EPA-650/4-73-001
A  MESOSCALE  WINDFIELD  ANALYSIS
      OF  THE  LOS  ANGELES  BASIN
                         by

                   Gerald E. Anderson

          The Center for the Environment § Man, Inc.
                    275 Windsor St.,
               Hartford, Connecticut  06120
                 Contract No.  68-02-0223
                Program Element No. 1A1009
           EPA Project Officer: Kenneth L. Calder
                 Meteorology Laboratory
          National Environmental Research Center
        Research Triangle Park, North Carolina  27711

                    Prepared for

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

                    June 1973

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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 recommen-
dation for use.
                                   11

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                            TABLE OF CONTENTS





Section                           Title                               Page




   1                   Introduction                                      1




   2                   Atmospheric Model                                 5




   3                   Flow Model                                      10




   4                   Computations                                    14




   5                   Empirical Constants                             14




   6                   Data                                            15




   7                   Results                                         15




   8                   Recommendations                                 19




   9                   References                                      20





APPENDICES




   A      Mesoscale Influences on Wind Fields                          21




   B      Los Angeles Windfield - ANAL70 Program Specifications        31




   C      Poisson Surface Data Fitting Technique                       37




   D      Computer Output                                              42







                          LIST OF ILLUSTRATIONS




Figure                           Caption                              Page




   1      Los Angeles Region and Surroundings                            4




   2      Model Determination of Inversion                               7




   3      Vertical Temperature Profiles for 29 September 1969            9




   4      Circulation Pattern in Vertical Slice                        11




   5      Effective Topographic Surface at an Inversion                12




   6      Constant Potential Lines for Flow Past Mountains             13
                                   iii

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Figure                            Caption                             Pa#e

A:  1   Scale ranges of significance for atmospheric boundary          22
        layer phenomena and measuring devices

A:  2   Vertical section of heat island thermal circulation            24
        and the temperature distribution producing it

A:  3   Layout of regions for topographic and thermal windfield        25
        analyses

A:  4   Topography of Connecticut                                      26

A:  5   Streamlines on Connecticut grid from interpolation             26
        between stream functions at 15 data stations

A:  6   Streamlines from topographic analysis of the same data         26
        as in Figure 5

A:  7   Net topography relative to a highly smoothed "mean"            27
        surface for Toronto region

A:  8   Potential of topographically induced wind disturbance          27
        for Toronto region due to unit west wind

A:  9   Heat island temperature distribution for Toronto               28
        region

A: 10   Heat island disturbance potential for the Toronto              28
        region

A: 11   Lake-breeze disturbance potential for Toronto region           29

A: 12   West-wind component of net wind in Toronto region for          29
        4m sec"  mean wind from west with topographic and
        thermal effects

C-l     Isotherms (°F) x 10"^ in Los Angeles Basin                     41
                                    IV

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                               ABSTRACT










       The rationale, derivation, and use of a mesoscale windfield




analysis is presented.  In the program reported on herein, the analy-




sis was applied to a specific region - the Los Angeles Basin.  This




application is in support of a multi-phased effort of modelling




ground level and/or three-dimensional air pollution distributions




in the region.  Los Angeles air pollution modelling efforts supported




by the Environmental Protection Agency are using data collected during




an experimental program carried out during the fall of 1969.  The meso-




scale windfield analysis described here was specifically applied to 13




hourly periods from 5:00 am to 5:00 pm on 29 September 1969, and one




period at 6:00 am on 30 September 1969.

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1.  Introduction





        A detailed description of an analytical technique for defining




two-dimensional (horizontal) wind patterns is presented in Reference 1.




A modified version of this analysis is herein presented and applied to




a specific site, the Los Angeles Basin.




        The basic assumption of the analysis is that in many situations




atmospheric boundary layer flows are approximately two-dimensional.  The




scale of vertical variability is so much smaller than the horizontal




scale that the flow may be considered as a horizontal flow perturbed by




vertical disturbances.




        All two-dimensional flows may be decomposed into uniform flows,




source^sink flows, and vortices.  That is, every real two-dimensional




flow is the superposition of a uniform flow and a distribution of sources,




sinks and vortices.




        Vorticity can only be introduced into a flow by a transfer-of-




energy process, as, for example, by friction.  In the atmospheric boundary




layer, friction against the ground surface introduces vorticity about




horizontal axes, but only vorticity about vertical axes can affect the




horizontal wind patterns.  Vorticity in the horizontal patterns may be




introduced by variations in the surface friction.  For example, the wind




is turned in toward rough regions.  Thus, a "friction island" will be




produced by a rough city sitting on a smooth plain.  This effect is




generally less than the "heat island" effect of the same urban area.  The




weakness of the friction effect on horizontal wind patterns is fortunate,

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since it is very difficult to define,  measure and/or  describe the friction




patterns of a large urban-rural complex.




        Source-sink effects (divergence-convergence)  on horizontal flows




often dominate the horizontal wind patterns and at  least some of  these




effects are observable and may be related to measureable characteristics




of the atmosphere.




        Since the mass of air is conserved in the atmospheric flows under




consideration only one mechanism exists for producing divergence  Of) .




Air must move vertically from or to the two-dimensional layer under consi-




deration.  Such vertical motions can occur in the near-ground layer because




of complex interactions with upper layers, but perhaps the dominant mecha-




nisms are thermal and mechanical interactions with  the ground surface




itself.




        Air flowing across a topographic surface must rise and fall to




follow the contours.  Since this effect is forced by  the surface, it dies




out with altitude.  Thus, there must be a net rise  or fall in the lowest




layer at each horizontal location.




        Similarly, air heated over a relatively warm  surface rises, and it




falls over relatively cool areas.  The rise and fall  depend on the rela-




tive surface temperatures.  These major mechanisms  that produce rising




and falling air are determined by surface characteristics, topography




and temperature, that may be measured with some precision.  The resultant




wind patterns may be determined by assuming linear  relationships between




the divergence and the surface property.  The analysis then correlates




cause and effect, but falls short of solving the relevant momentum and




energy equations that express the full range of interactions.  The present

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analysis is based solely on the mass continuity equation.



        The relevant derivations are presented in Reference 1.  The



results are given in terms of the velocity potential.  The velocity



itself is the vector gradient of the potential



                          V  =  V$



        The flow divergence is the Laplacian of the potential



                        V.V  =  V2$



        In Reference 2 the potential was presented as being composed of



three superposeable components, the mean flow potential, the topographic



potential, and the thermal effect potential.


                $ = $       4-  $              +  $
                      mean       topographic       thermal


In the present analysis, the application to the Los Angeles Basin involved



such large perturbations to the mean flow that this linear combination was



no longer assumed.  The topographic velocity potential is here assumed



to depend on the thermal potential patterns.



        The divergence due to the thermal effect is found to be proportional



to the thermal updraft velocity which, in turn, is assumed proportional to



the relative temperature of the ground surface.


                V2$  ,       ~ (T - ?)
                    thermal         '



                              where. T is the local temperature

                              and T is some area mean



        The divergence due to the topographic effect is found to be



proportional to the topographic slopes and to the wind vector approaching



those slopes
       V2$         , .   ~ (V$      + V$  ,     n)  -V(AH)
           topographic       mean      thermal



                    where AH is height of inversion above the

                    local topography

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        The application of these equations to the determination of wind




patterns in the Los Angeles area (see Figure 1) is described below.




Figure 1 shows the square outline of the region of analysis and the




surrounding land and ocean area.  San Nicholas Island, a data station for




this analysis, is shown in the lower left hand corner of Figure 1.









2.   Atmospheric Model




        Since the climate of Los Angeles shows considerable stability (i.e.,




the short-term variability is small) and the chosen experimental day is




typical of adverse air pollution conditions, the windfield model presented




is most applicable to the meteorological situation of that day and season.




However, that situation is of long duration and of significant concern.




        Characteristics of the autumn Los Angeles meteorology were inferred




from examination of Northern Hemisphere Data Tabulations for several Cali-




fornia coastal stations (Point Mugu, Vandenberg, and San Diego) as well as




the offshore station on San Nicholas Island.  This data was available in




CEM's library.  In addition, Weather Bureau records for Los Angeles Inter-




national Airport were obtained from the National Weather Records Center,




Asheville, North Carolina.




        The meteorological situation modeled on the basis of these records




is one of a Pacific High over a cool ocean surface producing a surface-based




inversion extending up to about 2000 ft.  RAOB's from these stations indi-




cated a persistent inversion with a nearly constant temperature gradient and

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a nearly constant upper limit near 2000 ft.   In this inversion layer,  the




synoptic scale pressure field is driving a light onshore breeze.   Land




surface temperatures become cooler than the ocean at night and may become




considerably higher than the ocean temperature during the day.




        During periods of a relatively hot land surface, a mixing layer based




at the ground raises the bottom of the inversion to some altitude above the




ground.  Sea breezes are concurrently developed.  When land surface tempera-




tures fall below ocean temperature, land breezes are developed, but the in-




version remains ground-based.




        The temporal stability of the upper portion of the inversion layer,




combined with a physical concept of thermal mixing over a hot land surface,




led to the use of a simple, but not novel, model of the thermal structure.




The altitude of and temperature at the top of the basic inversion are taken




to be defined by soundings at San Nicholas Island.  San Nicholas Island is




taken to be representative of the meteorology of the region as it is undis-




turbed by the topographic and thermal effects of the Los Angeles area.




Since the height required is of the order of 2000 ft, it is assumed that




the island itself has little thermal effect on the upper portion of the




inversion.




        It is further assumed that a gentle, synoptic scale breeze is




continuously advecting the air mass from  the ocean  to the land.  This ad-




vective velocity  is also defined by wind  profiles reported at  San Nicholas.




Wind  soundings  exhibit more variability at all  stations  than do  the tempera-




ture  soundings,   This is true also at San Nicholas.   It  is particularly




true  in light wind conditions such as prevailed on  29,  30 September 1969.




It  is also true that for very light synoptic scale  winds, the  local




flow  in the Los Angeles Basin is much more determined by the  thermal

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driving forces.  Thus, the determination of the "driving" wind is not as


critical for the present cases as it would be for cases with stronger


winds.  The advected thermal profile is simplified to a constant poten-


tial temprerature gradient between sea surface temperature and the tempera-


ture at the top of the inversion.


        The actual driving wind used in the analysis was a single constant


wind of 0.7 mps at 225°.  This is a somewhat subjective choice representing


an averaging, turning, and reducing (to make appropriate to the mixing zone)


of twice daily soundings taken at 500 and 1000 meters.


        Over hot land, it is assumed that a mixing layer of constant


potential temperature is adjacent to the surface.  The layer is assumed to


extend to the altitude at which the inversion temperature equals the local


surface temperature.  The resultant profile is shown in Figure 2.
                                                           T1constant
                                                           'above inversion
   Z=H'  I	i	|	)t Inversion Top
                T-TSea " T'-TSea
T"TSea ~ TLand " TSea
            Figure 2.   Model determination of inversion base.

