
simultaneously  the WAA begins to detect an aerosol.  Doyle (1961) suggests
that  the radii of the tiny embryos  that form is in the  neighborhood of 6A
and that the  number of molecules  contained in each embryo is about ZO.
Clusters of molecules  which do not exceed the critical size evaporate,
whereas those which attain a critical radius become  increasingly stable
and grow  into larger droplets.   The  rate of production of new particles
decreases as the aerosol surface  increases since condensation of the  acid
vapor will now occur on existing nuclei.  As the  particle concentration
grows,  coagulation becomes more important until finally the loss rate by
                                    51

-------
coagulation is just balanced by the production rate of new particles.  At
this time the maximum nuclei concentration is reached.  At later times
chemical nucleation continues to produce new particles, but the rate of
production is  less  than the coagulation rate so that the particle concentration
continues to decrease.  As the aerosol grows, new surface is  produced by
chemical nucleation and by condensation on existing particles.  At the
same time surface is  being lost by the coagulation of particles.  In most
experiments the  rate of production and the rate of loss  of surface achieve
a balance through a significant part of an experiment and a dynamic equili-
brium surface is achieved.  It will be shown later that the equilibrium surface
achieved correlates very well with the volume rate of aerosol  production.

            The total aerosol  surface area,  S,  (firm  /cm  ) behaves  in a
somewhat different manner.   It starts to rise  shortly after the initial forma-
tion of nuclei but rises more slowly and approaches a steady dynamic
equilibrium value which remains essentially constant throughout the latter
part of the growth period.  The volume,  V,  (urn  /cm ) begins to grow at
the same time as the surface  and grows in an  essentially straight line
fashion.   It will be shown below that this linear volume growth characteristic
of the SO-, photochemical  system may be explained in terms of a simple,
plausible model.

            The photooxidation of SO , in the atmosphere is believed to be
first  order in SO-,.  In the system under study here,  the rate of photo-
oxidation is low,  i.e., a fraction of a % per hour.  Consequently,  the  SO-,
concentration remains essentially unchanged during an experiment (up to
12 hours in the Calspan chamber and 7-8 in the University of Minnesota
chamber) and the products of  SO-, oxidation are produced at a  constant
rate.  The main product of SO-, oxidation in clean air is believed to be
SO,;  and if moisture is present, sulfuric acid droplets will eventually be
formed.
            Friend et al (1973) have suggested that the initial formation of
sulfuric  acid nuclei takes place through the following reactions:
                                    52

-------
            S03 + HZ0
            H2S04 + H20
                                                                     (3)
A  simple model for the  production of an aerosol in the SO-, photochemical
system which is consistent with our experimental observations can be based
on these reactions.

            The model assumes the  chemical reactions listed above and that
aerosol growth is governed by the following processes:

            (1)  The aerosol detected consists of sulfuric acid droplets.
            (2)  New particles are formed by  the chemical nucleation process
of reactions (l)-(3).
            (3)  Particles are lost in number  by coagulation;  that is,  when
two particles collide as  a result of Brownian  motion,  they stick together
and become  one larger particle.  The rate of this process is proportional
to the  square of the number concentration of such particles.
            (4)  Particles grow in size by condensation and coagulation.
Condensation is simply the diffusion of SO, and/or H,,SO, vapor to the  sur-
face of a particle  and its solution in the liquid particle.  The rate of this
process will be proportional to (Xv)Sh,-. where S is aerosol surface area
and h  is the mass transfer coefficient for Xv (SO"  and/or H?SO  vapor)
diffusing to the droplet surface.   It is assumed that water vapor also diffuses
to  and  from the particle at a rate sufficient to keep the internal water vapor
pressure  of the aqueous sulfuric acid droplet equal to the vapor pressure of
the water in the overall  gas phase.

            (5)  Wall losses and wall production effects are not important
(for small vessels of a few cubic meters and for long  working times in

                                    53

-------
larger chambers,  this assumption is  not valid; however, for the  experi-
 ments reported here this  assumption appears justified during the aerosol
production phase.)

             SO., production reactions  will start as  soon as  the lights are
turned on.  During the initiation period (SO,) builds up and  nuclei growth
takes place by reactions  (l)-(3) to sizes  sufficient to be detected by the
CMC.  The detection limit of most small particle counters is about 0, OOZ
jam.  This chemical nucleation process continues until substantial aerosol
surface area has been developed.   Once this occurs,  there  are  two parallel
paths which  allow for SO, and H?SO. vapor to participate in further aerosol
growth:  continued chemical nucleation and condensation.

             The expected rapid reaction rate of SO, with water vapor,  as
well as the exceptionally low vapor pressure  of H?SO . suggests that these
gases achieve  steady  state concentrations shortly after initial homogeneous
nucleation in the SO?  irradiated system.  The steady state conditions  remain
until enough  aerosol  surface has been  produced to allow  condensation  to be
an important mechanism.   Consequently, (SO,) will begin to fall and the
rate of production of new  particles through chemical nucleation drops.  This
model is consistent with our experimental data as illustrated in the plots  of
N and S against time  in the SO.-, photochemical system.

           Further insight into the aerosol formation process may be gained
by observing the development  of the aerosol size  distribution as a function
of time.   Figure 52 shows time histories of number concentration for four
different particle sizes observed with  the WAA for  experiment no. 15  in the
Calspan chamber,,  Initially,  the aerosol is comprised almost entirely of
very small (*".0075 u.m) particles.  As  condensation and coagulation proceed,
larger particles are  formed and the distribution broadens and shifts toward
larger sizes.  Finally, particles will  grow sufficiently large where fallout
will become  important and substantial volume loss  will occur.  Figures 53
and 54 show  typical growing aerosols  for high and low volumetric conversion
rates in the  University of Minnesota 600 ft  chamber.  Here the cumulative
                                     54

-------
                                              O = 0.007 /U m
                                              A = 0.013/< m

                                                  0.023M m
                                                  0.042,// m
62   102
                   142  182   222  262  302   342   382  422   462   502
                                   TIME (mini
Figure 52  TIME HISTORIES OF NUMBER CONCENTRATION FOR FOUR DIFFERENT PARTICLE
         SIZES OBSERVED WITH THE AEROSOL ANALYZER.   (RUN 15)
                          55

-------
            1.0 r

            0.7

            0.5

            0.3
        J-  0.07

        u  0.05
        <  0.03
        Q
           0.01

          0.007

          0.005
       RUN 58:  HIGH VOLUMETRIC CONVERSION RATE
                                               176V4 min
                                                48/4 min
                                               17'/i mm
                  5   10   20    40    60     80   90   95  98
                            PERCENTAGE
  Figure 53  PERCENTAGE OF VOLUME ACCOUNTED FOR BY PARTICLES
           SMALLER THAN THE DIAMETER DVG VS. DyG
 1.0

 0.7


 0.1

0.07

0.05

0.03
         UJ
           0.01

          0.007

          0.005


          0.003
                   RUN 60:   LOW VOLUMETRIC CONVERSION RATE
              2   5   10   20    40   60    80   90  95  98
                           PERCENTAGE
Figure 54  PERCENTAGE OF VOLUME ACCOUNTED FOR BY PARTICLES
          SMALLER THAN THE DIAMETER DVG VS. DVG
                                56

-------
aerosol volumes at different times are plotted against particle diameter on
log-probability paper.  It may be seen that as  time passes the aerosol grows
and at the same time the size distribution  broadens.  These curves allow
particle volume mean diameter to be determined rather easily.   Volume
mean diameters,  the diameter at which the cumulative volume distribution
curves cross the  50% line,  obtained  in this manner are plotted along with
the N, S,  and V values against time  plots for some of the  University of
Minnesota experiments as shown in Figures  33, 34, 41 through 46 and 51.
Examination of such  plots shows that the volume mean diameter increases
almost linearly with  time as an experiment proceeds.

