xvEPA
              United States
              Environmental Protection
              Agency
              Environmental Sciences Research  EPA-600/4-78-044
              Laboratory           August 1978
              Research Triangle Park NC 27711
              Research and Development
A Pilot Study on
Dispersion Near
Roadways
₯•:

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                RESEARCH REPORTING SERIES

Research reports of the Office of Research and Development, U S. Environmental
Protection Agency, have been grouped into nine series. These nine broad cate-
gories were established to facilitate further development and application of en-
vironmental technology.  Elimination of traditional grouping  was  consciously
planned to foster technology transfer and a maximum interface in related fields
The nine series are:

      1   Environmental  Health Effects Research
      2   Environmental  Protection Technology
      3.  Ecological Research
      4.  Environmental  Monitoring
      5.  Socioeconomic Environmental Studies
      6.  Scientific and Technical Assessment Reports (STAR)
      7.  Interagency  Energy-Environment Research and  Development
      8.  "Special" Reports
      9.  Miscellaneous Reports

This  report has been assigned to the ENVIRONMENTAL MONITORING series.
This  series describes research conducted to develop new  or improved methods
and  instrumentation for the identification and quantification of environmental
pollutants at the lowest conceivably significant concentrations.  It also includes
studies to determine the ambient concentrations of pollutants in the environment
and/or the variance of pollutants as a function of time or meteorological factors.
This document is available to the public through the National Technical Informa-
tion  Service, Springfield, Virginia  22161.

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                                        EPA-600/4-78-044
                                        August 1978
A PILOT STUDY ON DISPERSION  NEAR  ROADWAYS

                       by
               William B. Petersen
        Meteorology and Assessment Division
    Environmental Sciences Research Laboratory
  Research Triangle Park, North Carolina 27711
    ENVIRONMENTAL SCIENCES RESEARCH LABORATORY
       OFFICE OF RESEARCH AND DEVELOPMENT
      U. S. ENVIRONMENTAL PROTECTION AGENCY
   RESEARCH TRIANGLE PARK, NORTH CAROLINA  27711

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                              DISCLAIMER
     This report has been reviewed by the Environmental Sciences Research
Laboratory, U.S. Environmental Protection Agency, and approved for
publication.  Approval does not signify that the contents necessarily
reflect the views and policies of the U.S. Environmental Protection
Agency, nor does mention of trade names or commercial products constitute
endorsement or recommendation for use.
                         AUTHOR'S AFFILIATION
     The author, William B. Petersen, is on assignment with the U.S.
Environmental Protection Agency from the National Oceanic and Atmospheric
Administration, U.S. Department of Commerce.
                                     n

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                               ABSTRACT
      High frequency wind fluctuation data from the General  Motors Sulfate
Dispersion Experiment were used to estimate the dispersion near roadways.
The standard deviations of the wind direction and the elevation angle
were computed for six averaging times for three half-hour periods when
the winds were nearly parallel to the test track.  The EPA HIWAY model
was modified to use these fluctuation statistics directly to estimate
dispersion.  Results from analysis show that model  performance was improved
for parallel  wind conditions when the fluctuation statistics of the wind
were used to estimate dispersion.  The results also show that model estimates
are most sensitive to the vertical dispersion parameter.  Indeed, concentra-
tions seem to be insensitive to the horizontal dispersion parameter.

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                                  CONTENTS





Abstract	iii



Figures and Tables	vi



Acknowledgments 	 vii



     1.   Introduction  	 1



     2.   Data Base	3



     3.   Analysis of the Data	5



     4.   Summary   	17



References	18



Appendix





     A.   Determination of the  stability class



          from the Richardson Number	19

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Number
  1
  2
  3
  4
  5
  A-l
                       FIGURES