                                    7

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Thus, H, the height of the inversion base, is simply
                        |-T(X,Y) - T    "]


               H  =  »'    T- - T
                        L        SEA   J
        Inversion heights from this formula compare favorably with inversion



heights identified directly from temperature profiles.  Comparisons are shown



in Figure 3 where profiles reprinted from Roth (Reference No. 1) are marked



with inversion base location determined by the present method along with


those presented in Reference No. 1.

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                                              .  Annupv
                                              (KtT AflOVI
                                             HCflN It A. LLVEL)

                                                 2400
                                                 2000
                                                 1500
                                                 1700
                                                 800
                                                 400
                Temperature (°F)
                         74         6?
                          Tcriiperatiire (°f)
        	 OBIS rST
        	0910 PST

        	1206 PST

        	-1257 PST
      66
               74        82
                Temperature (T)
  ALT IT UK
(ffCT ABOVE
MEAN SEA LEVEL)

    2400
                                                2000
                                                1600
                                                1200
                                                800
                                                100
                        74        ZZ        90
                           Temperature ('F)
                                     Invrr.: i on Dnscs H.-srlcpd

                                       >i:  Cor-^ut»?d by prt- c nY mcchtd

                                       C  Vrora Roth ivporc
Figure 3.   Vertical temperature  profiles for 29  September  1969:   a)  Los  Angeles
             International Airport,  b) Hawthorne,  c) Commerce, d)  El Monte.
             Reprinted from Roth  (Reference  1).

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     Basic modifications to the windfield model described in Appendix A were



required to account for the typical presence of a strong inversion which



severely inhibits vertical motion and to account for the presence of the



very large scale topography present.  The formulation of the thermal pertur-



bation to the windfield was actually eased because well distributed surface



temperature observations were available.



     Equation A(8) of Appendix A is linear and eq. A(5) may be considered



linear if the windfield perturbations are small.  In the Los Angeles case,



windfield variations typically exceed the synoptic scale wind.  Thus, no



uniform "mean" wind can be reasonably defined for use in the forcing function



in eq. A(5).  For the model used here, the thermal effect is computed first



from the ground surface temperature distribution.  The resulting velocity



vector field is added to the synoptic scale (uniform on this scale) wind



vector.  The net windfield is used in the forcing function on the right-hand



side of eq. A(5).



     The presence of an elevated base of a strong inversion developed by



vertical thermal motions has a significant effect on the formulation of the



flow model.  As discussed in Appendix A, the model basically equates the



average over a chosen depth of the horizontal divergence to the difference



in vertical velocity over that depth.  Since the inversion itself has thermal



stability which inhibits vertical motion, its base is assumed to be a sur-



face of zero vertical velocity; that is, mass does not penetrate the inver-
            >


sion base.  These assumptions cannot be completely true since the inversion



base, itself rises and falls in a diurnal cycle.  The velocity of the inver-



sion base is, however, generally small compared to the maximum vertical



velocity in the layer b«low the inversion base.
                                   10

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      Consistent with  the  above discussion, it is assumed that the mesoscale
                                                                       i.
 thermal  circulations  are  contained within the mixing layer below the inver-


 sion  base  shown in Figure 4.  An exception to this concept is assumed when


 the land is  colder than the ocean.   In this case, the inversion is ground


 based, yet down slope  thermal drainage is not inhibited.  Another exception


 is that  where  the computed  H  is near zero (as over the ocean), a minimum


 value of  H  =  200 ft   is  assumed.  This allows flow from the cold regions,


 and is consistent with empirical estimates of turbulence scales for very


 stable layers.
                                                    Inversion Base
  200
  Minimum [
00 ft. 1  (	
inimum )  ^  .	
Level of Zero
Divergence
                Cool Surface
                                     Warm Surface
  Figure  4.  Circulation pattern in vertical slice.





     It is recognized that such a pattern will be partially hidden by ther-


mal and shear turbulence found in the mixing layer.  The conceptual model


shown in the sketch suggests that at about one-half the height of the in-


version base, the thermal motion is purely vertical.  H/2  then, is a con-


venient upper surface to define as the upper boundary of a near ground flow


regime.  The space between  H/2  and the inversion base would then be occu-


pied by a flow moving counter to the near ground flow.  With  AH  defined


as the inversion altitude minus the local topographic altitude, the model


uses  AH/2  as the layer depth over which the windfield is averaged.
                                    11

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     In regions where the topography penetrates the inversion base, the layer


thickness goes to zero, thus producing a very large flow perturbation.  This


represents the turning of the wind as it becomes parallel to the topographic


contours because of the extreme thermal stability of the inversion layer.


Numerically, however, the accuracy is lost as the singularity of the inter-


section is approached.  The correct analytic condition should be that the


component of the wind vector normal to the intersection should be zero; i.e.,
                           n
      -                                   ^.
where n is a unit normal vector and V$ = V.


     The algorithm programmed for solution of the Poisson equation, however,


only allowed specification of $ as a boundary value.  Therefore, the bound-


ary condition was approximated by specifying large arbitrary values of VH


(the topographic gradient) at the edges of topographic penetrations of the


inversion base.  This was done by setting VH to a constant large value


wherever VH was negative  (and the land surface temperature exceeded the


ocean's).  Thus, topographic penetrations became "mesas" with topographic


gradients large at the rims, but zero at the interior of these "mesas."


Another view is that the vertical resistance of the inversion increases


the effective topographic slope (see Figure 5).
   H
                                                           "Effective" h
              Fig. 5.  Effective topographic surface at an inversion.
                                   12

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        A separate trial of this scheme  was carried out and Figure 6
shows the potential lines corresponding to flow about such topographic
islands (the shaded areas).  It is seen that the condition of n'V = 0
is approximately met at the "shores" of the "islands" (Cliffs of the
mesas).  The trajectories, which would be lines normal to the potential
lines, are thus turned to be tangent to the "shores".
        Figure  6.  Constant potential lines  for flow past mountains.
                                   13

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     The program was written in ANAL70, a language available for use on a

UNIVAC 1108.  The program is printed in Appendix D and the program specifi-

cations in Appendix B.  Since ANAL70 programs are executed in fixed sequence,

flow charting is generally irrelevant and the type of specification used
                                                             s
seems most appropriate.



5.  Empirical Constants

     Although the model does not make use of the full set of relevant dynamic

equations, there is little empiricism in the solution of the equations used.

The only arbitrary constants defined are:

     1)  the altitude heating effect.  The surface temperature in an other-
         wise homogeneous thermal region is assumed' to lie one-third of the
         way between the constant temperature value and the constant poten-
         tial value.  This allows computation of an altitude effect on tem-
         perature that is reasonable in regions  of significant topography
         far from temperature data stations.  The correction is not large,
         so the accuracy of the one-third estimate is not critical.

     2)  the minimum  AH .  It is set at 200 ft  (as discussed above).

     3)  the "mesa" walls at topographic.penetrations of the inversion.  They
         are assumed to be 600 ft high.  Again,  the exact value chosen here
         is not critical.

     4)  the constant relating the ground temperature and the thermal updraft
         velocity generated.  It is assumed to be

                                      W    •  =  .001 .
                                   T - T
                                        SEA
         This value was chosen as  producing the most  nearly correct wind
         speed at the coast for sea breeze occasions, and is most subject
         to "tuning" adjustments.
                                    14

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6.   Data
        Ground surface temperatures were taken from data provided by Roth
from a 1969 Los Angeles experiment  (Reference 1).  Specifically, data was
used for thirteen (13) hourly periods from 5:00 am to 5:00 pm on 29 Septem-
ber 1969 and for 6:00 am on 30 September 1969.  Temperatures were provided
for nine (9) stations for most periods, but a few reports were missing in
the early morning hours.  Missing temperatures were assumed by inferring
consistency of patterns with the available data.  Gridpoint temperatures
were interpolated by the method described in Appendix C.
        Topographic height on a 50 x 50 mile grid with two mile grid
spacing x^ere taken from Roth (Reference 1).  Additional topographic data
was obtained from Dr. James Angell of ARL/NOAA.  This data was defined on
a 1/2 km grid of 116 points (N-S) by 137 points  (E-W).  An ANAL70 program
combined (by interpolation, where necessary) both sets of data on a 49 x 49
(1 mile) grid.  Point (1, 1) was located at 118° 37' 13" W, 33° 34' 53" N.
The inversion height, surface and inversion top temperatures, and the surface
synoptic wind were taken from San Nicholas Island soundings.


7.   Results
        The model was run for thirteen (13) temperature sets from 5:00 am
to 5:00 pm, 29 September 1969, assuming the San Nicholas Island data to be
constant for the entire day.  One run was made for data from 6:00 am,
30 September 1969.
        Computer printouts were obtained for:
           •  the analyzed temperature field (T),
           •  the grid point values of the velocity potential (PHI),
           •  the grid point values of the south wind component (V),
           •  the grid point values of the west wind component (U).

                                   15

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These printouts are reproduced in Appendix D.   Each printout sheet is labeled




at the top with the dependent variable name and a power of ten scaling factor.




Each label also includes the SETS number (e.g., 5:00 am is labeled SETS = 1).




All fields were printed out on a 25 x 25 grid  (i.e., every other point of the




49 x 49 grid) although the computations were done on a doubly dense net, as




noted above.  In the printouts, north (Y) is to the right.  Also zeroes are




printed on grid points of the PHI, U, and V fields where the topographic




surface rose above the local inversion.




        In addition, graphic display was generated with an SC4020 film




writer.  The fourteen (14) SC4020 frames are reproduced in Appendix D.  They




show wind vectors at the output grid points (i.e., at every other point of




the analysis grid).  The wind vectors are superimposed on topographic con-




tours, and regions warmer than the ocean that  rise above the inversion base




are cross-hatched with grid lines.  Wind vectors in cross-hatched regions




are suppressed.  Winds in these regions are not computed by the present model,




Indeed, they are not needed since it is assumed that the extreme topographic




contours are coincident with wind trajectories in the cross-hatched regions.




        The known general features of the Los  Angeles winds are reproduced




with both land and sea breezes generated at the appropriate times.   Inclu-




sion of the 6:00 am 30 September 1969 case was specifically to provide a




case for which significant portions of the ground surface were cooler than




the ocean.  The analysis results in land breezes for this condition.




Although the wind speeds for the land breeze case are too low for the




vectors to be displayed at many points in Frame  14, the land breeze is dis-




played in the grid prints of PHI, U, and V.   It will be noted in these dis-




plays that zeroes appear over much of the ground surface.  This indicates







                                    16

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that much of the ground surface was warmer than the ocean for even this




case.  The warm ground region appears as the gridded area in Frame  14.




        The land breezes computed for the fourteenth SET are, again, net




results.  They include a mean driving wind of 0.7 raps from the SW.  The




land breeze would be stronger in the absence of this synoptic component.




Winds this light are extremely difficult to define analytically and




observationally, but the use of observation to better define the mixing




depth (200 m used here) would increase the confidence in analytical results.