            Examination  of the aerosol number, surface,  volume and
volume mean diameter profiles for the SO-, photochemical system reveals
that the general qualitative behavior  of the system is the same regardless
of SO-, concentration  or humidity.  In addition, comparison of Figures 41
through 44,  which show the results of experiments performed in  the small
bag, with the remaining figures  representing large chamber data indicates
that the general features of aerosol behavior are riot influenced by bag
size within the working times of these experiments.
                                    57

-------
       D.  A General Correlation
            In these experiments a wide variety of conditions have been
explored.  One  significant point that emerges,  however,  is that the same
general trends in variation of aerosol nurnber, surface and volume with
time are evident in virtually all of the experiments.  This is particularly
true for volume and surface development.  The volume tends to grow
linearly with time and the surface attains  an equilibrium  value  which is
maintained throughout a significant fraction of  the growth period.  Clark
(1972) pointed out that a strong correlation exists between the volumetric
conversion rate in the linear portion of the volume  growth curve and  the
equilibrium surface.  He  found that a  log-log plot of c/v/Mt   against S^
yielded a  straight line.  In order to further test his correlation all the
useable data obtained in the Calspan and University of Minnesota  test series
have been plotted on the same coordinates.  The  results  are shown in
Figure 55.  It is seen that the general trend exists  and that the data  are
scattered uniformly and in good agreement with Clark's correlation  line,
The scatter in the results is felt to be primarily due  to fluctuations in the
WAA and  is not believed to reflect on  the  validity of the general correlation
line.
    1 x 10
        7
        5

 £
 5.
 oa
 O
1 x 10
    7
    5
       A  CALSPAN EXPERIMENTS      20,800 ftj
       O  LARGE BAG EXPERIMENTS      600 ft3
       P  SMALL BAG EXPERIMENTS      90 ft3
       O  LARGE BAG, CLARK (1972)      600 ft3
                      S = 314
    1 x 102
         0.1    0.2  0.3  0.5 0.7  1      2   3   5  7  10     2O  30   50 70 100
                                •$;
-------
        E.  Observed Rates of Photooxidation of Sulfur Dioxide

            In both the University of Minnesota and Calspan experiments,  it
 has  been found that the  rate of volume production approaches a constant
 value,  i.e., a plot of volume  against time yields a straight line.   The
 reasons for this are as follows:  Once an equilibrium  surface  has  been
 achieved,  the  concentration of SO, in the gas phase will approach  a steady
 state value.  Then the rate of oxidation  of SO, will be equal lo the rate of
 appearance of SO-, in the condensed phase in the form of sulfuric  acid drop-
 lets.  The rate of production of sulfuric acid aerosol, corrected for mole-
 cular weight change  and water concentration must be equal to  the rate of
 photooxidation of SO , which is a constant for these experiments.   Thus, the
 Tlope of the straight line volume growth curve may be related directly to
 the  rate of photooxidation of SO-,.  The governing equation is:

                       _ d[S02l  B dV x Q x P  x^l                      (4)
                           dt      dt          MU2

 where  p   is the  density of the  sulfuric  acid  droplet, P is the weight fraction
 H-,SO.  in the drop, MW is the molecular weight of SO,, and MW7 is  the
   C.   ~r                 i                              £-          
-------
            Using equation (4) and the measured value of  dvyc/"fc     in each
experiment, the rate of SO-, photooxidation can be determined.  These rates
are listed in Tables IV and V for the University of Minnesota and Calspan
experiments, respectively. It is rather disturbing to note that there  is a
large spread between the maximum  and minimum observed rate of photo-
oxidation.   The range is from 0.069% to about 0. 529% per hour for the
University of Minnesota experiments and from  0.005% to 0.022%  for the
Calspan tests.   This variation cannot be directly tied to any obvious  experi-
mental  variable such as SO-, concentration,  bag size,  or  relative humidity.
The  lower values observed in the Calspan experiments are partly due to
lower light  intensity; however,  recent results of Friend et al (1972) have
shown that Aitken nuclei are formed via the SO-,-O atom oxidation reaction
in the presence of water vapor  and that Aitken nuclei are  not formed to any
extent by the interaction of SO-, excited states with O-,, H -,O, or O-, and H-,O.
If these results are correct,  then any calculated SO-, photooxidation must be
due to chamber contamination.   According to Friend et al,  no observable
nuclei should be formed in a contamination-free SO-,-clean air system.

            In the Calspan  chamber, the only source of O-atom would be
from the photolysis of background NO-,.  It is fairly simple exercise to
calculate what  the background NO-, levels  would have to be in order to
achieve the  SO-, photooxidation  rates reported here.  Based  on the light
intensity of  the  Calspan chamber, the SO, photooxidation rate via O-atom.
                                   ~~)
attack is equal to fNO J"j (1. 62 x 10   )%/hr.  This calculation suggests that
NO-, background levels of 0. 3 to 1.5 ppm  are needed to account for the
photooxidation  rates  observed here.  Such high levels were not detected in
the experiments nor  would they be expected in extensively filtered air.

            A second contribution,  that of SO-, photooxidation in the HO?-
SO _,  reaction, is not  so  easily eliminated.  Hydroperoxy radical concentration
is usually several orders  of magnitude greater than that of O-atoms in the
atmosphere (and the  chamber), and therefore may contribute significantly
to the SO-, photooxidation rate.   We  are presently looking into the contribution
                                     60

-------
this  reaction may
qu.es.
have on SO-, photooxidation via computer modeling techni-
            Figure 56 shows an attempt to correlate the photooxidation rate
with relative humidity.  Here the observed photooxidation rate in % per hour
is plotted against relative humidity for University of Minnesota experiments.
Three groups of experiments are shown: the initial work done at low
humidities by Clark, and on this program the variable humidity experiments
done in the  small bag.  (Since all experiments in the Calspan chamber were
conducted at 30% RH, these points were not included in the plot.  The observed
SO-, photooxidation rates, however,  were on the average  lower by a factor of
at least ten.) All the points  seem to scatter in the same general way, and
there is no  trend evident with changing relative humidity.  The scatter
observed probably came  from some sort of contamination.  The most likely
sources are atmospheric pollutants which are not removed by the  charcoal
scrubbing system.  Synergistic interactions between SO-, and these materials
could result in significant changes in the SO-, photooxidation rate  and in the
rate of aerosol  formation.
                      1.0
                      0.7
                      0.5
                   z  °'3
                   o
                   K
                   g
                   x
                   o
                   6
                   o
                   a.
                   ff 0.1
                     0.07
                     0.05
	 *-- -
-
%**
o
- :
O LARGE BAG EXPERIMENTS •
D SMALL BAG EXPERIMENTS "'
O LARGE BAG, CLARK (1972) *
[ <
^,
?
0-
0
D



O
<
O f
D



"O""
!>
)
o
)





i i, i
0
D-









D
O


1


- --,

_,
- - -i
- .
1
                                    40     60
                                      RH (%)
                                                80
                                                       100
         Figure 56  SO2 PHOTO-OXIDATION RATE VS. RELATIVE HUMIDITY
                                     61

-------
            Another possible source of scatter in the results is the unstable
performance of WAA.  The  charger performance in this instrument is at
times somewhat variable and if this variation goes  unnoticed,  errors in  the
surface and volume measurements can result.  This would lead to errors in
the measured volumetric conversion rates,  and thus the computed SO,
photooxidation rates.

            Although the data do not show any clear  dependence of the SO?
photooxidation rate on relative  humidity, the quantity of aerosol formed  is
strongly dependent on humidity.  Volumetric aerosol production rates are
much higher at high relative humidities, as  would be expected since the
developing aerosol is composed of H-,SO. droplets.  The effect is  illustrated
in Figure 57 which shows the dependence of  '/TiO^"] • dvVc/t  , the volumetric
production rate adjusted  for SO-, concentration,  on relatively humidity.
The high volumetric  production rates at high relative humidities result from
the fact that the equilibrium water to acid ratio in the aerosol  droplets
increases with humidity.  Thus for any  given quantity of SO, produced, a
larger volume of aerosol will be formed at high relative humidity  than at
low relative humidity.  This is  significant because  in terms of environmental
impact, it is the quantity of aerosol formed  rather  than the rate of SO-,
photooxidation which is important.