Orientation of test track and perpendicular
distances of the meteorological  towers  from
the center of the test track 	
a  and DZ computed  from a  and a  respectively
                                                        Page
                                                         4
                                                         9
SFK concentrations (ppb) 	    11
                                     	    14
                                     	    16
Measured SFC versus estimated SFC
           b                    o
Measured SFg versus estimated SFg
                                         -1
Turner stability class as a function of L   and z
                                                         21
                              TABLES
Number                                                           Page
  1       a  and a  for Different Averaging Times	    8
  2       Wind Direction and Wind Speed During the Three
          Half-Hour Periods   	
  3       Stability Class for Each Half-Hour Period  	   12
  4       Regression Analysis  	   15
  5       Comparison of Model Estimates  	   17
  A-l     Stability Class as a Function of L"   	21
                                   VI

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                          ACKNOWLEDGEMENTS

     The author wishes  to  express  his appreciation to Bruce Turner and
John Irwin for their helpful  discussions and  review; to John Ashley and
Tim Christiansen for their computer  programming assistance; and to Caryl
Whaley and Joan Emory for  their  aid.
                                   VII

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                          1,   INTRODUCTION
     This paper discusses the results of a pilot study on data  ob-
tained from the General Motors Sulfate Dispersion Experiment (Cadle et
al, 1976).  The purpose of this study is to investigate and develop
methods for estimating dispersion near roadways.  A major objective of
this study is to investigate the performance of the EPA HIWAY model
(Zimmerman and Thompson, 1975) using dispersion estimates from  the
fluctuation statistics of the wind.
     The HIWAY model does not use the infinite  line source approximation
to estimate concentrations downwind of a line source.   Concentration
estimates are made by numerical integration of  the Gaussian plume point
source equation.  Thus, concentration estimates are functions of the
horizontal and vertical dispersion parameters (a  and  o ). Pasquill
(1976) stated that the horizontal dispersion parameters (Pasquill-
Gifford (PG) dispersion curves) are most appropriate to a 3-minute
sampling time.  One would expect that for longer sampling times, say
1  hour, a  would increase and thus increase dispersion.
         «/
     For the case where the wind is  near perpendicular to the roadway,
the infinite line source equation is a good approximation.  The effects
of crosswind dispersion are not important since the crosswind dispersion
from one segment of the line is compensated by  dispersion in the oppo-
site direction from adjacent segments.  However, when  the winds are near
parallel to the roadway, it is no longer appropriate to assume  that  the
dispersion from one point is compensated by that of adjacent points.   In
the past it has been observed that HIWAY overestimates concentrations
when the winds are near parallel  to  the road.  If the  overestimation of
HIWAY is due to a conservative estimate of 0 ,  it should be most noticeable
during parallel wind conditions.

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     The General Motors (GM) Sulfate Dispersion Experiment provides an
excellent data base for investigating dispersion near roadways.  Not only
was this a controlled roadway study, but also three components of the wind
were measured and recorded every second at 20 locations across the
test track.  This high frequency wind data is the most valuable in estima-
ting dispersion.  The data used in this pilot study represent three half-
hour periods during which the winds were nearly parallel with the the road.
While the analysis of the data from the three periods gives valuable
insight into the dispersion during parallel wind conditions, the major
function of this paper is to set forth the techniques that will be
used to analyze the whole data set.  The entire data set consists of
about 60 half-hour periods.  A brief description of the GM data follows
in the next section.

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                             2,   DATA BASE
     The data used in this analysis is a small  part of a data set col-
lected at Mil ford Proving Ground by General Motors during the sulfate
dispersion experiment.  The experiment was performed during October
1975.  The data used in this paper consists of three half-hour periods
on October 24.  A fleet of 352 catalyst-equipped automobiles were driven
around a 10 km narrow oval track.  At the sampling locations, about
halfway down the track, the cross section simulated a 4-lane road with a
median.  Eight vehicles were equipped to release sulfur hexafluoride
(SFfi) as a tracer.  The SFfi was sampled at 20 locations in the vicinity
of the test track (see Figure 1). SFg samplers were located on towers
1  through 6 at heights of 0.5, 3.5, and 9.5 m.   Samplers were also located
on stands 7 and 8 at 0.5 m.  Gill u-v-w anemometers were on towers 1 through
6 at heights of 1.5, 4.5, and 10.5 m.  On stands 7 and 8 the anemometers were
at 1.5 m.  The meteorological data consisted of 1-second values of the u-v-w
components of the wind from the 20 anemometers.  The sampling time for SFg
was 30 min.  For a more detailed discussion of the experiment and the data
set, see Cadle et al.  (1976), and EPA (1976).