        Gridprint output of PHI may be interpreted by noting that flow is from




low PHI values to high PHI values. The flow speed is proportional to the




differences between PHI values at adjacent grid points.  For SETS = 14, the




output shows a minimum PHI at (x, y) = (37, 25);  [i.e., (19, 13) on the




25 x 25 grid =37, 25 on the 49 x 49].  The location of a minimum PHI is a




center of divergence.  Since flow is constrained by the inversion from




leaving the valley northward, flow spreads out as a land breeze southward,




flowing about both sides of the Palos Verdes elevation.  West winds appear




near the major area of inversion at both the western and eastern borders




of the region.  The west wind region at the west edge is much smaller




because the synoptic scale wind is blowing counter to the land breeze,




whereas in the east it is adding to the divergent flow.  West winds at the




eastern border may be unrealistic but the analysis cannot make predictions




without data, and no data is available on ground temperatures at or beyond




the limits of the region.




        In the rest of the region the land breeze is seen to be a maximum




near the coast and to be stronger and more uniform at sea than inland.
                                 17

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        Sharp vertical gradients of  the wind  often observed  in extremely




stable slope wind,  valley drainage,  and land  breeze cases  also emphasize




problems in defining horizontal wind fields for  regional pollution analyses.




The breeze blowing  in the face of a  man on the ground  may  be quite differ-




ent than that read  by the anemometer (at,  say, 20 ft)  that he is  tending




and could be in the opposite direction from the  breeze which entrains




effluent from a nearby chimney stack.




        Some boundary effects seem somewhat unrealistic.   At the  northern




edge of the region  this is probably  because the  mountains  and the boundary




condition prevent flow from crossing much  of  the north border, but this is




also the region of  the most complex  topography and most commonly  lies above




the inversion base, so it is difficult to  judge  the flow features realisti-




cally for this region.  The closed circulation cell that appears  in the San




Fernando valley seems superficially  like that observed. It  is doubtful,




however, that the analysis is accurate enough in this  region to trust.




        The inversion does not rise  to allow  mixing layer  flow into the




San Fernando valley until 10:00 am on the  29th (Frame  6).  By 11:00 am it




has risen more and  mixing layer flow is crossing much  of  the northern ridge




bordering the Los Angeles basin.  The net  flow across  the  northern border




of the analysis region is zero, however, because of boundary conditions




applied in the absence of data.  It  is unclear how realistic the solution




is near the borders of unknown temperature and/or flow.




        Similarly,  flow in the eastern part of the region  is strongly




influenced by assumed boundary conditions  there.  If the region to the




east of the analysis region is warmer than is assumed, there would be a




more westerly component to the wind  vectors,  and flow out  through the




eastern border.




                                  18

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         Since  the  cool-land drainage patterns  involve extremely thin layers,




they would be most sensitive to small-scale topography in the real world




and to assumed values of empirical constant in the computer.  Thus, solu-




tions for cool-land regions and/or times should be more suspect than hot-




land regions and/or times.




        A magnetic tape record of the numerical results for these fourteen




(14) cases was submitted to EPA to be compared, by their computer, with




observational data and with windfields defined by several objective inter-




polation techniques.







8.  Recommendations





        Since the guiding of the flow by the largest scale topographic




features seems to be such a major feature of the results, it would seem




important to use the more correct gradient type boundary condition.  This




assures that the flow is parallel to the topographic contours.  The




algorithm for this type of boundary condition has been written, but has




not yet been included in the program.




        Formulation of the boundary conditions for the thermally driven




wind seem unduly arbitrary and seems to lead to unrealistic flow patterns




in a limited section along the northern border.  This could probably be




improved.




        Further calibration runs could improve the specification of the




constants of the problem.




        A small amount of additional programming could produce output with




above-inversion windfields in the same display.  It might be somewhat mis-




leading, however, since there should be little pollutant transfer at the







                                  19

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field intersections.   That is,  pollutant leaving a zone in which the topo-




graphic surface lies  above the  inversion should override the mixing layer,




while pollutant reaching the edge of a ground-level mixing region should




be swept into the counter-current flow in the upper half of the mixing




layer.









9.  References





    1   Roth, P. M.,  S.D. Reynolds,  and P.J.W. Roberts, 1971:  The




              treatment of meteorological variables.  Appendix C,




              Development of a  Simulation Model for Estimating Ground




              Level Concentrations of Photochemical Pollutants^




              Report  71-SAI-17, June.






    2   Anderson, G.  E., 1971:   Mesoscale Influences on Wind Fields.




              J. Appl. Meteor., 10,  377-386.
                                 20

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 Appendix A:   Mesoscale  Influences  on  Wind  Fields*
                                                 ABSTRACT

             An analysis of meso^cale influences on protind level wind fields indicates that topocraphy and the thermal
           cells associated with mc^o^cale ground temperature anomalies (urban heat Uhuids and !anj-\vuter con-
           tiasts^ arc the major dctciminors of hori/ontal trajector>r perturbations on scales appropiiatc tor air pollu-
           tion analyse.- Simple an.ilv-es ba-ed on the divergence equalion [u:mit calculations of uiml fields for aii
           pollution trajectories that  appear much more iralistic than conventional objective anaKsis of surface wind
           observations The anaUsi- provide? a unique objictive procedure for ical-tinie inU-.uiMiion of the conserva-
           tion of pollutant equation or for the development of regional air pollution climatolosy
1. Introduction

  When atmospheric winds are measured, the icsulting
reported values are  on physical micro- or macroseales
that are inappropriate for many theoretical  01 applied
needs. A particular need is for knowledge of mesoscale
wind fields to be used in calculations of the dispersion
of atmospheric pollutants. ]n  spite of the power of
modern computers and  programming languages, it  is
not practical for wind-field analyses lo press the analvti-
cal  state-of-the-art.  Thus, in  the following work, it  is
intended that t!;<- i.iiahsis shuiilel provide  an an Unite,
quantitative  model  of  the  most  significant  known
effects, should not  violate  important  consliaints of
neglected  effects, and should be simply and economi-
cally appropriate for real  applications. The  analysis
presented here was  developed in its original form  by
the  author  for use  in the  Connecticut air pollution
simulation model  (Hilst,  19681. Kxtensions to 'hcnnal
perturbations \\ ere made for the Center for the Kn\ iion-
ment and .Man  (C-CM)  air  pollution model  for the
Toronto Metropolitan Region.
  The difficulties encountered in  trying  to measure
mcsoseale wind fields  are suggested by  Fig.  1. The
relevant  scales for atmospheric pollution  are  roughly
mapped  out as  the appropriately  grey area  in  this
figure. The  heavily outlined  Male regime-,  \\hich are
susceptible to direct  measurement  by wind  measuring
devices such  as anemometers, pib.il.- and tetioon-, over-
lap very little  of  the regime of interest for pollution
problems.
  Alternative approaches to determining wind fields on
the scale of pollution cloud,' include incline I measure-
ment and  the  use- of theory.  Pressure  iiieasurxiiients
are used lo el. fine wind field-, on a svnoptic si.dc, but
the macros'/ale "wealher" pattern-- 5,0 defined  aic also
seen (Fig.  1) to be  o! an inelc vant  scale.  ''Theimal"
fields are  sometimes of appropriate  scale--,  but  diiect
measurements  of these field-, .ue: not usuallv 'i\ ailahle,
and  the theory of the'se- fields as a  function o:  --uif.ice,
moisture and i adiation < ejiulil ion-, is not fu in e iiou^li to
allo\\ us to obtain solutions for all such theimal motion
fields.  In  this  paper,  the only thermal  fields  treated
are  tho-^e  due  to "heat  island"  and  "lake breeze"
effects. The long time-scales of these phenomena make
them significant thermal influences on pollution  wind
patterns.
  Suiface faction elements and their effect on boundary
layer ilow may be significant, but technical work, to date
in meteorology has not disclosed suitably simple analy-
ses appropriate to our needs for mesose-alc  influences
usable in the air pollution model. Comparative analysis
indicates  thy I  the generally greater roughness of  the
built-up area  of  a city creates  a  "friction huirp,"
analogous  to  a  heat  island in urban areas, but  the
magnitude of the friction effect on wind field..-, is con-
siderablv less than the heat island effect on wind fields.
In geneial, it is onlv the horizontal variation of rough-
ness (e.g., the  urban-rural  contrast) that affects hori-
zontal wind trajectories.  Since,  icni^hness  cannot be
described  with precision, inclusion of fiiclional eilects
in this analysis does not seem feasible at  this time.
  One more factor is  depicted in Fig. 1—topography.
Topographic elements are measurable,  their influence
on  atmospheric flow is  subject  to objective analysis,
and their scales neatlv  overlap  the scales  of interest
for pollution problems. \Ve ma}1 anticipate a correspond-
ence between the scale of the topoguiphic elements and
of tin- atmospheric  motions they induce. Therefore, a
call.ulation of low-altitude flow over a given topography
should  give at least a component  of a real  wind field
th:tt would be relevant to pollution and other mcsoseale
aiuth ses.
   It would seem  that thermal,  topographic and  fric-
tion.il  eilects could, to a reasonable appio\imation at
le'asa, be decoupled.  In the- following an.'.lysis, frictional
cllecis  a;e  ignored, and  thermal  and  topographical
el'cMs are each  treakd separately.  The solutions  are
added  io obtain  the'  nel wind-field  disturbance. The
disturbance  he-Id  added  to  the  obseived or assumed
--\ iioplii uinel  field  \icld-, the net cal< ulaled  wind.
 *   Manuscript  by  G.E.  Anderson  (GEM),  reprinted  from Journal of Applied
     Meteorology, Vol.   10,  No.  3, June 1971,  pp.  377-386.
                                                  21

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                          JOL'KNAI.  OK  Al'I'f. IK. I)  M M 'I K I) K () I. I) G V
                                                                                     Vol L'MK 10
2. Analysis

ii. Typographic i^iinl Jiclih
   It was intended  to develop u technique for defining
mesoscalc wind lields that would  be feasible and eco-
nomically practical for  use in routine  operation of a
computerized pollution model. Therefore, it \vus »>M.-n-
tial  to  determine  those  analytic  featuits of gieatesl
significance.  The  topographic anuKsis  presented here
specifically considers conservation of ina^s only. Cu tain
aspects of  dynamics .ire  used  but. the momentum
equation is  not solved. The energetics  of the problem
are not considered. This approach seems  reasonable
in light of the remarks of  the previous .section.  If the
momentum  (friction) and heat exchanges between the
atmosphere and the surface  are  not considered,  the
impenetrability of the surface is  its most significant
characteristic.  \Ve write, then, the three-dimensional
continuity equation for an incompiessible atmosphere,
assuming  a limited vertical  motion, so that pressure
changes are small:
                   dll   dv  du
                   —+—+ —=0,
                   dx   dy  dz
                                    (i)
where .r, y, z are the orthogonal  mean wind-oriented
coordinates, and H, v, u are the corresponding velocity
perturbations.
  ff we are concerned  with the horizontal wind field
averaged over the depth of the pollutant cloud, we may
write (1) as
 f
 /
Jk
                                 dw
                                                  (2)
                                         where V i-, the gradient vector in the hoii/.ontal plane,
                                         V the total pi rliirbrd velon'tv i'i the horizontal plane,
                                         Si the local altitude of the smf.u •_, // the upper bound of
                                         the disturbed ail, and the ovcibar indicates an average
                                         o\ er 3.
                                            K.\pre--ion (2) may be  integi.tted  and  the  result
                                         -implilied b> noting that

                                         (//—//,!--//,  if the wind-field disturbance h thick]
                                                      compared to toponi.iphical variations
                                         ic(H)  ~0,  i.e., the topographic effect is not felt
                                                      .•bo\e the height //
                                         :.'(/;)   ~ LT- V//, v\here II is the unperturbed mean
                                                      velocity
(3)
                                         \\'e also define

                                         V = V0', where ' is the potcntialjunctioii of the
                                                  perturbation.