       F.   The Propylene-NO   System

            Because  of the  low  light intensity observed  in the Calspan
chamber, only three propylene-NO  experiments were  performed during
                                  X
the first year.  In  each of the experiments,  NO-, and propylene were injected
directly into the chamber after  first filtering the  chamber air  for  10 to 1Z
hours.  In two of the three  experiments, some production  of nuclei occurred
prior to irradiating the samples.  NO,  NO-,, oxidant and aerosol growth
were monitored for each of the  experiments.
                                    62

-------
                    =5,
                     (M
                    O
uu
70

50



10




?
- , . O LARGE BAG EXPERIMENTS
— t 	 D SMALL BAG EXPERIMENTS
- ' : '
-







1
 i

•o - to
(.
••••©<
a




o

11
k
0






L

O
D

; 0; . ,
•i ; ^ -- -i

,






i '• i ; i
                        0     20     40     60     80     100
                                     RH (%)
  Figure 57  NORMALIZED VOLUMETRIC CONVERSION RATE VS. RELATIVE HUMIDITY
            The results are summarized in Table VI, along with the two
NO-propylene experiments that were performed in the 600 ft  University of
Minnesota chamber.  The table shows initial concentration of gases, volu-
metric conversion rates,  peak nuclei concentration, and equilibrium surface
area, as well as chamber temperature  and humidity.  The University of
Minnesota tests were partially designed to study the effect of humidity on
aerosol behavior in the  NO-propylene system. Examination of the table
shows that the  volumetric conversion rate, <^v/a.t ,  is much larger for the
high humidity case, a result which is supported by more recent Calspan
tests.  Also, the maximum  nucleus concentration is twice as great in the
high humidity case.
                                    63

-------
                                 Table VI
        SUMMARY OF NOX-PROPYLENE PHOTO-OXIDATION EXPERIMENTS
RUN
NUMBER
N02
ppm
[C3H6]
ppm
dv/dt
urn /cm hr
NMAX
103 cm"3
SE
2 3
(U m /cm
TEMP.
°C
RH
%
COMMENTS
CALSPAN
19
20
21
3.00
2.15
1.51
1.5
1.5
1.5
0.52
0.90
1.20
450
300
450
135
>200
240
~25
~25
~25
— 35
~35
~35
STIRRING
STIRRING D. Rx
STIRRING D. Rx
UNVIERSITY OF MINNESOTA
65
67
INO),
0.55
0.55
2.19
2.19
1.00
9.26
260
521
515
900
27
30
25
65
GROWTH 250 mm
DECAY 190 mm
GROWTH 260 min
DECAY 20 mm
   [NO)( DENOTES CALCULATED INITIAL NO CONCENTRATION
   D Rx DENOTES DARK REACTION PRODUCING NUCLEI BEFORE LIGHTS WERE TURNED ON
            Examination of the NO and NCU concentration profiles for the
University of Minnesota tests  (Figures  58 and 59) shows that the onset of
aerosol growth occurs when most of the initial NO has been converted into
NO^.   It is  possible that NO has an inhibiting effect on the production of
aerosol, which is consistent with the general belief that ozone- olefin
reactions are responsible for  gas to aerosol conversion in such systems.

            Time histories of  aerosol number,  surface and volume concen-
trations for these experiments are shown in Figures 60 and 61.  It may be
seen that  the general characteristics of the developing aerosol are quite
similar to those  exhibited by the  SO? system.  In the Minnesota NO  -HC-air
                                   <—                             3C
experiments, the initiation period before the  onset of aerosol growth is
much longer than that in the SO-,  tests.   Delayed aerosol formation did not
occur in the Calspan tests probably because NO?  (and not NO) was introduced
into the chamber.
                                    64

-------
Q.
a
     0.7
     0.6
     0.5
     0.4
U
8    a3
     0.2
     0.1
              D NO
              O NO.
                                                        RUN NO. 65

                                                        [NO] j = 0.55 ppm

                                                        C3H6!i =2'1
                                                        R.H. - 25%
              40
                     80
                           120    160
                                                              320
                                    200     240     280

                                     TIME (mini

Figure 58  NO AND N02 CONCENTRATION WITH TIME FOR RUN 65
     0.7
     0.6
     0.5
     0.4
§   «>-3
     0.2
     0.1
              a NO
              O NO-
                                                        RUN NO. 67

                                                        (NO) ( = 0.55 ppm

                                                        IC3H6'i *2'19 pP
                                                       , R.H. = 65%
       0      40      80     120    160    200    240    280    320
                                         TIME (mint

     Figure 59  NO AND N02 CONCENTRATION  WITH TIME FOR RUN 67
                                      65

-------
 ai
 0
 u.
 oc
 LJ
 §  3
 O
 O  AEROSOL VOLUME CONC. /*m3/cm3
 A  AEROSOL SURFACE CONC.  (102 //m2/cm3) .
            VJUMBI
            yWm)
          AEROSOL NUMBER CONC. (105/cm3)
       O 
                                                                           a
                                                                         ~ >u
                                                                         2 oo
   14
  12
   10
E

          40   80   120   160   200   240   280   320   360   400   440
                                    TIME (mm)
         Figure 60  AEROSOL DEVELOPMENT WITH TIME  FOR RUN 65
      O AEROSOL VOLUME CONC.//m3/cm3
A  AEROSOL SURFACE CONC. (102//m2/cm3)
   AEROSOL NUMBER CONC. (105/cm3)
                                                LIGHTS OFF
                                                266 min
      O 
RUN NO. 67
[NO] ( = 0.55 ppm
[C3H6li = 2.19 ppm
R.H. = 65%
           40     80     120    160     200    240    280    320     360
                                   TIME (min)

         Figure 61  AEROSOL DEVELOPMENT WITH TIME FOR RUN 67
                                                                             CO
                                                                             5
                                      66

-------
            The above figures also show that the volumetric growth curves
in the Minnesota tests were non-linear; in the Calspan experiments one of
the three  tests had a non-linear growth rate.  Part of the explanation may
lie in the  volume vs time curve shown in Figure 61 for experiment no. 67.
The figures show a significant loss in volume in the latter part of the lights
on period of the experiment. This decrease could be  due to wall losses or
to gas  phase destruction of the aerosol already  formed.  The processes
responsible for loss  of aerosol to the wall in the NO-propylene system
should be similar to  those in the SO-, system.  Such losses do not occur to
any significant extent in the SO-, system,  so it is unlikely that wall losses
are responsible for  the observed volume decrease in the NO-propylene
system.  Gas phase destruction of the aerosol is possible and this implies
that some of the  species which originally condensed to form the growing
aerosol have dropped to such low concentration  that they begin to evaporate
from the surface of the particles.  Although this is possible, it is much
more likely that  the apparent volume decrease is an experimental artifact.
Figure 62 shows two aerosol volume distribution curves near the end of the
experimental runs.   Here the volume distribution function AV/A log  D
is plotted against particle diameter at a fixed time.   The area  under  the
curve between any two diameters corresponds to the  volume  of aerosol in
that size interval.  Early in the  experiment it may be seen that the  volume
distribution is a  more or less symmetrical curve. However, as time pro-
gresses,  more and more of the righthand part of the  curve appears to be
cut off.  This  suggests that  the aerosol is growing out of the  size range of
the instrument which, in turn,  could lead to a deviation from linear growth
at long reaction times.