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                                 TOWER 1(
                                              42.7m
                                 TOWER 2Q—T
LANE1
LANE 2
                                           14.6m
                                 TOWER 3O-
                                           16.5m
                                                                     25.4m        11.8m
LANE 3

LANE 4
                                 TOWER'
                                 TOWER5(
                                 TOWER 6(j-
                                              27.7m
                                                I
                                                  42.7m
                                                     62.7m
                                 STAND 7
                                                        112.7m
NORTH
                                 STAND 8
     Figure 1. Orientation of test track and perpendicular distances of the meteorological
     towers from the center of the test track.

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                     3,   ANALYSIS OF  THE DATA
     The data chosen for this pilot study were three half-hour periods
on October 24.  These periods were chosen because the winds  were  within
5° of parallel to the test track.   The fluctuation statistics  a.  (standard
                                                               y
deviation of the horizontal  wind direction) and a. (standard deviation
                                                 
of the vertical wind direction) were calculated from the wind  data
collected by the anemometer on Tower 1 at the 4.5 m level  (see Figure
1).
     The standard deviation of the wind direction was calculated  from
the u and v components  of the Gill anemometer.   The mean wind  direction
i is given by,
                         6  -
                              n
                              E
where 9. = arctan ()
To avoid the discontinuity at 360°, each 9..  was  assumed to be  a  unit
vector with components u and v.  e is now defined as,
                            ~n  * ~1
                             E  u.
                 e = arctan
 Defining  e  in  this way  eliminates  the discontinuity problem and avoids
 the effect  of  the wind  speed  on  the mean wind direction,  a   is now
                                                           9
 given  as,
                                     -nV2
                            n
                            E
                           1=1
i)

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It is apparent that the maximum deviation between 9. and e is 180°.
Therefore, if the absolute value (ABS) of the difference (e. - e)
was greater than 180°, the deviation is equal to 360-ABS(e.-e).
     The standard deviation of the vertical wind direction was computed
from the three components of the wind field.  The horizontal wind speed
Vu is defined as,
 n
                         VH - (u2 + v2)1/2
                         'H
The mean elevation angle $ is given as,
                      = arctan

                                 n  A
                                 z  VH
                                1=1  Hi
where w is the vertical component of the wind.
unit vector.  aA  is given as,
                                      ~~ 1/2
                            s (<(>, -
                                                w and Vn are components of a
                                n
     The relationship between the horizontal dispersion parameter, a ,
and  aQ was suggested by Hay and Pasquill  (1957, 1959).
                         a   (x) = a      x,
                          J         T,S
                                                               (1)
where;  x =  BUS
        3 =  ratio of the Lagrangian to the Eulerian time scales,
        u =  mean wind speed,
        s =  averaging time,
        T =  sampling time.

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The relationship between a  and a, is not as well understood as that for
                          Z      cf>
the horizontal dispersion.  In this analysis the following relationship
was used to estimate a  :
                         a_(x) = V   x.                        (2)
                          f-        T j D

     For each half-hour period an and a, were calculated for different
                                o      

that the dispersion during these three half-hour periods is that typical of B-C stability. The EPA HIWAY model was modified for this analysis to make concen- tration estimates from the dispersion parameters determined from a. and h a,. Both a and a are assumed to have the form of ax , where a and b y z are constants determined from the data. For example, a. is determined o for six averaging times. 0 and x are then calculated using Equation (1) •J for each of the six averaging times, a is then known for six downwind distances. The constants a and b are calculated for each interval in the following way:


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a. and b. are used to determine a  when the downwind distance is between
 J      J                        J
the intervals x. and x/.+1% .   There are five intervals for which a and b
are determined.  For downwind distances less than that given by the 5-
second averaging times, a-| and b-j are used to determine a .  For x greater
than that given by the 90-second averaging time,  ag and
                                                           are used as the
appropriate constants.  Similarly, constants (c and d) are determined for
az(x).
     The initial dispersion parameters a   and a   used in the modified
HIWAY model were not changed.   The appropriate victual distances nec-
essary to account for the initial dispersion are:
                                                            i
                       1
Where:
               0   = 3 m,
                yo
                   = 1.5m.
Finally, the equations used to estimate 0  and a  are
°y (XJ} =
                            (x
                                    b,
                                  x)
                  (x.) = c. (x_ + x)
                                    d.
where x. = x  + x or xz + x in the j
                                    .th
                                       interval.
     The modified HIWAY model was used to estimate SFC concentrations at
                                                     D
the 20 sampler locations (See Figure 1).  In Figure 3 are scatter plots
of measured SFC concentrations versus model estimates for the three
              b
half-hour periods.  Figure 3 also contains a composite of all the data for
the three periods.  The dashed lines on the plots are least squares fits
to the data with the regression information in the upper left-hand
corner of the plot.  Table 2 shows that the mean wind speed and direction
were steady during this time.
                                      10

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                PERIOD ONE
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M= 0.904

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N=20




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                                                             PERIOD TWO
     0)234

         ESTIMATED SFg CONCENTRATION
                                             z
                                             o
                                             <
                                             CC
                                             LL.
                                             CO
                                             a
                                             CO
                                             <
B =-0.732
M= 1.027 i
R= 0.948
N=20



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                                                         12345

                                                       ESTIMATED SFe CONCENTRATION
               PERIOD THREE


a
LU
OC
3
C/l

LU
B =-0.309
M= 0.967
R= 0.897
N- 20




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                                                             ALL PERIODS
            12345

          ESTIMATED SFe CONCENTRATION
                                             <
                                             oc
                                             o
                                             o
                                             to
                                             CO
                                             <
                                                   B =-0.404
                                                   M= 0.875
                                                   R= 0.892
                                                  0      2      4      6      8      10

                                                      ESTIMATED SFe CONCENTRATION
         Figure 3.  SPQ concentrations (ppb). B, M, R, N in the plots are the intercept
         slope, correlation coefficient, and number of data points respectively.
                                          11

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               TABLE 2.  WIND DIRECTION AND WIND SPEED DURING
                         THE THREE HALF-HOUR PERIODS

Half-hour periods
1
2
3
Wind direction
182
183
175
Wind speed )m
2.5
2.2
2.9
sec"1)




     The improvement in the performance of HIWAY can be shown by analyzing
concentration estimates using three different approaches to estimating
atmospheric dispersion.  The approach described in Turner (1964) uses cloud
cover, ceiling height, and wind speed to determine the stability class.   The
stability class for each half-hour period was determined using the wind
speed at the experimental site and the observations of cloud cover and ceil-
ing height at 3-hour intervals for Flint, Michigan (about 44 km north of
the site).  The Richardson Number measured at the site was used subjectively
to determine how fast the atmospheric stability was changing.  The stabili-
ty was never allowed to change more than one class from one half-hour period
to the next.  Another approach used to determine the stability class was
that suggested by Golder (1972).  Solder showed an empirical relationship
between the Richardson Number, roughness height and the stability class.
Appendix A contains a more complete description of how Golder1s technique
was applied to this data set.  The stability class for each half-hour  period
was determined by the two techniques mentioned above is shown in Table 3.