                                         Then (2) becomes
                                                                    1
                                                                   //
(4)
                                                                                                          (5)
                                           If, now, velocities are normalised by the mean wind
                                         speed [', h is normalized by the layer depth //, and
                                         the divergence by its suiface value V:(h), i.e.,
                                                          V    =U'U,
                                                          h*   =h'H,
                                                        we obtain
                                                                                       = v V/;*.
(6)
                                                                        OOOOO O O
                                                                       Pollutant clouds
                    10
                                                Horizontal scale—meters

                           KlG. 1. Srale ranges of significance for aUnojihcrir boundary |a>'er
                                        pluToincn.i ,ind me
                                                      22

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JUNE 1971
G K K A I. 0  K .  A N D E R S () X
                                                                                                       379
  Eq. (ft) is an expression for Ihr mean disturbance to
the wind field over the layer which is disturbed. If we
are concerned with  tracing the flow of pollutant, we
would wish to know the mass-'icciglitrd mam disturbance
to the wind field.
  Classical Indrodvnamie calculations (see Lamb, 1932,
and Shapiro, 1953) show thai the potential disturbance
due to topogiaphic elements is felt with little diminu-
tion to heights that arc of the order of the  dimensions
of the elements (i.e., a hill's uidins of curvutuie or the
spacing between  ridges);  thus,  the  topographic  dis-
turbance should be substantially constant ovei depths
of significant pollution.

b. Mean isiitJs
  To generalise the calculation, and to avoid the re-
quirement of solving (6) for every/ mean wind field, the
only  input  wind  fields used were a unit  west wind
(yz=\,  Pj = 0)  and,  separately,  a  unit south wind
(i>,—Q,  i'j, = l). If the mean wind fields  are uniform,
Eq.  (6) is  linear,  and perturbation fields can  be  ob-
tained by scaling and adding the fields due to each of
the unit component winds.
  In  some cases  the synoptic-scale  patterns  may  be
small enough  to  warrant  the  definition  of a non-
uniform mean wind  field. In these cases, it is a simple
matter to assign vx, vb mean  wind components to each
calculation grid point.

c. Topography
  Topographic heights h  are icquired  at  a  suitable
array of grid points.
  For the Connecticut analysis,  a single,  low-pass
smoothing of the topographic data was used to remove
regional-scale  topographic ''trends." The net topog-
raphy used in the model, then,  is the local grid point
height above or below the topographic "trend."
  Since Eq. (6) relates the hoiizonlal flow  divergence
to the topographic gradient,  the wind-field  solutions
using unadjusted  topography will include  divergence
at all scales for  which topographic  gradients  exist.
Modeling of  the  largest scale (i.e., scales comparable
to the dimensions of the  region) perturbation-, of  the
wind  may be quite unrealistic. Topographic effects at
these scales depend heavily on lopograpln be\ond  the
region's boundaries.  Topographic  wind-field perturba-
tions  on the regional scale are not geneialK  significant
for  pollution modeling  in  an\  case since they would
superimpose a weak  convergent  or divergent wind field
over  the entire region.  This would  merely affect  the
overall space-averaged conuntration  levels  bv a vcrv
small amount.  In Connecticut  there is an overall
increase of  mean  height abo\c sea level from  .south to
north. The  hill.s and vallt\-, then, represent  depai lures
from  the local mean height.
                         iJat v conditions
                    To  solve  (6)  the  velocity perturbation potential y specification  of  a zero  potential on  the
                  boundary. This coi responds to the assumption that the
                  mean,  synoptic  wind pievails outside  of  and on  the
                  boundary  but is pertuibcd within the region.

                  c. 27. crmallv ilri: en ^ i'/;,;'j
                    The mass conservation   equation   (2}  piovides a
                  faiih  good model of the effect of nicsoscale thermal
                  cells  on hoiixontal wind-field  patterns. The  relevant
                  growth or decay time  scales are long with respect to
                  dispel  sion integration  time  scales, and  the vertical
                  extent of suih thermal cells is often large with respect
                  to the pollution Liver  thickness of interest; thus,  the
                  theimal effect  is  to  produce  a quasi-steady,  quasi-
                  hoiisontal wind  disturbance in the near-ground layer.
                    The thermal  effect is assumed to be independent of
                  the lopogiaphic  effect -note  that Fqs.  (o)  and  (7)
                  are both linear -and thus,  the thermal effect is calcu-
                  lated  for a flat surface. On a flat suiface  the vertical
                  velocity at the surface is zero, but surface temperature
                  anomalies produce finite vertical velocities at the upper
                  limit of the polluted laves (Fig. 2). Fq.  (2) then reduces
                  to
since
                             at the top of the layer; w* is assumed  to
                 depend on Ts, the ground temperature (a function  of
                 x and y) and f, the spatial mean value of Ta. Without
                 solving the dynamics of the thermal cell, a large mea-
                 sure of realism may be obtained  by simpK setting
                                             A(T,-T)
                                        7/o
                                                                   (8)
                 where .1  is a constant of proportion:ditv to be deter-
                 mined from observations.
                   The scale  factor A  in  (8) represent* the  sensitivity
                 of the wind  field 10 the temperature potential. It must
                 be  evaluated experimentally.  Experimental measure-
                 ments of the Toionto heat island  etlecl reported by
                 Findlay  and Hirl  (1969) were used  to  determine A.
                 Cia'tKs'  theorem for souice-sink  fields relates the flu\
                 acros/- a closed  buundarv  to  the  total  divergence
                 (bouue strength) inclosed; thus,
                                  f n.v,j7'= f
                                 J i'         J n
                 where /' is the perimeter, R the ana of the region and
                 n n unit vector normal to the perimeter.
                                                    23

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380
                         JO I" UN A I.  01-  A IT I. I l-ll;  M P. r F, O k O I.O G Y
                                                                                                       t: 10
  Since (8) relates V-V  (and,  hence,
7',, — T, we have
                                           to .1 and
-i    r         if                 v"   /f>\
-= /  n.V,/P/ /  (fa-T)tlR = ---  _ (  -),
//  y/.        / ./*             (T,-r)\R/
                                                (in)
where  {'„ is  the  outward normal component of wind
across  the  boundary, the caret represents an average
over A', or P, and the overbar is an average over some
area that is large with respect to R.
  Thus, .1 may be determined from a single deteimina-
tion of the radius of ina.\iinum inilow associated with a
given temperature  field. The  case studied by Findlay
and llirt indicated a maximum inflow velocity of 1.7
m sec"1  associated  with a  temperature potential of
~2.5C.  With  the  temperature  field characteristics
postulated  in the next section, these data give a value
of A/II =0.1. The precision  of  this  result  obviously
leaves something to be  desired but Findlay and Ilirt's
comparison  with  Gold's  (1956)  theoretical  results
should be valid  for lhi< result also.  The result  should
be more effective than  anemometer  \\ind readings to
sort out thermal and  topographic  wind-field modes.
  As a  minimum,  this  linear relationship centers  up-
drafts over "hot spots" and makes  the intensitv of a
thermal cell proportional to  the energy input. Advec-
tion of  the thermal patterns has not been accounted
for, but could easily be included in multi-layered models.

f. Thermal patterns
  When the wind generating routine was developed for
the  Connecticut  air  pollution simulation model,  the
scale of the entire state was large compared to urban
and coastline  effects. For  Metropolitan Toronto,  the
uiban development and the lake front are both signi-
iicant  to  the scale size oi  the  region.  This section
addresses the heat island  and  hind-water interface
patterns which  were analyzed only for the Toronto
region.
  In addition to linear superposition of thermal  and
topographic wind  fields, it  is assumed  that  distinct
thermal effects can be separated from each other and
that these  effects are also additive. By  identifying in
lilt; Toronto region, for example, separate "city heat
island" and "lake brec/.c" ell'ects, suitably repiemula-
tive ground temperature patterns ma\ be established for
each by Using a minimum number of parameters.

If. Heat island
  For  a heat island, the temperature  is assumed con-
stant over  the heat source area and is assumed to have
different (lower) values at a suburban strip along the
lake shore and on a perimeter that is far enough away
to be unatfeclcd b\  these heat sources. These  tempera-
tures are used as boundary conditions for  the solution
of the La Place equation

                      V2rs = 0,                   (11)

to determine the temperature field between  the heat
island and  the remote perimeter.
  The  only free parameters are the center city tempera-
ture and the remote temperature (the suburban tem-
perature anomaly is assumed to  be  propoi tional to
that of the  urban  area). This pattern, combined with
the lake-land temperature field described  in  the next
section, reproduces  the major  characteristics  of  the
climatological  temperature  fields  observed  for  the
Toronto region (Findlay and Hirt,  1969; Munn et al.,
196-1.)  The actual  wind-field computation assumes a
unit  (city-remote)  temperature.  The  perimeter is
assumed to be  experiencing  a  pure inflow; thus, it
should be a line of non  (horizontal)  divergence.  Ac-
cordingly,  is zero on the  perimeter as  a boundary
condition for the solution of the wind potential equation
(
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JUNE 1971
                                      G E R A 1. U  E .  A N O E R S O X
                                                                                                         381
                             Ty at K ing Creek -^*


                                   Heat island
                          Toronto International
                          Airport          ~~*
                                 I at Islington
                                                   Coarse grid lak*? breeze rvgiou-^

                                                        0  Ilef. U-mp. locations for
                                                           (Mi-aMU't«ri?ed thermal fit-Ms,
                                                Toronto region v .^f
                                                 	    *"* "
	•—	———»O —i
5             c
             V f   \

   Fine topo. region^.    *
                        FIG. 3. Layout of regions for topographic and thermal wind-field anah ses.
A. Lake breeze
  The surface  temperature is assumed to have a con-
stant value over the water and another constant value
over the land.
  Since the thermal circulation cell  analyzed is larger
than  the dispersion model region, finite  values of the
velocity disturbance  potential should  be expected on
the region's  boundaries. Thus,  boundary  conditions
for  the  solution of  (8) depend on the wind field outside
the region. Further, the scale of  the external effect is
large  compared  to the dimensions of  the analyzed
region;  therefore,  the  effect of enors in  the boundary
conditions  might  be expected to be observable well
inside the region. That is, the ''window frame" may be
quite wide  for the case of Metropolitan Toronto.
  To provide more realistic boundary conditions,  the
thermal cell problem is solved on a much coarser grid
for  a much larger  region. As an  example,  the region
used in  this study extended beyond the south shore of
Lake  Ontario and  comparable distances in  the  other
directions,  as depicted in Fig. 3. Since the large region
ought to more nearly match the extent of the overall
thermal cell and since the Toronto region lav well in
the interior of the larger region, the coarse-grid solution
was deemed  to provide realistic  boundary  conditions .
for  the inner, fine-grid region. The ground temperature
distributions   assumed for  the   coarse-grid  problem
consisted of a constant tempeialure on the  lake and a
different constant  lempcratuie over the land. The lake
geometry used  is superimposed on a. true  outline of the
            lake in  Fig. 3. Data required for  the  Toronto  region
            consist of temperatures at the lake, and far inland.