            Following the analysis of the  propylene-NO  experiments, the
Calspan data  were compared with  computer simulation results using the
propylene-NO  reaction model developed by Demerjian,  Calvert and Kerr
(1973). This model has proven quite successful in simulating the experi-
mental chamber  results of Altshuller et al  (1967) and Spindt (1973) for the
                                    67

-------
>
<
       O AEROSOL VOLUME CONC. * m3/cm3
          AEROSOL NUMBER CONC. (105/cm3)
        RUN NO. 67
        O134 mm
          249.5 mm
                                                                  MAXIMUM
                                                                  RANGE FOR'
                                                                  WAA
    2  	
    .001
Figure 62
                                            Dp VS. Dpm
                                     68

-------
propylene-NO   system.  The modeled results are  shown as continuous solid
             5C
lines in Figures 63 and 64 and are compared with experimental data which

are  shown in symbols.  The only rate  constants altered from those used in

the original model were photolytic reactions depending on available light

intensities and the two heterogeneous reactions,
and
                                    HONO2                          (5)
                    NO2 + NO + HZO—> 2 HONO                     (6)
The measured rate constant for NO-, photolysis determined in the Calspan

chamber was  used and all other photolytic rate  constants were scaled down

proportionately.   The rate constants used for reactions (5) and (6) were

lower by an order of magnitude as compared to those  used in the referenced

report.  This is reasonable  in view of the reported heterogeneous nature

of these reactions and the different surface-to-volume ratios of the chambers

used.  The surface-to-volume ratio in typical smog chambers is in the range
               -1                                  S             -1
of 2 to 5 meter  , while the  Calspan chamber has a   /  /~r 0. 25 m  .  The

modeled results are in quite good agreement with experiment,  except for

experimental  ozone  values which are  consistently high in the Calspan

studies.  Uncertainties in the initial propylene concentrations present
                                  *
could account for  this discrepancy.
'Experiments 20 and 22 were run before the hydrocarbon analytical system
 was  set up.  Therefore, initial propylene concentrations were approximated
 based on expansion of known concentrations of propylene into the chamber.
 The  expected concentration of propylene was 3 ppm.  In light of more
 recent determinations using the hydrocarbon analytical system, these
 concentrations are probably closer to 1. 5 ppm.
                                    69

-------
            3.0
    10
 o
          I
                                               EXPERIMENTAL POINTS



                                               a = NO

                                               A= o3

                                               O = NO

                                               	 MODELED RESULTS

                                                   RUN NO. 20
               0    10    20    30   40    50   60   70   80   90   100
                                                                            50
                                                                            40
                                                                            30
                                                                            20
                                                                            10
                                                                                 E

                                                                                 i
                                                                                 a
Figure 63  EXPERIMENTAL AND MODELED RESULTS FOR THE PROPYLENE - NOX SYSTEM
            2.0
   10.0
    5.0
 O
     0 L
J.

 CM
O
z
            1.0
            0.5
                                                        EXPERIMENTAL POINTS



                                                        D =  N02

                                                        A =  03

                                                        O =  NO

                                                        	  MODELED RESULTS
                                                             RUN NO. 22
                                       ' A
                                                      a
                                               A   A   A  A
                                 O  O   O   O  O   O
              0   10  20  30   40  50  60   70  80  90 100  110  120 130


                                   TIME (min)
                                                                            50
                                                                            40
                                                                             30
                                                                        E
                                                                   20   .c
                                                                        a.
                                                                        a


                                                                   10  e"
Figure 64  EXPERIMENTAL AND MODELED RESULTS FOR THE PROPYLENE - NOX SYSTEM
                                         70

-------
It should be noted that the above data are derived from a limited number of
preliminary experiments and are not intended for  in-depth modeling.  More
detailed comparisons of experimental and modeled results for the  NOx-
propylene  system will be made during the coming  year.

        G.   Chamber Effects on Aerosol Behavior

            So far the aerosol behavior has been discussed as though there
were no walls  containing the photochemical system, although it is  obvious
that in any laboratory chamber wall effects can  be an important factor in
determining the behavior of the aerosol.  Typical  effects include:  reactions
which take place directly on the walls, contaminants which remain on the
walls and catalyze a variety of photochemical reactions,  and gas or  parti-
culate phase materials which are lost to the walls.

            In  the systems used in  this investigation, the influence of walls
on SO-,  photooxidation rates was not an important factor. This can be partly
seen by reviewing the University of Minnesota data tabulated in Table V,
in which it is shown that the  observed SO-, photooxidation rates did not reflectj
a dependence on bag size.  It may be argued,  however,  that  any observed or
calculated SO-, photooxidation is due to contamination in light of Friend et a I
(197^) suggestion that Aitken nuclei arising from SO-, photooxidation  would  be
formed at rates too small to be observable in a  contamination-free environ-
ment.  The nature of such contaminant initiated  reactions are not  fully
understood at this point, and so possible  wall effects in this  regard cannot
be evaluated.  A more logical approach is to examine aerosol behavior within
the chamber as an indicator  of the effects of walls on the overall system.
Three experimental techniques were used to study the importance  of wall
effects:  coagulation experiments, linearity checks on volume production
curves  for the  SO-, photochemical aerosol, and chamber reactivity tests.
These studies are briefly described below.
                                    71

-------
            1.  Coagulation experiments

               The rate of coagulation of an aerosol is given by
where k is the mean coagulation rate constant for Brownian coagulation.  Its
value depends on the particle size distribution but for a monodisperse distri-
bution with particle diameters in the range 0.01 to 0.05 fim, (the range of
                                                              - 9    3
interest in this work), the value is slightly greater than 1.0  x 10   cm /
particle-sec.  According to Fuchs (1964), as the aerosol becomes  more
polydisperse, k increases.
              In a smog chamber,  particles may be lost by diffusion to
the walls as well as by coagulation.  The governing expression then becomes

                          - ~jf   =  kN2 + a N                      (8)

where a is a first order wall  loss coefficient and N is particle number.
Ignoring the dependence of the second term  on N, integration gives

                             —  -  —            a)
                                    o

If wall losses are unimportant a plot of 1/N against time for a decaying aero-
sol should  yield a straight line of slope k. However,  if wall losses are
significant, the apparent value of k will increase as N decreases.   Experi-
ments have been performed at both Calspan and the University of Minnesota
in which number concentration have been measured and the  results plotted
in the form of 1/N against time.   The results  are summarized in Tables VII
and VIII.   The plots are presented in Figures 65 to  79 for the University of
Minnesota  tests and Figures  80 to 96 for the Calspan  tests.
                                    72

-------
CO
z
D
CC
CC
O
u.
to
<
o
uj
H-
<
CC

•z.
o
o
o





i
UJ
5
O
o


v- '05
§ "E
Q
U T—
•* o
H '05
I CO

-1 0
0 r-
CC

D 5
uj E
_
1-
H
I
o
_, c
uj i
H
CC
2



















05
O
CO
UJ
(3
CC
<
_1






c c
E E
° 8

H H
UJ UJ
CC CC
2 I?
2 5
cc cc
3 3
U U
Q Q
cc cc
1 1

(»ooo>a.J f- t-
^ssssssss--




















o
<
CO
^
2







c c c
E E E
o o o
^ u3 in
H H H
UJ UJ UJ
cc cc cc
H H H
cc cc cc
33 3
U 0 0
Q Q Q
CC CC CC
5 S 2
a. a. a.

t— to m i— r^
»~ O) ff) T- 00
*~


r- o> m 10 a>
t i- O O 0




in o o o o





o o o o o
ro m ^ CN o
in m r~ o> o
in in in in 10

                                                              UJ

                                                              I UJ

                                                              HI
                                                              CC UJ
^80. £

S2<§
0>->M
";<
-------
                  Table VIII
COAGULATION RATE CONSTANTS FOR SEVERAL EXPS
       PERFORMED IN CALSPAN CHAMBER
AEROSOL
EXP. NO.
4
12
23
24
21
13
25
3
11


20 C3H6
22 C3H6
BEHAVIOR
STIRRING
YES
YES
YES
YES
YES
NO
NO
NO
NO


-NOX YES
-NOX YES
(LIGHTS ON)
SO2 -.AIR !
K cm /sec
\*
4.1 x 10~11
8.3 x 10'11
2.1 x 10'10
3.1 x ID'10
3.2 x 10"10
9.4 x 10~11
2.6 x 10"10
2.0 x 10'10
1.2X10'10