           TABLE 3.  STABILITY CLASS FOR EACH HALF-HOUR PERIOD

Stability class
determined from
Turner (1964)
Golder (1972)

First
E
F
Half-hour period
Second Third
D D
F F
                                      12

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     Figure 4 is a scatter plot of measured SFg concentration versus
model estimates using HIWAY with the three different techniques to estimate
dispersion.  For the data plotted as squares and stars, the stability class
was determined from the Richardson Number and the Turner (1964) approach,
respectively.  In both cases a  and a  came from the PG curves once the
stability class was determined.  In the third data set, plotted as diamonds,
the dispersion was estimated from a. and a, using Equations (1) and (2).
                                   o      y
Table 4 shows a summary of the regression analysis of the three sets of data.
The slope of the regression line was significantly improved using on-site
estimates of dispersion.  However, the correlation coefficient was not
improved.
     Using two different sets of dispersion parameters in HIWAY, then analy-
sing the results from model estimates, is analogous to using two different
models.  When two models are compared with the same measured concentrations,
one has to be very careful about statistical statements concerning the
regression results.  For the case in which both models are compared with the
same measured concentrations, the deviations from the regression lines could
be correlated.  Thus for the same measured concentrations, it is not appro-
priate to use a T-test, formed using a pooled variance in the standard way,
to test the difference between the regression slopes from the two models.
A suggested way to overcome this is to split the data into two sets (private
communication from R. J. Hader, N. C. State University, 1977).  The two
data sets should have the same characteristics.  One approach to insure that
the range of concentration is the same for both data sets is to rank the
measured concentrations and assign every other value to a different data set.
One set would then be used for comparison by one model and the other set with
the other model.  A T-test could then be used to test for the significant
difference between the two slopes.  This approach was not used for this pilot
study because of the limited size of the data set.  However, this approach
will be pursued with further analysis of the GM data.
     Four data points (squares) were not plotted on Figure 4.  Although
the concentration estimates fell outside the boundaries of the plot, they
were used in the regression analysis.
                                      13

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   10
CJ
Z
o
o
CO
                               4             6

                       ESTIMATED SFe CONCENTRATION, ppb
10
  Figure 4.  For the data plotted as squares the stability class for each half-hour
  period was determined from the Richardson Number.  For the data plotted
  as stars the stability class was determined from the Turner (1964) classifica-
  tion scheme.  For the data plotted as diamonds the dispersion parameters ay
  and az were determined directly from  OQ and  o0.
                                     14

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                       TABLE 4.  REGRESSION ANALYSIS
Type of dispersion
Slope
               Correlation
Intercept	coefficient
Dispersion
  parameters from
  Equations 1 and 2
PG curves
  stability class
  from Turner (1964)
PG curves
  stability class
  from Richardson No.
 0.875
 0.536
 0.268
-0.404
-0.087
 0.065
0.892
0.923
0.890
     As suggested in the introduction, concentrations in the vicinity of a
line source should be most sensitive to crosswind dispersion when the winds
are parallel to the line source.  In order to investigate this, concentra-
tion estimates, using a modified HIWAY model, were made using 
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                             4            6

                      ESTIMATED SF6 CONCENTRATION, ppb
10
Figure 5. For the data plotted as squares oy was determined from OQ and az
from the PG curves.  For the data plotted as stars ay and az were determined
from the PG curves.  For data plotted as diamonds ay and az were determined
from OQ and a0 respectively.
                                  16

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                TABLE 5.  COMPARISON OF MODEL ESTIMATES
                Measured           Model          Ratio of
 	concentration (ppb)     estimate (ppb)  model/measured
 Stability class
   from Richardson No.       5            18.41             3.68
 Stability class
from Turner (1964)
Dispersion parameters
from Equations (1)&(2)
5
5
9.49
6.18
1.90
1.24

                                 4,  SlfMARY

     The major objectives of this pilot study were to develop the
methodology to estimate the dispersion parameters from the fluctuation
statistics of the wind using a small sample of the GM data, and to
modify the HIWAY model to incorporate these dispersion parameters into
the model computations.  To that end the pilot study has been a success.
     The following conclusions can be made as a result of the analysis
of the data used in this pilot study: (1) during conditions when the winds
are nearly parallel to the test track, concentrations are less sensitive
to crosswind dispersion then expected; (2) dispersion parameters determined
from the fluctuation statistics of the wind have a shape similar to the
PG curves for downwind distances up to 500 m; (3) the fluctuation statistics
of the wind indicate that the atmosphere near the ground was more dispersive
than the stability class indicated; and (4)  the performance of the model
was significantly improved using the dispersion parameters determined from
wind fluctuations.
                                     17

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                              REFERENCES

Cadle, S. H., D.  P.  Chock,  J.  M.  Heuss,  and  P.  R.  Monson,  1976:
  Results of the General  Motors  Sulfate  Dispersion Experiment.   GMR-
  2107.  General  Motors Corporation,  Warren,  Mich.   178  p.