            3.  Limitations and extensions
              The  analysis applies to  problems  that: 1) are sub-
            stantially steady during many model time-steps, 2)  ex-
            hibit spatial variability of topography  or ground tem-
            perature at scales  from regional-scale to  grid-space-
            scale, 3) exhibit absolute topographic  slopes that  arc
            much less than unity, 4) consider vertical scales small
            enough  that pressure is substantially constant, and 5)
            consider advective velocities that are much larger than
            the relative velocities of diffusion across streamlines.
              The  major  arbitrary assumptions are:  1) that  the
            advective transport of  pollutant can be meaningfully
            determined  by a  "bulk  velocity"  even  though   the
            advective trajectories vary with altitude (for  "thin"
            pollution layers or "thick" velocity perturbation layers
            this assumption is  irrelevant); 2)  that local vertical
            thermal  velocities  are  proportional to local  ground
            temperature anomaly; and 3) that the ground tempera-
            ture  distribution  can be adequate!}' described by a
            limited parameter (variable data) pattern derived from
            climatology.
              The constant pressure limitation suggests that this
            analysis is inapplicable to mountainous regions. It is
            suggested that replacing Kq; (1) with the compressible
            form of the conservation of mass equation would permit
            considi-ialion of (.uses for which the  Houssinesq appro\i-
                                                       25

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382
JOCKX.U.  or  Ai'i'Liri)  \i r.'i r.o i' 5.
                                                     26

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JUNE  1971
GERALD  E.  ANDERSON
                                                                                                         383
                          FIG. 7. Net topography relative to a highly smoothed "mean" surface
                                              for Toronto region.

dimensional arrays ma)' be controlled by single ANAL    only a few hours, and the program requires only a few
70 statements. For example, solution of a Laplace  or    seconds of 1108 computer time per time step.
Poisson equation as required in this work is effected by      The topographv of Connecticut is shown, for refer-
a single ANAL 70 statement. Programming (of a first-    ence, in Fig. 4, while Figs. 5 and 6 show the comparison
cut without de-bugging) of  the total  analysis requires    of the present scheme with a conventional analysis of
                        I'"jO. 8. 1'oU-htia] of topographically induced v.aid disturbance for Toionto
                                          region due lo unit \\tst uiiui
                                                          27

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 384
JOCKN.M.  OF  A I1 I' I. I 1C I)  M K '1 K O 1«) I. O C. Y
                                                                                                    VOI.L-MK. 10
                            FIG. 9. Heat island temperature distribution for Toronto region.

surface wind observations for the state of Connecticut.   produces  spurious  closed circulation cells  and  much
Fig. 5 shows a conventional objective  analysis which   large-seile wave  structure that is not consistent with
fit  values  of  streanifunctions which weic determined   observed wind rields  above the surface layer. It  shows
f or each of 15 data stations. Fig. 6 shows the topographi-   no  structure  consistent  with  the  topography. The
cally determined wind field. The ''objective" technique   topographic analysis, on  the other hand, shows effects
                           FIG. 10. Heat island di«turbaiice potcntbl for the Toronto region.
                                                     28

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JUNE 1971
GERALD  K .  AN D KK S O \
                                                                                                          385
                             FIG. 11. Lake-breeze disturbance potential for Toronto region.

only on the scale of the Berkshire (western) and eastern   wind field, and the heat island and lake breeze tcmpera-
hills'and the Connecticut River Valley. All disturbances   ture and potential fields for the Toronto region. Fig. 12
are small in  the Long Island Sound  and shore area,   shows a net wind field for the specific case of U = 4i+0j
  Figs. 7-11  show  computer-generated net  (filtered)   (m sec~'),  a \ve»t  wind,  7'.u = 2C = 7\and — T,^c,  Te
topography,   the  lopographicallv  induced   potential   =\C — Tcny — T,Kmoie, and crz — 150 m.
                FIG. 12. \Vest-win
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386
JOURNAL  OF  A PI'I. IK I)  M I-.  T K O K O I, O G Y
Yol I MI, 1(1
  The net wind field is calculated according to
where
                                                 (14)
  For the Toronto case the topographic effect  is teen
to be minimal.  There are few  topographic features in
the region with slopes on the order of oV_\ (A is the
grid spacing). From  (8)  it may  be seen that  slopes
of this order  are required to produce velocity changes
that are  a significant percentage  of  the  mean wind
velocity.
  The bluffs  along  the  lakeshore and some   ravines
more or less transverse to  the coast are  quite steep and
represent significant height changes. Each  is, however,
a linear feature with transverse dimensions less than one
grid spacing. As discussed in the previous section, sub-
grid-scale features are effectively filtered and thus con-
tributed  little to the computed wind-field perturbation.
  To more cleailv sre the- effect of the-e  topogiaphu
features,  a smaller  region was defined encompassing
only the urban center and some of the coastal bluffs.
The dimensions of this area were one-third of those of
the previously defined region, and the topography was
read on a grid three times finer. The array unit  dimen-
sions were thus the same as for the large region. Stronger
perturbations were  noted with  this calculation, but
they were, naturally, confined to the immediate vicinity
of the topographic disturbance. The effect on a  trajec-
tory crossing  the disturbance was minimal. It may  be
noted that wind-field divergence is produced only  by
topographic gradients parallel to the mean wind, and
therefore wind along a linear feature  will produce  no
effect. If  wind crosses a ravine,  it diverges  on  the
upwind  bank and converges  on  the  opposite  slope.
Thus,  the net effect  is not strong unless  inegularities
in the ravine topography meet the scale  criteria dis-
cussed above.  Wind crossing a bluff or cliff line  experi-
ences a simple expansion or contraction, but the stream-
lines  downwind  continue on  parallel  to  the  upwind
direction.
  Although the apparent  changes in the «ind field aie
small, and change the local trajectories  little, the effect
on  long-distance trajectories can be significant. Since
small perturbations integrated over long path lengths
can produce  large   displacements,  small changes  in
divergence patterns  have much  \ote inlluence near
the beginning of a trajectory tl\ui  thev do further on.
                                The  thrrmalK  induced wind held* are gc-nnallv ob-
                              served  a^ coinponi nls of mole ( ompli \ wind in ld-> and,
                              as discussed in tin- Introduction, observations are not
                              generally valid in defining mi so.si ale wind Ik Ids. There-
                              fore, tin re is  litllc physical evidence upon which the
                              present calculations may be judged  The patterns stem
                              theoretically xiti -fucloiv and are consistent with  such
                              observations  as i \isi. Validation of  the pollution dis-
                              persion model would be, perhaps, the  best  test,  of the
                              wind-field analysis.

                              5.  Conclusions

                                An objective analysis of  mesoscale  wind Helds has
                              been presented. The analysis makes use of precisely
                              known pin sit al characteristics  (topography) and the
                              geographic distribution of  homogeneous surface  tem-
                              perature  regions,'  lo  reduce a  previous  dependence
                              upon observational data of doubtful validitv or appli-
                              cability. Topically, as for  Metropolitan Toronto, the
                              only temporal data  requiicd are  the  mean, s\ noptic
                              scale surface \\ind, and surface  temperatures at three
                              prescribed locations.
                                The  wind  Fields computed by this  analysis appear
                              much more  realistic  than  do wind fields produced by
                              other objective anahses. The analysis  is computation-
                              al!} simple, and the parameterized .lesults can be linearly
                              combined  as  required for real-time,  forecast or hypo-
                              thetical caac-s. .Regional eliinaiolog} would depend only
                              on  synoptic-scale  wind  roses and  thus pro\ides the
                              only known  objective scheme for regional air pollution
                              climatology.

                                                 REl-F.KEXCES
                              Fmdla\  H.  F   and >f S. Hirl, 1U69. \i\  nrbnn-indnred  rneso-
                                  circulation. .\lmnsplicric Environment, Xcw York, Peigamon
                                  Press, Vol. 3, 537-542.
                              Gold, K , 1956. Smox—The rate of influx of surrounding cleaner
                                  air  II cat/in, 11, 230-232.
                              Hiht. G R , 1968. An air pollution model of Connecticut  Froc.
                                  IBM Sci. Ci'inp. Sy»:j>..  \\~iiUr and Air Resource \[aiuge-
                                  nicnt. 11!M Data Processing Division, White Plains,  N. Y.,
                                  251-J71.
                              Lamb, Sir Hoi ace, 1932.  Uvdri'dyiiamics.  Xeu  York.  Dover
                                  Publ , p. 76.
                              Munn  R F , K  f.. Tilus and K  J  \\ ikon, 1964: A pri-limmary
                                  c^imialc <>f th<-  m\erMon  climalolouv al'"»n^  the Toionto
                                  laki-hori--. Mc'tcfirolo'.'ic.il lirarrh, Department of Transport,
                                  Canada, CIR-U:.?. 1 FC 5o'>.
                              Sh;i[)iro. Archer H., 1933" The Pyn>irnics and  T/ifrntt'dyHdniics of
                                  Coinfic^ililc  Fl.ii'J  F/o;^, \"ol. 1. New Y"ork, Ronald Press
                                  163 pp
                                                  30

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Appendix B:  Los Anpeles Windfield ANAL70 Program Specifications

Definitions of required arrays

  GRID    is basic analysis grid of 49 by 49.  Point  (1, 1) is at
          118° 37' 13" W, 33° 34' 53" N.

  GRID'   is a grid staggered with respect to GRID.  Only interior
          points are included.

  GRID"   is a grid staggered with respect to GRID'.  It's inter-
          sections are thus on GRID intersections, but since only
          points interior to GRID' are included, the peripheral
          points of GRID are excluded.
Input Data

  Read the data that is the same for all sets -

          X (PLACES - vector of nine (9) X grid locations of
                      temperature observing stations measured
                      east of western edge.

          Y (PLACES) - ditto, nine (9)  Y locations measured N of
                       southern edge.

          H (X, Y)   - 49 x 49 array of grid point topographic
                       heights.

  •  Repeat • steps for each set.

  •  Read data for the current set -

       VARIABLES

          T (PLACES) - vector of temperatures observed at 9 places.

          NW (X, Y)  - temperature at sea and at NW corner;
                       i.e., at (1,  31) and (1, 49).

          SE (X, Y)  - temperature at sea and at SE corner;
                       i.e., at (43,  1) and (49, 1).

       CONSTANTS

                 SEA - sea surface temperature

                  H1 - height of top of inversion (over sea).

                  T1 - potential temperature at top of inversion (over sea)

                  Us - west wind component at sea.