AEROSOL
SYSTEM
EXP. NO.
4
16
14
27
12
13
14
1
16
27
C3Hg - NOX SYSTEM
6.2 x 10 10
7.8 x 10"10

BEHAVIOR
STIRRING
YES
YES
YES
YES
YES
NO
NO
NO
NO
NO


(LIGHTS OFF)
— o
K cm /sec
\f
5.7 x 10'10
1.6 x 10'9
2.1 x 10~9
3.0 x 10'9
3.3 x 10'9
1.5x 109
3.7 x 10'10
4.1 x 10'10
9.3 x 10"10
3.0 x 10"9


                     74

-------
 E

-------
      15
to
 'o
      10
                                 LIGHTS OFF  '  '   •  '
        0            50           100          150           200
                              TIME (WIN)

           Figure 67   AEROSOL COAGULATION - U. OF M.   RUN 51
       15
       10
                                              15.9 x 10"1Q cm3/sec
             40    80   120   160   200   240   280   320  360  400
                                TIME (mm)

             Figure 68  AEROSOL COAGULATION - U. OF M.  RUN 52
                                       76

-------
(O
 'o
       15
       10
                   LIGHTS OFF AT 142.5 mm
DARK SLOPE =
21.1 x 10 10 cm3/sec
                     50
                                                           200
                                  100          150
                                     TIME (mm)
              Figure 69  AEROSOL COAGULATION - U. OF M.   RUN 55
                                                                        250
to
 'o
       15
                                                    19.6 x 10~10 cm /sec
                                              150
                                                           200
                                 100
                                 TIME (mm)
             Figure 70  AEROSOL COAGULATION - U. OF M.   RUN 56
                                     77

-------
      15
      10
  (0
  'o

  ~    5
  Z
            RUN NO. 57
 LIGHTS OFF
-T AT 70 min
           LIGHT SLOPE =

           0.8 x 10'10 cm3/sec  ,
                                                  19.5 x 10'10 cm3/sec
                     50
                                                              200
                                   100           150
                                       TIME (mm)

             Figure 71  AEROSOL COAGULATION - U. OF M.  RUN 57
vo
 'o
      10
            RUN NO. 59
                    LIGHT SLOPE =

                    0.5 x 10~10 cm3/sec
                                             11.1 x 10"10cm3/sec
                     50
                                                              200
                                  100           150
                                      TIME (mm)
             Figure 72  AEROSOL COAGULATION - U. OF M.   RUN 59
                                      78

-------
    15
 £  10
CO

 'o
         RUN WO 60
                                                       187 x 10~10 cm3/sec
                  SO           100          150          200




           Figure 73  AEROSOL COAGULATION - U. OF M. RUiSI 60
 £
 u
up

 'o
      0    40    80   120   160  200  240   280   320   360   400

                                 TIME  (mm )


          Figure 74  AEROSOL COAGULATION - U. OF M.  RUN 61
                                  79

-------
     28
     24
 E   20


-------
              2.9 x 10 10 cm3/sec
     0    40   80   120   160   200   240  280   320   360   400

                                  TIME (mm)


       Figure 77  AEROSOL COAGULATION - U. OF M.   RUN 64
10
'o
              10.7 x 10 10 cm3/sec
                 100
                                                      400
                       200          300

                           TIME (mm)


Figure  78 AEROSOL COAGULATION - U. OF M.   RUN 65
                                                                   500
                                 81

-------
                                                                          500
             0           100          200          300         400
                                         TIME (min)

              Figure 79  AEROSOL COAGULATION - U. OF M.  RUN 66


                                                       RUN NO. 1, MARCH 18, 1973
                                                       SO,, = 1.33 ppm
           1.6
           1.3
           1.2
           1.1
           1.0
. of.
LIGHTS OFF
             50   60    70    80    90   100

                                         TIME (MIN)

Figure 80  AEROSOL COAGULATION SO2 - AIR SYSTEM WITHOUT STIRRING - CALSPAN
                                        82

-------
           1.6
        CO  1C
         E  7'5
           1.2
           1.1
           1.0
                                                    RUN NO. 3, MARCH 19, 1973
                                                    SO2 = 0.68 ppm
                                                    LIGHTS ON
                                                   ' CALSPAN
                                 LIGHT SLOPE =
                                 1.25 x 108 cm"3 min'1
             0    42    52    62    72    82
                                         TIME (mm)
Figure 81  AEROSOL COAGULATION SO2 - AIR SYSTEM WITHOUT STIRRING -CALSPAN
           4.0
           3.6
           3.2
         "  2.8
        
-------
                RUN NO. 11, MARCH 2, 1973
           112  122   132   142   152   162   172   182  192
 Figure 83  AEROSOL COAGULATION S02 - AIR SYSTEM WITH STIRRING - CALSPAN
         1.0
      in
       'o
         0.5
              • RUN NO. 12, MARCH 23, 1973
              t SO2 = 0.44 ppm
LIGHTS OFF AT 390 min
LIGHTS ON AT 92 min  .
           92   132   172   212   252  292  332  372  412   452
                              TIME (mm)
Figure 84  AEROSOL COAGULATION SO2 - AIR SYSTEM WITH STIRRING - CALSPAN
                                     84

-------
           8.8
       „-  7.6
        E
       10
        'o
           6.4
           5.2
                  RUN NO. 13

                  SO2 = 0 39 ppm
                                                         LIGHTS OFF AT 250 mm
                                                         •  DARK SLOPE =
                        ; LIGHT SLOPE = 5.63 x 10"9 cm3/mm
             172   182   192    202  212  222   232   242   252   262   272   282  292
Figure 85   AEROSOL COAGULATION SO2 - AIR SYSTEM WITHOUT STIRRING - CALSPAN
           9.0
            8.0
       to
        'o
                 RUN NO. 14, MARCH 24, 1973

                 LIGHTS OFF  :  .   .  .

                 SO2 = 0.91 ppm       :
                                                    K = 1.28 x 10"7 cm3/mm
              0    32    42    52    62    72   82   92   102
Figure  86 EFFECT OF STIRRING ON COAGULATION IN S02 AEROSOL DECAY -CALSPAN
                                         85

-------
                 RUN NO. 16, MARCH 26, 1973
                 SO, = 0.90 ppm
             0.3
              0  40    50    60    70    80    90   100   110   120  130  140  150
                                      TIME (min!
Figure 87  AEROSOL COAGULATION SO2 SYSTEM WITH AND WITHOUT STIRRING - CALSPAN
            0.7
            0.6
        pj~  0.5
            0.3
            0.2
            0.1
RUN NO. 17, MARCH 27, 1973
SO2 = 0.48 ppm
                                   .  3.17 x 10~8 cm3/mm
               0  40    60    80   100   120   140  160   180  200   220  240
                                      TIME (mm)

           Figure 88  AEROSOL COAGULATION SO2 - AIR SYSTEM - CALSPAN

                                          86

-------
            6.0
            5.5
        1C
        'o
            5.0
            4.5
                 . RUN NO. 20, MARCH 29, 1973 i
                                K = 3.7 x 10 8 cm3/mm
              0   112   122   132   142
                       TIME (mm)
Figure 89 AEROSOL COAGULATION N02 -  PROPYLENE SYSTEM WITH STIRRING - CALSPAN
           3.0
           2.0
       up
        'o
            1.0
                   RUN NO. 21, MARCH 30, 1973
                   SO2 = 0.58 ppm
LIGHT SLOPE =
1.7 x 10"8 cm3/mm
             82     92     102      112     122     132
                                     TIME (min)
                                                         142
 Figure  90  AEROSOL COAGULATION SO2 - AIR SYSTEM WITH STIRRING -CALSPAN
                                        87