Golder, D., 1972:  Relations Among Stability Parameters  in  the
  Surface Layer.   Boundary-Layer Meteorology 3, 47-58.

Hay, J. S., and F.  Pasquill, 1957:  Diffusion from a fixed  source at
  a height of a few hundred feet in the  atmosphere.   J.  Fluid Mech.,
  2^ 299-310.

Hay, J. S., and F.  Pasquill, 1959:  Diffusion from a continuous  source
  in relation to the spectrum and scale  of turbulence,  pp  345-365
  in Atmospheric Diffusion and Air Pollution, edited by  F.  N. Frenkiel
  and P. A. Sheppard, Advances in Geophysics, 6, New York,  Academic
  Press, 471 pp.

Pasquill, F., 1976:   Atmospheric Dispersion  Parameters  in  Gaussian
  Plume Modeling, Part II.   Environmental  Monitoring Series.  EPA-
  600/4-76-030b.   US EPA, Research Triangle  Park,  NC 44 p.

Selected EPA Research Papers, 1976:  The General Motors/Environmental
  Protection Agency Sulfate Dispersion Experiment.  EPA-600/3-76-035.
  US EPA, Research Triangle Park, NC  146 p.

Turner, D. B., 1964:  A Diffusion Model  for  an Urban Area.   J.  Appl.
  Meteor. 3, 83-91 .

Zimmerman, J. R., and R.  S. Thompson, 1973:   User's Guide  for HIWAY,
  A Highway Air Pollution Model.  EPA-650/4-74-008.  US  EPA,  Research
  Triangle Park, NC  59 p.
                                     18

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             APPENDIX A,
DETERMINATION OF THE STABILITY CLASS
     FROM THE RICHARDSON NUMBER
                   19

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     The Richardson Number (Ri) was calculated for each half-hour period in
the following way:
                             Ri =
where    g = gravitational acceleration,
         T = absolute temperature,
         z = height,
         u = wind speed.
Wind speeds and temperatures used in the calculation of Ri were measured
at 1.5 and 10.5 m.  The appropriate height for z is given by the geo-
metric mean of 1.5 and 10.5, equal to (1.5 x 10.5)"1.  For unstable
atmospheric conditions, Paridolfo and Businger hypothesised that Ri is
related to the Monin Obukhov length (L), (Paulson, 1970).

                              ,-1 _ Ri
                              L   =F~                               (A-l)

For stable air, an empirical relationship was found by McVehil (1964).
                              ,-1 =       Ri
                              L   ~   z (1-0R1)                       (A-2)
Colder (1972) showed an empirical relationship between L and the Turner
stability types.  Consistent with Golder, e was assigned a value of 7 in
Equation (A-2). e  is the reciprocal of the critical Ri (Binkowski, 1975).
The figure below  shows the Turner stability types as a function of L~
and roughness height z  .  The roughness height typical of the terrain
around the test track is  3 cm.  Figure A-l below is very similar to
Figure 5 in the Golder paper.
                                      20

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 (cm)
           _.12  -.10  -.08  -
                                                     .04
.06   .08
Figure A-1.  Turner stability class as a  function  of  L~   and z .
If a horizontal line is drawn across  the  figure  at z   =  3 cm,  the
stability classes are determined by the ranges of  L~   bounded  by  the
dotted lines.  For Ri greater than zero Equation (A-2)  is used to
calculate L~ .  For the Ri  less than  zero,  Equation (A-1) is used to
determine L  . The following values were used  to  define each stability
class.
              TABLE A-1.  STABILITY CLASS AS  A FUNCTION  OF L"1


Range of
L
L
L
L
L
L
-1 <
-1
-1 <
-1
-1
-1

L"
-0.
-0.
-0.
0.
0.
0.