                  V  - south wind component at sea.
                   SL
                                   31

-------
   * * * * Compute Surface Temperature Distribution *  * *  *
•  Subtract 1/3 of adiabatic lapse (i.e.,  from sea level to  station
                     altitude)  from observed temperatures, giving
                     estimated  temperature for similar  geographic
                     location and similar  surface thermal properties
                     if the surface were at sea level.
•  Define known data temperatures at proper grid points in GRID -

            T(SEA)  - temperature at X,  Y's for which H = 0;
                      i.e., at all ocean gridpoints;
                      i.e., IF H(X,  Y)  = 0, T(X, Y)  = SEA

            T(SE)   - linear increase in temperature from coast to  SE
                      corner along southern row;

                      i.e., T(X,  1)  49  = SEA + 2—2- [T(49, 1)  - SEA]
                                    43           °

                            T(49, 1) =  T (between SEA and Santa Anna)

            T(NW)   - linear increase in temperature from coast to  NW corner
                      along western column;

                      i.e., T(l,  Y)  tt9  = SEA + ^|i [T(l, 49)  - SEA]
                                    31           1°

                            1(1,  49) =  T(Burbank)

            T(N)    - constant temperature along northern row equal to
                      that at NW corner;

                      i.e.,  T(X, 49) = T(l, 49)

            T(E)    - linear decrease in temperature along eastern column
                      from NE corner to SE corner;

                      i.e., T(49, Y) =  T(49, 1) + |jp [T(49,  49) - T(49, 1)]

               T    - modified observed temperature at the 9  data stations;

                      i.e., At PLACES;   T(X, Y) = T[X(FLACES), Y(PLACES)]

            NOTE:     Temperature not yet defined at remaining points.
   Temperature field initial fit

      Keeping above defined temperatures as boundary values (internal
      and peripheral), solve  V2T = 0 at remaining points.  Note that
      keeping ocean points at T(SEA) effectively moves the boundary
      to the shore.

                                     32

-------
     Compute  V2T at the 9 observing stations;  i.e., at X(PLACES),  Y(PLACES).

        (Note V T  will be zero everywhere else except at shore;  do  not  compute
             V2T  at shore).
     Repeat • • steps 10 times to smooth  V2T.

                Smoothing by interpolation spreads  V2T,  the curvature
                of the T field, so that the total curvature is conserved,
                but is spread over an area around data points.  The limits
                of the spread field expand radially one grid point per
                double interpolation.  In each  interpolation the function
                at a point on one grid is the average of  the function values
                at the four (surrounding) nearest points  of the other grid.
  • •   Interpolate V2T onto GRID.

  • •   Interpolate V2T back onto GRID;   F (X,  Y)  = V2T smoothed.


  •  Re-solve temperature field from V2T = F (X, Y).

  •  Add 1/3 of adiabatic lapse (up to altitude of each X,  Y gridpoint)
     to each gridpoint temperature.  Result is  temperature  field.

           T(X, Y)  = T(X, Y) + .002 H(X, Y)

) * * * * Compute Thermal Wind * *  * *
     Compute
(T-SEA)/(T,_SEA)
H1 - H I     = AH (X, Y)
                 AH is the depth of the atmospheric mixing  layer.
  •  Generate a mask array (GRID)  with 1's where the mixing depth is
     negative (i.e., the topography penetrates the inversion base)
     and the temperature exceeds the sea temperature (i.e., if T -  SEA
     is positive,  the base of the inversion must be above sea level).
     MASK is zero  elsewhere on GRID.

  •  Set  AH  <200 to 200:  i.e.,  set a minimum  AH.


  •  Compute thermal forcing function
     where MASK is zero

           FT(X, Y) = - <<(T-SEA)/jtAH/2)
                                33

-------
The constant empirically relates the updraft to the temperature;
                       a  =
                                w
                             T - SEA '
Compute thermal boundary conditions.

 1)  At W and S boundaries, assume all divergence is along boundaries
     Divergence across these boundaries is zero.  These are boundaries
     along which significant thermal gradients exist.  Isotherms are
     substantially normal to the boundaries.  There is no observational
     data for thermal gradients across these boundaries.

 2)  Assume divergence along N boundary is zero, since N boundary has
     already been assumed to be isothermal (except for small altitude
     effect).

 3)  Assume velocity (V) across N boundary at X = 25 is zero.  Thus
     N boundary is a pure updraft zone of maximum convergence.  This
     assumes that surface temperatures north of the region do not greatly
     exceed those at the northern edge of the region.  Observational data
     is absent outside the region.

 4)  Assume the intersections of the coastline with the W and S bound-
     aries are at equal potential.  Solve (integrate V2$ = FrjO for
     each boundary:
     at W boundary:
                                    9$
                    $(1,1)  =  0 ;   —-  (1,49)  =  0 ;
                                    dy

                              49                y  y
       .'. $(1,1)  =  -(y-1)   f  FT(25,y)dy +  J  J FT(l,y)dydy ;
                              1                 11
     at N boundary:

                        $(x,49)   =  $(1,49) ,

     i.e, constant value from NW corner is used along N;
                                34

-------
   at S boundary:
                     $(1,1)  =  0

                     $(43,1)  =  $(1,31) ,

   i.e.,  $  is equal at coastal points,

                                  49

        .'. $(x,l)  =  X-^1   - 30 y* FT(l,y)dy +

                                  1          '11
                       43 x                 xx

                     ~ If FT(x»1)dxdx  +  Jj  FT(x»Ddxdx ;
                                31 y '
                       i i
                          i i
   at E boundary:
      $(49,y)  =  $(49,1) + [$(49,49) - $(49,1)]
                     49
                         j
                                        y y
                                            •— (49,y)dydy
                                       1 1
   49
48

                                      49 y
                                      / /
   Solve Poisson equation  V2  $   =  F    for  thermal wind potential.


   ) * * * * Compute Topographic  Wind  * * * *
e  Add synoptic (at sea)  surface wind  to  thermal wind
                         U+U,_
                          s     T
                                     x
  V  -
                                     Vy$  .
«  At inversion mask,  sec   AH =  -600  to represent  extreme damping of
   vertical motion.


®  Compute gradient  of topographic  height,  V(--AH/2).


o  Compute local vertical  component of surface wind due  to topography.

                            V$ • V(-AH/2)  -
                               35

-------
o  Set minimum of  AH/2  to  100.





«  Compute topographic forcing function     w   /AH/2 = F




e  Compute net flow boundary conditions



        *_- U  X + V   Y + *_
         BC    s      s       T




«  Solve Poisson equation  V2 = F,rnp for resultant wind potential,




•  Compute gradient of resultant wind potential to give resultant

   wind vector.


                   V = V$




•  Return to beginning of loop
   End
                                 36

-------
    Appendix C:  Poisson Surface Data Fitting Technique





        It was desired to provide an interpolative (surface fitting) scheme


for defining two-dimensional fields consistent with data observed at a sparse


set of randomly located stations.  The specific application for which an inter-
                                                               j

polaticn was desired was the surface temperature distribution in the Los Angeles


basin.  The mesoscale windfield analysis described in the body of this report


requires a surface temperature distribution as a forcing function for the


thermal perturbation of the wind.



        In the Los Angeles experiment, surface temperatures were taken at nine


(9) observing stations.  Although the stations were not located on any regular


grid pattern, they were well spread over the 50 x 50 mile experiment region.


A significant portion of the experimental region is ocean surface.  Although


sea surface temperature observations were not available, sea surface climatology


for the region shows the temperature is exceedingly steady in time and uniform


in space.  The assumption was made that all ocean grid points were at 64°F


during the test period.  Four general types of interpolative techniques were


noted that have been used widely for analyzing gridded fields from observed


data.  They are -


      e  Statistical fits - e.g., "least squares" fits of the constants


         of a chosen functional form (often plane surfaces).


      e  Influence factor fits - the value of the field at any grid, point


         is the sum of "contributions" from each data point, where each


         contribution is the value at the data point weighted by some functional


         of the distance between the data point and the grid point in question.
                                     37

-------
       •  Spectral fits - whereby a family of  surfaces  of  a  periodic

          functional form (sine and cosine waves for Fourier analysis)

          is spectrally weighted to provide a  desired degree of

          approximation to the data points. Spectral filtering  is

          often used to limit the family "membership" and/or to  specify
                                                             /
          the data fitting accuracy required.



       »  Boundary value fits - the value of the field  at  any grid

          point is the solution of an equation given the data points

          as boundary values.



        Each of these approaches offers advantages for  certain classes  of

problems.  Statistical fits are used where there are many  more data points

than there are acceptable degrees of freedom in the fit surface.  Influence

factor approaches seem appropriate when they represent  a conceptual model;

that is, the field at one location is seen to  actually  depend on the  field

shape at points beyond the nearest neighbor data point. Spectral fits  are

generally used when there are not only many more data points than acceptable

degrees of freedom, but there are also many realizations of  each degree of

freedom (i.e., many wave lengths) within the analyzed region.



        Several facts and assurnptions about the surface temperature observations

in the Los Angeles region suggest that the last scheme, the  boundary  value  fit,

would be more appropriate than the.other schemes described.



        It is assumed here that "noise" in the data is  not great, and need  not

be filtered.  Certainly the observational noise is very small -  thermometers

are very accurate - while sub-grid scale variability of the  temperature field
                                     38

-------
does exist, subjective examination of the data suggests that for this appli-




cation the variability is much less than the temperature differences between




'observation stations.  Thus, we want a surface that goes exactly through the




data points, introduces no degrees of freedom not required by the data, and




allows each data point to influence the field very strongly in its own




neighborhood.






        The scheme developed fulfills these requirements.   The equation




                    V2T = F(X,Y)  is solved with T




held fixed at all known or assumed interior data points and at peripheral points,




Specification at data points allows a perfect fit of the data while the form of




the equation and the specification of F(X,Y) (given below) assure that only




enough degrees of freedom to fit the data are allowed.  Specification of




peripheral values lends an arbitrariness to the scheme, but seems consistent




with the view that no analytic scheme can be known to be correct near a region




where data is not available.  Therefore, boundary values which simply preserve




the essentials of the interior of the region do the least violence to our




sensibilities.






        It is desired to define a forcing function, F(X,Y)9that reduces the




surface curvature,  V2T as much as possible in the neighborhood of each data




point while allowing "smooth" transitions between neighborhoods.  That is,




neighboring points should determine surface slopes in intervening regions,




but surface curvature should be small everywhere.  To accomplish this, we




first solve the Laplace equation -





                    V2T =0    (T specified at data points and periphery)




and then compute the Laplacian at the data points (it is necessarily zero
                                    39

-------
elsewhere).  Repeated smoothing of the point values of V2T is carried out




by an operation which preserves total curvature.  This then produces a




distribution of surface curvature which, in a region about any data point,




is proportional to the deviation of that data point from a mean surface.




The smoothing algorithm used first defines the value at the center of each




grid cell to be the average of the values at each corner of that cell.  Next,




the value at each grid intersection is the average of the values at centers




of the four adjacent cells.  Each pass through this smoothing operation




spreads the same total surface curvature to a region one grid square larger




all around.  The smoothing is repeated for a number of times equal to the




average spacing between data points.




        Trials of this technique on Los Angeles temperature data gave




temperature distributions qualitatively consistent with subjective analyses,




with somewhat more detail, i.e., smaller scale content, in the patterns.