-------
              8.0
              6.0
           o
           T-
           z
              4.0
              2.0
                     RUN NO. 22, MARCH 30, 1973
                     1.51 ppm NO. + 1.5 ppm C,H_
                              £         *S O
K = 4.7 x 10~8 cm3/mm
                 86     96
                               106
                                      116      126
                                        TIME (mm)
                    136     146
                                                                    156
                                                                            166
Figure 91  AEROSOL COAGULATION NO2 - PROPYLENE SYSTEM WITH STIRRING - CALSPAN

                 RUN NO. 23, MARCH 31, 1973         !  '   !  !   :
                 SO2 = 0.56 ppm                          i               :
                 LIGHTS ON
              3.0
           up
           'o
              2.0
              1.0
                                LIGHT SLOPE =
                                1.24 x 10~8 cm3/min
                          162
                                    172
             182
          TIME (mm)
                                                        192
                                                                  202
   Figure  92  AEROSOL COAGULATION S02 - AIR SYSTEM WITH STIRRING - CALSPAN

-------
           I RUN NO. 24, APRIL 2, 1973;

           ' SO2 = 0.42 ppm

           'LIGHTS ON AT 110 mm •
        2.0
         1.9
         1.8
         1.7
         1.6
         1.5
         1.4
         1.3
                    LIGHT SLOPE =
                           8   3
                    1.87 x 10  cm /mm
            136
                       146
                                 156        166
                                       TIME (mm)
          Figure 93  AEROSOL COAGULATION SO2 - AIR SYSTEM - CALSPAN
                                                       RUN NO. 25, APRIL 4, 1973

                                                     ,  SO2 = 0.29 ppm

                                                       LIGHTS OFF   .
         3.0



     "E  2.8
      u
     up
      'o
      C  2.6



         2.4



         2.2



         2.0



         1.8
               100  110   120   130   140   150   160    170

                                         TIME (mini
Figure 94   AEROSOL COAGULATION SO2-AIR SYSTEM WITHOUT STIRRING - CALSPAN
                                         89

-------
          3.1
          2.7
       I  2.3
      in
       'o
       -  1.9
       Z
          1.5
          1.1
          0.7
          0.3
                                                        j RUN NO. 27, APRIL 6, 1973
                                                        ; SO, = 0.30 ppm
                                                         LIGHTS OFF
              122   142   162   182   202   222   242   262   282   302   322
                                      TIME (mm)
          Figure 95   AEROSOL COAGULATION SO2-AIR SYSTEM - CALSPAN
     03
     'o
9.2
8.8
8.4
8.0
7.6
7.2
6.8
6.4
6.0
5.6
5.2
4.8
4.4
4.0
3.6
3.2
2.8
2.4
                RUN NO. 28, April 8, 1973
                SO2 = 0.80 ppm
                LIGHTS OFF
               K = 7.73 x 10"8 cm3/min
                                                   \  '  '       -83
                                                       K = 12.25 x 10  cm /min
              60    70   80    90    100   110   120   130   140
                                  TIME (mm)
Figure 96  AEROSOL COAGULATION, S02 SYSTEM WITH AND WITHOUT STIRRING
                                          90

-------
            The data are presented for both lights on and lights off portions
of the experiments.  For the University of Minnesota tests,  Table VII lists
the length of time for which aerosol decay was observed when lights  were
on and off, the apparent coagulation rate constants k  for both cases, and
also any departures from linearity in the 1/N against time plots.  The lights
on decay data represents information that was taken after the peak number
concentration was attained in a normal aerosol production experiment,

            In both the Calspan and University of Minnesota tests, it may
be seen that the slope of the 1/N against time curves  suddenly increases
when the lights are  switched off (see,  e.g., Figures  65 and 82).  This  sug-
gests that generation of new particles  is occurring as long as the chamber
is illuminated resulting in a smaller number  concentration loss  rate.
Once the lights are  off, the generation  of new particles ceases and only
coagulation and diffusion to the walls are operative mechanisms of aerosol
decay.  The  lights on rate  constants as shown in  Table VII exhibit wide
variation but in most cases are a factor of 3 or 4 lower than the lights  off
values.  The values of k  in the dark exhibit significantly less scatter and
are clearly higher in the small bag than in the large bag.  Averaging all
University of Minnesota experimental  results gives a value of k   dark,
12. 5 x  10    cm /particles-sec in the large bag and 18. 0  x 10    cm  /particles-
sec in  the small bag,,   The difference between these  values can be attributed
to larger wall losses in the small bag.   It is noted in Table VII that experi-
ments  52,  65,  56,  57,  and 60  all show  upward curvature  in the 1/N against
time plots.   This  upward curvature  suggests  that wall losses are beginning
to be important.   On the average this upward curvature appears after 260 min
in the large bag and about 110 min in the small bag.  Again this indicates more
surface loss effects in the  small  bag, as would be intuitively  expected.

            The coagulation rate  constants shown in  Table VIII (page 72)
for experiments performed in the Calspan chamber have  been separated into
stirred and non-stirred cases with and without lights on.   As in  the Minnesota
experiments, the  coagulation rates are much lower (up to a factor of ten)
when the lights are  on  suggesting that additional aerosol is being generated

                                    91

-------
during this phase of the experiment.  Other characteristics of the data
are:

            (1)  Stirring vs non-stirring.  During the  lights on portion of
the experiments,  stirring did not appear to influence  the result.  When the
lights were  off, stirring resulted in a coagulation rate that was on the
average twice as great as the non-stirred  runs.

            (2)  Taking into account the particle  size ranges encountered in
these experiments ( <_ 0. 024 urn) to <_ 0. 042 |j,m), the coagulation rate is
lower than the  predicated  theoretical value (i.e.,~10 x 10     cm /sec) for
all cases  when lights are on and greater than theory by a factor of two when
lights were  off and stirring was employed. The  only time  K was about equal
to theory  was in lights off experiments  in  which  there was  no  stirring.

            These coagulation data for the Calspan chamber suggest that
coagulation  rates differ from theory whenever the lights are on or when
stirring is employed.  Experiments are still  being performed with a new
aerosol sampling system to determine when wall effects begin to influence
aerosol behavior in the large chamber.  Data from the University of Minne-
sota tests do not include stirred runs but show a similar trend in coagulation
rates when lights are on.

            Calculations of aerosol half  life were made for the large and
small University of Minnesota systems.  According to theory, the coagulation
rate constant,  k ,  measured in the dark should equal k + j-. ,  where (3 is a
wall loss  coefficient where k  is the theoretical coagulation rate  constant,
                                                     -10    3
If we assume a theoretical value of k, of about 10 x 10   cm  /sec,  fi can be
determined  according to

                              ke = V fe   '
                                                                      (11)
                                    92

-------
            The average value for N in the small bag experiments was found
                53                            43
to equal 1. 3 x 10   particles/cm , and in the  large bag 8 x 10  particles/cm  .
Substitution of these values  in into the above expression gives values for
of 10.4  x 10"5 and 2. 0 x 10"5
In terms of aerosol half life,
           - 5             -5     -1
of 10.4 x 10   and 2. 0 x 10   sec   for the  small and large bags respectively.
                               t1/2  =  In 2/p                         (12)
gives values of 1.85 and 9.6 hours for the small and the  large bags,  respec-
tively.  (A value of 14.25 hours is obtained for the Calspan chamber  if  the
average coagulation rate constant is used from the dark  cases without stirring.
Statistically,  however, there is too much scatter in  the limited data  to allow
this  calculation to be considered  valid.)  These numbers represent the time
that  would be required for the number concentration to be  reduced to one-half
through wall losses acting alone.  Additional data gathered during the coming
year will  be used to refine  these  calculations.  For aerosol volume loss,  the
half  lives will be longer since the large particles (which contain most of the
volume) will diffuse to the wall more slowly than small particles.

            2. Linear Aerosol Volumetric Growth Curves

            Clark (1972) has suggested that departures from  linearity in the
volume vs time curves for  the SO., photochemical system indicate the pre-
sence of wall loss effects.