1
095
055
018
005
013
013



and
and
and
and




> -0.
> -0.
> -0.
> 0.




095
055
018
005


Stability Class
A
B
C
D
E
F
                                      21

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                              REFERENCES
Binkowski, F.  S.,  1975:   On  The  Empirical Relationship Between The
     Richardson Number and The Monin-Obukhov Stability Parameter.
     Atmos. Environ.  6,  453-454.

Colder, D., 1972:   Relations Among  Stability Parameters in the
     Surface Layer.  Boundary-Layer Meteorology 3^ 47-58.

McVehil, G. A., 1964:  Wind  and  Temperature Profiles Near the Ground
     in Stable Stratification.   Quart.  J. Roy. Meteor. Soc. 90. 136-146.

Paulson, C. A., 1970:  The Mathematical  Representation of Wind Speed
     and Temperature Profiles in the Unstable Atmospheric Surface Layer.
     J. Appl.  Meteor. 9. 857-861.
                                    22

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                                   TECHNICAL REPORT DATA
                            (Please read Instructions on the reverse before completing)
 1 REPORT NO
  EPA-600/4-78-044
                                                           3 RECIPIENT'S ACCESSION-NO.
 4. TITLE AND SUBTITLE

  A PILOT  STUDY ON DISPERSION NEAR  ROADWAYS
             5. REPORT DATE
                Auaust 1978
                                                           6. PERFORMING ORGANIZATION CODE
7. AUTHOR(S)

  William B.  Petersen
                                                           8. PERFORMING ORGANIZATION REPORT NO.
9. PERFORMING ORGANIZATION NAME AND ADDRESS
                                                           10 PROGRAM ELEMENT NO.

                                                              1AA603   AB26 (FY-78)
   (same as block  12)
                                                           11. CONTRACT/GRANT NO.
 12. SPONSORING AGENCY NAME AND ADDRESS
   Environmental Sciences Research  Laboratory -  RTP,  NC
   Office  of  Research and Development
   U. S. Environmental Protection Agency
   Research Triangle Park, NC   27711
             13. TYPE OF REPORT AND PERIOD COVERED
                In-House
             14. SPONSORING AGENCY CODE
                EPA/600/09
 15. SUPPLEMENTARY NOTES
 16. ABSTRACT
      High  frequency wind fluctuation  data were used to estimate  the dispersion
 near roadways.   The standard deviations of the wind direction  and the elevation
 angle were computed for six averaging times.  The EPA HIWAY model  was modified
 to use  these fluctuation statistics directly to estimate dispersion.  The data
 from the General Motors Sulfate  Dispersion Experiment were used  in this study.
 In particular,  the data used in  this  pilot study were three half-hour periods when
 the winds  were  nearly parallel with the test track.  Results from analysis show
 that model performance was improved for parallel wind conditions  when the fluctuation
 statistics of the wind were used to estimate dispersion.  The  results also show
 that model estimates are most  sensitive to the vertical dispersion parameter.  Indeed,
 concentrations  seem to be insensitive to the horizontal dispersion parameter.
17.
                                KEY WORDS AND DOCUMENT ANALYSIS
                  DESCRIPTORS
                                              b. IDENTIFIERS/OPEN ENDED TERMS
                           c.  COSATI Field/Group
 *Air pollution
 *Wind (meteorology)
 *Atmospheric diffusion
 *Roads
 *Mathematical models
                             13B
                             04B
                             04A
                             13B
                             12A
13. DISTRIBUTION STATEMENT
 RELEASE  TO PUBLIC
                                              19. SECURITY CLASS (ThisReport)
                                                UNCLASSIFIED
                           21. ^O. OF PAGFS
                                31
20. SECURITY CLASS (This page)

  UNCLASSIFIED
                                                                         22. PRICE
EPA Form 2220-1 (9-73)
                                             23

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