        A typical computed temperature field is shown in Figure C-l.




        Several manually drawn isotherm maps from the same data all showed




much the same qualitative characteristics, but the variations between manually




contoured maps were comparable to the difference between each and the analyti-




cal map.




        Required computer time for a 49 x 49 grid  (2401 grid points) with




an ANAL70 program on an 1108 is about 10 sees.
                                   40

-------
                                -2
Figure C-l.  Isotherms (°F) * 10    in Los Angeles  Basin
                            41

-------
Appendix D:  Computer Output
     Contained herein is a set of results of windfield analyses for thirteen

(13) consecutive hourly periods from 5:00 am to 5:00 pm on 29 September 1969,

and one for 6:00 am 30 September 1969.  The first sheet is a listing of the

ANAL70 program.  The next 56 sheets are reproductions of computer printout

of (x,y) gridpoint values of four variables for each time period.  Each

sheet has a computer printed label containing:


     1)  the number of the case (SETS = 1 is 5:00 am, etc.);

     2)  the variable name -

         T   = temperature field (°F) fitted to the 9 data points,
         PHI = computed velocity potential,
         V   = the south wind component in m/sec,
         U   = the west wind component in m/sec;

     3)  a power-of-ten scaling factor; and

     4)  the names of the independent variables, x and y, in each. case.


     The format for all printouts is the same.  The 25 x 25 array represents

the values of the variable on a grid consisting of every other computed point,

North is to the right.  On the PHI, U, and V printouts, zeroes are printed

where the topographic surface lay above the inversion base, a.nd_ the ground

temperature, simultaneously, is above the sea surface temperature.

     Finally, there are fourteen (14) computer-drawn maps, for the same cases

showing -

     1)  topographic contours at 500 ft intervals, the first being
         the coastline;

     2)  grid lines where inversion restricts flow;

     3)  wind vectors at alternate grid points - scale may be
         determined from grid-line interval (vector one interval
         long represents a wind of one m/sec).
                                   42

-------
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  	__L.A. -vir^F-jELu ANALYSIS	

  ) 0. L'«  M^Ot-HJUfi  - -—  ...--.     -- 	
  ) CL'lTtK  FiI.I,,c. C  Cf 49 Y OK X 4-J:0£FIK.  II"  OF-47 Y FROM 2 OF X 49    _	  .. .
—1U I 4-c. »  "r 49 v C.F X i:[£FlNt_ <-.•"  OF 47 Y FKOM 2  OF X 1
--SLrI.«c S  OF Y  1 uF. 49 XJC-EKIM: !,» '  OF Y 1 OF 47 X-FROK 2 -  	
—:VrI-it C" ..'r  'i7 Y FRoM 2 OF  X ?5:OEFInF. NC• OF Y  48.5 OF X ?5
—jth-1.4fe-NwC-Cc -Y-49 Or X l;~l>.l!.c--,.i.JC-!-^C-Y-4.ti.S-.-OF X.AjCCfJ?^ ^EC  OF Y 1 nF-.X,1
—Jcrl.it. ;.LC Ic  V 19 OF X 4v:Dt_KI''C E« OF ? Y FRO" 1 TO 49 OF X 49
—OErI.4E it CF  r 1  Of" 7 X Frtw.1'  4j:L.tFU:£ .'JW OF 19 Y  TO 49 OF X 1		 	
—ricri Jt WuCAbi  cr Y 31 c,- A  I:UI;FINE  SCO'.ST OF Y i  OF x 43
—CLi-Ilu I^u Of  I1', hi FftoM-1 uY  b;'f>:ceFlNC V'tCTOR  OF-  625 PLACES FROM  0   	- --
—aLrl.it. LATA v/r  1 jETSU'Erif't S.-KEAD OF 1  TIMES
	} T***T*«"t*t «t* t*i IijPi.'T »*^^**f^***«^*^^^-***^-*t*'****t*^*»*'t**tt***t***t******
             ;:KF:AD f^/r:Y:r,.>,r  SI,£/H:H GF 4<5 f OF 49 X:RFAD i2
                46
                06-
                71
                DQ
                09
              -ii3
       	137.
               Io8
         	2*2
 2o 1
-295-
 2S5
          10/ _=  1:106 -s 2:iQ9 ==  3:lj6 r= 4J97 ==  l.:6l  ISO == H
          F0i< jArA SET'j      )_»*»*«»»* t*<-4*»************»********************************_
          .READ sO/T;I;.READ 49/NW:NW:.READ t9/SE:SE:.96  = 1C6
         _ )_»»***A»*4.»»*»*4.**_^%_ij^.3.6i:.t,a - ii:.3i MOT  si:.3i * 97:.AT sr.:.3i  == 4«:.AT NW
          .3i-==- 49:.£,1 N:.31~=_ 49;.?y  C' == 31:.AT £:.31 == 25:.i:Y.;.3a *..&i «.-yfeo2t,Jn_6--=.Ji	^	
          ) »***«4*»****jitt» CuMhUTt- UCcKAL Wl.'jD »***********»*** + ******»***»***********
          > 	GtNtPATE  InrK.-IAL Fi,Pcr:3  FO''CTIOH	

          .4i -  si;.41 » ;!0i ii:.41  + ii:.ii MEG ti:.u  » POS .'i
               349
               <,,*;
               3u5

               4o7
               4*7
       	5,9- -


               5J7

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               bob-
               7uO
            •_._. 7,5
  .FrtA'tc G.(IC'l./X»Y:.l 5i == A!.?!  51  == Y:.r>LOT  It21t,51 r6I/X,YjH
  >	r'_oi cuObo HATCHING ABOVE INVERSION	————————
  .A( 11:.PLOT  l,2l/X:.rtT 11:.PLOT 1>21/Y
  .41 MOST cOC.:.4i  l?:.4i - U * 300.:.2) 31 * -.00i:-.2l 7 41 / 52flO:.ll  NOT  - -
  .21 * n:.our  ii»riAiivi-'Vni.k-i:.0"T  2i»SKir/FT               :.n GRID == o
 ~)~	*-^^;^^--~™'*^£^K*ir.~Ttf*rkL-&bw^*nv-.cMwu^m&---~*-~~~"^--*'*''~-*'--'-~*
  .31 C" == 2i:. 33  $Y + 3i:.-'f NC'!.99 MINUS 33                                 )W
  ,J1 W" == 21:.^J  $Y + 3li,3i $Y +  J3.-.AT »:.!! ==-Y *  99-'.AT *.:.ll.+ 31--  ~-)W

  '.31 s"'== i-r:.33'?x.-»-'3i:.3i ix +  33:.AT SCOAST:.IOO ==  31  -			xs-
  .AT Wi.O/,iT; .91  ==  il:.9d - ljj;.9<3  /  43.:.AT S:.31 + X  *  96:.AT s:.ll == 31  )S

  ,AI iitc:.ijc  ==  J?:.AT Nrc:.ui ==  3i:.AT E:.3i — Y *  ioo:.ico * 49.         >F

  ) 	 INITIAL. FlEt.tU  SOLrfE ECW. COKPUTF. VELOCITY COMPONENTS	
  ,9^ + 96:.',<*  /  49.:.AC ani-":.;)!  + Y » 99:.L« »n»si».ni'i.««iooo./x»Y  -   — —
  .OwT il«GRrO/'JHl'T:.OeL > • 1.21i Ji/X. Y
 _)--*****-*»»»< ^J^JM'^^-^Co'-^-Ufl- 4.Jt'.~.UrJAPtHt—WI^-"> ******-***.***».**t-*****.*-********.*****
  .1 t 108;.2J +  U9;.Or:L »,ll,3l,4l/X,Y:.l « li:.IM ll,6r»IO/FT:.3l * 21
  .21 MINUS 31  ^  t:.tl-MOST lC«.:.tl  /  4i:.i'l + li:,IN 31 ,r,RID/PHl 'T —	- 	
  .11 GRID' ==  X:.lt  * iOy;.AT «RT3»:.ll  + Y * 10?!.11 +  3i:,Ifi SlfGRIO/IMVRSN

  ) *** + ****<**«., ^ n t CJTP'.M »«.*•**»********»*•«»*****»*»«•» + »*»**<
  .UEL ,.l,2l.ll/X.Y;.*l 6 -- 311.34  VECTOR -_= u:,37 = 34:.31  41  * 11
  711 REAL. VECTOR  ==  rL«CwSJ.U + .OOi:.14 11 / 25.:.14 +  .5:.17 REAL ROUND 14
               772
               772
          .31 41 *  i:.jvA|nE :H/V:.SHOW  3i/v,r: .i>vi Y iiri7:.34 ==-n:, WRITE 3it3/v --		
          .31 41 »  ^J.-.NAME 3vu:.SHOW 3i/A,Y:.i,.iPLY n,i7:.37 == 31:.WRITE 3i,3/u
         --.K.C-f^-HTtTH-, r4-/ ri-*/-Pt;rt<:«^i	•
                         )
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 .£18.-  .  .- L.A. -WJUDK1ELU AMAHf-SIi		  		AMAL70 PAGE.--- 1 _E3 MAR. 73  18:42:47
         l

           Of-      T(     X,     Y)  II, UN PS  1.0000+02
 ,L4d -.640- ,o40 .640-.640 -.£-'10 ,6'tC;-,640  ,b40  .640 -,{.4G .640 .61*0  ,640  ,64fc-,640 .65E .681  ,679  ,616 ,681_,683 .681  ,6<)5  ,710


 .(>4u  .640  .o40 .040 iutn .f".C .640  .6,0  .640  .640 .640 .640 .640  .6"0  .640 .640 .653 .670  .632  .617 .681 ,682 .6*7  ,694  .701
 • u4U  .640  .j'10  .btO .o4( .f-4B .641;  .640  .o40  .640 ,{4j .640 .ftto  .64(,  .646 .64_0 .645  .665  ,?02  .696 .686 .684  .68";  .693  .704
                                                                               %

 ,t/4j  ,b'iO  ,U40  .t.i.0 ,u4c .f>0 ,6iir.  .640  ,otO  .640 ,64j .MO .640  ,6'IO  .fi'tO .640 ,'6^1  .670  ,f92  .699 ,6»3 .683  .685  .693  ,702
 • btrf  .bmj'.otQ  .bl*0-.o10 -btO .640 .6i*0-.o'tO  .6^C .frtO .6HO--.6i»o  ,6'10  ,6«0  .6i»v  .6i(0  toku  .6i«0 -o'lf, ."HC ^'.Q .6^0  .t,".o  .6"«0 .610 .f'"*0 .f'^o  .61?  .6"tZ  .616 ,6"52 .661  .672  .605 .678 ,683 .686  .693  .700
       .0^0  .olO  .640 >o1f! ,6i,r> .618 .630  .640  .640  .610 .612 .(.13 .644  ,f,41»  .6<|8 .6SS .659  .677  .685 .678 .683 .6P6  .693  .702