            The theoretical basis for this hypothesis may be understood in
terms  of a simple model.   It is based on  two assumptions:

            (1)  When the lights are on, the rate of aerosol volume production
is  constant and
            (2)  Wall losses are due  to diffusion  of aerosol to the  walls.
Diffusion  processes are first order so that the rate of loss of volume to
the walls  will be proportional to the  volume itself.
                                    93

-------
            A differential equation which describes the process may then be
written,  giving
                                dV
                                dF
                                    =  R  - aV                          (13)
where  R is the volume rate of production of new aerosol and a is the wall
loss coefficient.  Solution of this equation with the boundary condition V  =  0
at t = 0 gives
                              V = 5-   (1 - e"Qt)                        (14)

For small values  of at this may be expanded to give

                              V = Rt or -^r  =  R                        (15)
                                        dt

so that initially linear growth is expected, however,  as at increases, the
rate of volume growth decreases  and the volume eventually  approaches a
constant value at large values of at.   Departures of the  volumetric growth
from linearity depend on the value of at and do not depend on R.

            Figure 97 shows the general shape of the volumetric growth
curve predicted by this model as  well as the no loss volume growth curve.
Here dimensionless volume,  Va/R,  is plotted against dimensionless time,
at.  For small values of  at the curves with and without losses are quite
close to  one another and  diverge as at increases.  The curves diverge
gradually, but there is no sudden departure from linearity.  This suggests
that experimentally it might be difficult to detect downward  curvature of
the volume against time plot unless at is relatively large.  The  coagulation
                                                   -5             - 5     -1
experiments described above gave p values of  2 x 10    and 10.4  x 10   sec
for the large and small bags,  respectively.  The parameter p is analagous
to a except that it is for number loss rather  than volume loss.   For a
monodisperse aerosol, a and (3 are equal.  That is not the case  here and
the aerosol volume is weighted more heavily toward larger  particles which
diffuse more slowly to the walls.   Consequently, a will be smaller than  p.
                                    94

-------
               0.9
               0.8
               0.7
             tr
             8
               0.6
             2
               0.4
             Z
             O
             to
               0.3
               0.2
               0.1
                            NO LOSSES, Voc /R = 
-------
                                  Table IX

                EXPERIMENTS TO DETERMINE THE LENGTH OF THE

                     LINEAR VOLUME PRODUCTION PERIOD
RUN
NUMBER
dv/dt
fj.m3/cm3 hr
TIME LINEAR
minutes
Mm
COMMENTS
LARGE BAG
18
19
20
22
24
25
27
65
66
67
0.87
1.38
2.36
6.27
22.9
16.7
0.39
1.00
5.63
9.26
280
160
115
85
> 60
> 60
370
240
> 170
180
0.060
0.046
0.045
0.045
> 0.060
> 0.053
0.065
0.055
0.10
0.080







C3H6-NO
OUT OF WAA SIZE RANGE
CsHe NO GROWS OUT OF
SIZE RANGE OF WAA
SMALL BAG
55
58
60
3.98
10.9
2.21
> 140
140
> 160
> 0.055
0.090
> 0.040



         NOTES:   dv/dt DENOTES THE SLOPE OF A PLOT OF AEROSOL VOLUME AGAINST TIME.
                TIME LINEAR IS THE LENGTH OF THE LINEAR PORTION OF THE PLOT. DoV IS
                THE PARTICLE VOLUME MEAN DIAMETER AT THE END OF THE LINEAR
                GROWTH PERIOD


that suggests itself is that the non-linearity appeared when the aerosol grew

out of the size range of the instrument.   This  appears to be the case for

Run 67 as was explained above.   Close examination  of the  size distributions

show that this  is also the case for runs 66 and 58.  Note that all of these

runs show non-linearity at rather large volume mean diameters.  The

behavior of the other  runs, however,  cannot be explained  so easily.   In

fact, the only possibility that immediately presents  itself  is an error in

the calibration constants for  the  WAA.  These constants are in the process

of being  reevaluated and will hopefully shed further  light on the problem.
                                    96

-------
            Comparing small and large bag experiments also show some
unusual results.  Experiments 20  and 55 have nearly equal volumetric
production rates, but the linear growth period in the small bag  is more
than 160 min while that in the large bag is 115 min, this trend is exactly
opposite from that expected from simple theory.  Run 55 in the small bag
has a volumetric conversion rate which falls  between runs 20 and 66 in the
large bag.  The  linear time of  >140 min also  falls between the values of 115
and  > 170 found in  runs  20  and  66, respectively.  Again the shorter working
period expected  in the small bag is not apparent in the volume production
curves.

            Something other than wall losses  appears to be producing the
departures from the linear volumetric production curves. This effect may
be instrumental  or it may be involved in the physics and chemistry of the
SO^, -photooxidation system. In any case, departures from linearity  in the
volumetric growth curves cannot be used as the  sole tool for assessing
chamber wall loss at the present time.  The most reliable available tech-
nique for  assessing the  importance of wall losses is based on the coagulation
experiments.  With refinement the coagulation results should yield useful
information about volume loss  as well as number loss.

            3.  Chamber Reactivity Tests

            At the University of Minnesota several experiments were per-
formed to determine the influence of  the condition of the charcoal in the
scrubber  and the surface of the Teflon bag on photochemical aerosol pro-
duction.   Three  basic conditions were investigated; aerosol formation  in
the original large bag with the  original charcoal in the scrubber,  both  of
which had been used in the 48 experiments; aerosol formation in the old
bag with fresh charcoal; and aerosol  formation in the new large bag with
the fresh  charcoal in the scrubber.  The  results of these experiments  are
summarized in Table X. Here two types of behavior, maximum nuclei
concentration and dark growth,  were monitored at two different relative
humidities for  each chamber condition.
                                    97

-------
                                 Table X
                    CHAMBER REACTIVITY EXPERIMENTS
RUN
NUMBER
49
50
52
53
54
61
63
64
SYSTEM
OLD BAG-OLD CHARCOAL
OLD BAG-OLD CHARCOAL
OLD BAG-NEW CHARCOAL
OLD BAG-NEW CHARCOAL
OLD BAG NEW CHARCOAL
NEW BAG-NEW CHARCOAL
NEW BAG NEW CHARCOAL
NEW BAG-NEW CHARCOAL
[so2i
ppm
0.27
0.27
0.23
0.23
0.27
0.21
0.34
0.29
RELATIVE
HUMIDITY
%
23
58
30
30
j58
28
26
58
CNCMAX
5 3
10 particles/cm
1100
1020
350
330
720
730
500
920
DARK GROWTH
YES
YES
NO
SLIGHT
YES
YES
YES
YES
            The least reactive chamber condition as indicated by the least
dark growth and the lowest peak nuclei concentration was the old bag used
with fresh charcoal.  This was particularly true with respect to the maxi-
mum nuclei concentration which was approximately halved.  This combination
proved to be less reactive than the new chamber with new charcoal which
suggests that some sort of chamber conditioning process takes place.  Some
conditioning also seems to have  occurred during the series of runs performed
in the Calspan  chamber during the joint workshop.  In those tests, the
volumetric  conversion  rate steadily decreased for  the first nine or ten
experiments as the chamber appeared to become conditioned to the SO-,
system.   Once  achieving  a fairly low  level only the introduction of new gases
caused any  significant increase in the volumetric conversion rate.  More
experiments of this  type will be  performed after the new lighting system is
completed in the  Calspan chamber and the new teflon bag at the University
of Minnesota has had additional time to age.
                                    98

-------
V.      SUMMARY AND CONCLUSIONS

        During the first program year, emphasis was placed on examining
aerosol behavior in the relatively simple SO?-clean air system using
                                                                    -1
chambers of widely different surface-to-volume ratios (i.e.,  O.Z3 ft  ),
        -1             \                         3
0. 65 ft   and 1. 31 ft   )„  At Calspan a 20, 800 ft  aerosol chamber was
employed for these tests while smaller systems involving 600 ft  and 90 ft
teflon  bags were used at the University of Minnesota.   A limited  number
of experiments were also performed using the propylene-NO  system.
                                                            X
        Substantial effort was directed toward upgrading and testing the
Calspan chamber and its support facilities.  Improvements included installa-
tion of chamber lighting and air purification  systems, resurfacing of the
chamber  walls  with a chemically resistant fluorepoxy polymer and installa-
tion of suitable gas analysis instrumentation. Numerous tests were performed
to evaluate wall effects and establish overall chamber background reactivity.
Additional modifications to the present lighting system are being made as a
result  of  tests which showed a  k, ~ 0.05 min  or approximately 10% of noon
day  sunlight.   The improved system is expected to provide a five-fold
intensity  increase in k, to  *s 0. 24 min

        Greater control of  chamber  conditions was available in the 600 ft
University of Minnesota chamber.   Although  stirring could not be employed,
fairly  precise  temperature and humidity control could be achieved in the
experiments.  Tests were  designed to study  the formation mechanisms of
aerosols  in the SO,-clean  air system and  to  a lesser extent in the NO
                  £                                                  x
propylene system.  The effects of relative humidity on aerosol formation
as well as the  influence of  bag  size  on particle growth and decay  was also
studied.

        Although a number  of experimental facilities were encountered during
the  testing period, the overall  utility of the large chamber was convincingly
demonstrated.  Evidence to date points to chamber working times in excess
of 11 hours before wall effects  begin to influence test results.  Additional
experiments during the coming year should establish the useful working
                                    99

-------
time available in the large chamber.  Coagulation experiments performed
at the University of Minnesota point to effective working times of four to
six hours in the 600 ft  chamber and about two hours in the 90 ft  chamber.
Somewhat longer times are indicated from the linearity of the  volume con-
version rates.

       An important conclusion derived from  the first year test results
is that aerosol formation presents an extremely sensitive  indicator of
chemical reactions  that occur in a smog chamber.  In fact, the reaction
threshold as indicated by the onset of Aitken nuclei formation in SO-, photo-
oxidation cannot be  detected by present gas analysis instrumentation.  It
has been shown that the fraction of SO-, involved in the reaction is extremely
small even  though particle concentrations often exceed 10  cm   .  In this
respect, aerosol formation has  also  been  shown to be a sensitive indicator
of impurities  existing in the chamber at concentration levels far below gas
analysis detection limits.   Such highly sensitive contaminant effects occasion-
ally result in seemingly difficult to explain aerosol behavior patterns.  At
this point no attempt has been made to provide a completely consistent
account of all the experimental data presented in this report.

       It is concluded that the SO-, photooxidation  test system  studied in this
first year Calspan-University of Minnesota program has provided data on
aerosol behavior that is generally consistent with  the accepted understanding
of the reaction system.  A relatively simple aerosol formation model for
SO-, photooxidation is presented in this report.  The observed  number concen-
tration, volume and surface growth rates  correlate satisfactorily with aerosol
behavior patterns predicted by the model without apparent wall effects causing
significant deviations.  Particle number decay as  predicted from coagulation
theory leads to the conclusion that a  relatively long chamber reaction time
is available for experimentation.  Precise definition of chamber  working
times and evaluation of aerosol behavior in more complex HC-NO  systems
are objectives of the coming year program.
                                    100

-------
                              REFERENCES
Altshuller,  A. P., et. al. ,  1967:  Environ. Sci. Tech., p. 889.

Bray,  W. H.,  1970:  Water  Vapor Pressure Control At Aqueous Solutions
       of Sulfuric Acid,  J.  of Materials, Vol.  5, No.  1,  p.  Z33-248.

Clark, W. E., 1972 Ph. D. thesis,  University of Minnesota, Measurement
       of Aerosol Produced by the Photooxidation of SO-, in Air.

Demerjian, K. L., J. A. Kerr,  and J.  G. Calvert, Advan. Environ. Sci,
       Tech., Vol. 3, Wiley-Interscience, N. Y.

Doyle, G.  J.,  1961:  Self Nucleation in  the Sulfuric  Acid Water System,
       J. Chem.  Phys., Vol. 35,  No.  3,  p.  795.

Friend, J.  P.  et. al, 1973:  On  the Formation of Stratospheric  Aerosols,
       J. Atmos. Scio, Vol. 30, p. 465-479.

Fuchs,  N. A., 1964:   The Mechanics of Aerosols, The McMillan Co, ,
       New York,  N. Y.

Gorden,  R. J., 1967: Pilot Study of Ultraviolet UV Radiation in Los
       Angeles,  J. S.  Nader, El., PHS Pub. No. 999-AP-38.

Skala,  G. F.,  1963:  A New Instrument for the Continuous Measurement of
       Condensation Nuclei, Analytical Chem. , Vol.  35, p. 702-706.

Spindt,  R. S., Gulf Research &  Devel. Co.,  Pittsburg,  Pa., private
       communication.

Whitby, K.  T., et. al. ,  1972; The Minn.  Aerosol Analyzing System Used
       in the  L.  A. Smog Project, J. of Coll.  &  Interface Sci. , Vol. 39,
       No.  1.
                                    101

-------
                                   TECHNICAL REPORT DATA
                            (Please read Instructions on the reverse before completing)
1  REPORT NO,
  EPA-650/3-73-002
                                                           3. RECIPIENT'S ACCESSION-NO.
4 TITLE AND SUBTITLE
  DETERMINATION OF THE  FORMATION MECHANISMS AND
  COMPOSITION OF PHOTOCHEMICAL AEROSOLS
                                      5 REPORT DATE
                                        December 1973
                                                           6. PERFORMING ORGANIZATION CODE
7 AUTHOR(S)
  W.  C.  Kocmond, D.
  K.  L.  Demerjian
                                                           8. PERFORMING ORGANIZATION REPORT NO.
i.  Kittelson,  J.  Y. Yang, and
                                        NA5365-M-1
9. PERFORMING ORG \NIZATION NAME AND ADDRESS
  Calspan Corporation
  P.O.  Box 235
  44S5  Genesee Street
  Buffalo, New York 14221
                                      10. PROGRAM ELEMENT NO.

                                         1A1008
                                      11. CONTRACT/GRANT NO.

                                        68-02-0557
 12. SPONSORING AGENCY NAME AND ADDRESS
  Environmental Protection  Agency
  National Environmental  Research Center
  Research Triangle Park, North Carolina 27711
  and  Coordinating Research Council, New York, NY
                                                           13. TYPE O.F REPORT AND PERIOD COVESED
                                                             Interim  6/72  - 6/73
                                      14. SPONSORING AGENCY CODE
15. SUPPLEMENTARY NOTES
16. ABSTRACT
    Calspan Corporation  in  collaboration with the  Particle Technology Laboratory of the
University of Minnesota is engaged in a study of  the  formation mechanisms  and  growth
processes of photochemical aerosols.
    Experiments are being conducted in Calspan's recently completed 20,800  ft   smog
chamber and also in University of Minnesota's 600 ft3 and 90 ft^ chambers.   In the
work reported here emphasis  is placed on studying aerosol behavior in the  S02  system
and chamber effects on  aerosol behavior.  Future  work will emphasize aerosol  formation
in representative hydrocarbon-NOx systems, with and without SO,., present.   Effects of
chamber size, relative  humidity and artifical nuclei  on aerosol behavior will  be
investigated.
                                KEY WORDS AND DOCUMENT ANALYSIS
                  DESCRIPTORS
  sulfur dioxide
 smog chamber
 hydrocarbon-NO
 chamber effects
 photochemical aerosols
 photochemical particles
 sulfuric acid
                         b.IDENTIFIERS/OPEN ENDED TERMS  C. COS AT I Field/Group
13. DISTRIBUTION STATEMENT

Release Unlimited
                         19. SECURITY CLASS (ThisReport)
                                                                         21. NO. OF PAGES
                                              20. SECURITY CLASS (This page}
                                                    22. PRICE
                                                      110
EPA Form 2220-1 (9-73)
                                            102

-------