       .040  .u40  -640 .&4C .f"lO .6^f .6bil  .644  .643  ,f,43 .641 ,f4(j .644  .b49  .656 .6^4 .658  .672  .687 .67B .683 .6B7  .694  ,7Q2
 .c4u  .tHO  .o4d  .61,0 .04;  .6%? .666 ,6oO  -641  .6,1  .641 .641 .643  .648  .651  .656 .65B  .662  .668  .685 .677 ,682  .695  .700  .710


 • u4u  .bi.0  -fcHO  .6,0 -o4c .6,5 .64? .6^2  .640  .640  -641 .642 .648  .651  .653  .658 ,6f>3  .666  .671  ,6»3 .680 .686  .7fl7  .707  .712
            -t>4C  .6MO--o4f. .6.,0-.63'3-.6i9  .640  • 649 -. f-41 .644 .647 .651  .657 .663 .67fl  .674  .675  .677-.678 - .704  .71)  .715 .744
 .u4u  •fc'-O  '^40  -&4C -j4(j .6.|g .640  .6i9  .63^  .640 .f,4j .643 .646  .651  .658 .667 .6«0  .679  .678  ,680 .688 .699  .701  .732 .752
      .b40  .o40  .6,0-.ol;- .6,0—640  .640  -640  -640  .641 .643 .616  .651  -657 .664-673  .677 -.678  .684-.698 .705-.706  .740  .732


      .640  .olO  .640  ,o4p .C-lC .640  .640  .640  .639  .MO .642 .645  .649  .654 .660 .f.69  .675  .678  .6^3 .689 .696  .701  .712  .756
 .04o ."40  .040  .640' .o4o .640 -6i9 .6^8  .637  .63?-.638 .640 .643 .647  .652  .657-.665 .669  .673  .680 .687 .696 .731  .755 .772


 .64U .040  .o4g  .640 .64f. .649 .6J8 ,6j6  .635  .6^5  .&J6 .638 .641 .645  .649  .654 .6f>l .663  .668  .676 .684 .706 .751  .767 .776
 .t.4o-.040  ,o40  .040 ,e»4c  .f'00 ,6j6  ,6j4  .633  .6^3 .634 .6J& .638  .642 -.648 .653 .6H6  .661- .666-.672 .683- ,738  .75=;  .717 .772


 .04t, .b'tO  .u4u  .6i« .63,.  .6^b .6^4  .6ji  .632  .63? .631 .633 .637  .642  .657 .667 .656".660  .664  .6'Q .683 .713  .739  .735 .772
-,t>4u .040  .040  .<>37 .o36 ,6j4 .632  .6jl  .t>30  .6jO .629 .630 .t-33  .615  .6S8 .657 .656  .660- .665 .670 .681 .724  .713 .735 .772


 .olu -o'lO  .oJ7  .ti5 .1.3.; .6^2 .6jl  .6,;9  ,u27  .6^8 .ft2o .635 .620  .645  .655 .653 .657  .662  .666 .673 .691 .743  .717 .727 .761


- ,o4(J ,030  ,o3b  .6.13 .o3/ .kj,?_ ,&j)  .6^8  .620  .6^9 .fjl .636 ,637  .657-.656 .656 .664  .665  .669 .675 ,6«9 ,715  ,736 ,7?6 ,756


 .t>4J .616  .oil  ,fc^9 ,03,  .f-jj .&j3  ,6iE  .632  .6i5 ,^3U .f43 .649  .666  .659 .663 .677  ,669  .674 .679 .703 .713  .73? .716 .740
      .039  ,o22  .6^0  .6i>r- .6j4 .6J7 ,6^V  .64l)  .643  .645 .649- .657 .669  .670  .667 ,671 ,6f.l  .679  .616 .704 ,725  .713  .716 .744


      .646  .^i?  .fi^  ,o3, .6^'! .fa,) ,6sb  .&47  ,6i,l  .c-,5., .656 .667 .671  .674  ,67i ,67'i .582  .C.C2  .6-17 ,7n9 ,724  .730  .7?! .752
      .o4i>  .1.41  .lo?  .o'»1 .*"i;< ,t3,P ,d^l  .t.56  .6ol  .r'in .665 ,*77 .679  .681  .682 .6«1 .6^3  .6"8  ,6^b .716 .7?4  .732  .738 .770
                                                              58

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 -7U9	---L.A. SilNDFNy.O ANALYSIS	-  - —		 	ANAL70 PAGE- ... _ 2—23-MAR 73  1B;((3:OE






 OR10r>RINT OF    PUi (     X.     Y) IN UNITS  1.0000+01
       . 062. ,j94 .Ii:6-.i5d -.19o -.222-.253. .234  .316 .347 .370 ,tlO-.'*'tl .173  .509  .000  .000 .000 .000 .000-.000  .000  .000  .000






       .087 .ill .136 ,16o .Ia5 .210  «23b  .263  .269 .316 .343 .369 .395 .1(20  .441  .000  .000 .000 .000 .000 .000  .000  .000  .000
  • l)9t  .111 «i2ti . I4b .16.? .Joe .1*9  .219  .2"*!  .263 .28b .3o7- .326 .349 .370  .390  .000  .000 .000 .000 .000 .000  .000  .000-.000





  • I2o  .130 .l4o .Ib5 .164 .173 .1(35  ,2jo  .216  .236 .254 .271 .287 .304 .321  .3tO  .000  .000 .000 .000 .000 .000  .000  .000  .000
  • l5d  .161 ..±63 .104 .164 .Io4- .lu7 .179  .195  ,2'll  .224 .236 -.?46 .258 .282  .000  .000  .000 .000 .000 .000 .000  .000  .000  .000






  • l9,j  ,lQ6'.j.Bl .175 .105 .ID? -1U .IbO  -174  .Iu7  .]9j ,?03 .208 .000 .000  .000  -OnO  -000 .000 .000 .000 .000  .000  .000  .000
 • ^Zj.  .212  .202-.lii& .16<; .H3 .0-iO .OoO-.iob-.163  .173 .000 .000- .000. . 000 -,-000  .000  .000  .000 .000 .000 -.000-,000  .000  .000






 .^S^  .240  .<^b .?-ii° .iS.i ,!H£ .030 .0U0  ,U00  .01.0  .p03 .003 .000 .000 .000 .000  .000  .000  .000 .000 .000 .000 .000  .000  .000
  .c8i  ,2b9 .^53 .?-33 ,io3 .C-OC -000 .O^O-.^OO  .0U3  'POO  -000 .000 -.000 .000 .000  .0^0  .000 .000 .OflO .000 .000 .000  .000  .000






  .31j  .300 .c:66 .20B .^42 .Don .QJO .OjO  ,(,CO  .00"  -000  .000 .000 .000 .000 .000  .QfO  .000 .000 .000 .000 .000 .000  .000  .000
 • -51*,;  .332-.J21 .3il..j,^ -ijn- .3^7 -.349-,^47-.3^3 ..(jOa .000 -OPO .000 .000-000  .0"0  .000 .000 .000 .000 .000-.000  .000  .000






 .i7t  .3u4  ,Jb6 ..15,0 O43 .Jo? .3^0 .351 .339  ,3^'J  .cOJ .000 .000 .000 .000 -000  .000  .000 .000 .000 .000 .000 .000  .000  .000
 ."tOi  .396  ,jfe9 .3»4-.o3t-.37^ .373 .3ua .  .t2o .M5 .411 -''o7 -^JO .^c3 -'129  .441  .138  .00.1 .000 -000 .000 .000  -OnC  .000  .000 .000 .000 .000 .000  .000  .000
--.46j.  .456  ."+bl  .446.--. 442 .Ion .4^7- .442 -. nbO - .4b5  .453  .POO  .000-.000 .000 -.000  .000  .000  .000  .000 .000 .000 .000  .000  .000






 • 49j.  .4at>  .-»B1  .476  ,>»7i .'l;,7 .4'i? .too .q69  .474  .481  .493  .000 -000 .000 .000  .0"0  .000  .000  .000 .000 .000 .000  .000  .000
 02i .516  tJlu  .;.u5--.^0r)  •il'r> •"*'! - ,(»o«-.i»9l-.i»95 .502  .512  ,52b .000 .000 .000-.000-.000  .000  .000 .000 .000 .000 .000-.000





 .55^ .540  ..,40  .J^4  ,b25  .5^? .5j.7 .514 .514 ,5i7 .523  .532  .^42 .000 .000 .000 .000  .000  .POO  .000 .000 .000 .000 .000  .000
 .bflj. .b7o  ,o7o  .bo4  .b57  .'•-».  .&-»5 .540 ,'ji9 ,545-.54b  .5r>A ,R63 .000 .000 .000 .000  .000  .000  .000 .000 .000-.000 .0"0  .000





 .Oil .60o  .ul,l  .jV'.,  .^(!V  .5o?  .b.V1. ,S7j .j67 .5t>7 .£71  .579 .^92 .000 .000 .000 .000  .OCO  .000  .000 .000 .000 .000 .OHO  .000





 -.o4i .637  ,334  .6jO  .035  .(=,JP  ,6^1 ,6u4 ,b99 ,5'j? ,60.j  .605 .f-.SJ .OnO-.OOO .000 .OnO  .000  .000  .000 .000 .000 .000 .OnO  ,000





 .o7j. .6oV  ,u7,j  ,f,71  .06':  .6^1  .0^2 .6-11 . o3b .637 ,f.3fl  .000 .-00 .000 .POO .000 .O""  .000  .000  .000 .000 .000 .000 .010  .000





 .VOo .697  .71^  .7<;1  .72i  ."'ifr  .6^,4 .f.04 . j',0 .OuO .fOj  ,00'> ."00 .000 ,000 .000 .nOo  .000  .000  .000 .000 .000 .POO .000  .000





 • i.oj .oeo  •(>•>')  .7^4  .r-j;,  .70f>  .c *j  .ooi ."Oo .opo .000 .000 OOT  .000  .or>o  .000 .000 .000 .non ,ono  .000





 • oOo .Oi«0  ..lO'j  .'--.,'J  ."0.;  .'u'1  .C--C .OjO ...Oil .OuO .fPj  .Ooi> .«f'(j .000 .Ol'O .000 .010  .000  .000  .000 .0"0 .000 .100 .000  .000
                                                               59

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 —7«cl	L,l..-*i*,W-If.U< -*U«i.YS.IS	.	—	ANAL70-PAGE	3—23 KAR- 73-18:US:02
      bLTS^l

 GRlDHKiNT OF      VI      X.      Y)  iN Uu!T3 1.0000+01
         16<^ .l&O—loO—lt>f.-.JoO  .i;fi .Ji.7-,156—.1!>7—)bu  . 157-- 157--. 157—.156  .118—ortp -000 ..COO -.000 ,000-. 000—.000 -.000 — 000


        .12-* .J.22 .1<;2  .i^i  .1^:5  .l — 112--, 111 — ; 1 j -.507-,, 107 ,106 — 101—103 ,.000  .000 .noO—000 .000-.000  .000 .000—000


   • lit* .051) .ut" .0<<5 .c,"4b  .0;-2  -0<=f> .Oo!> .G?2 .090  .088  .082  .0^3 .OE5 .076  .1?2  .000  .000 .POO .000 .000  .000  .000 .000 ,000
 --.iio-..-013 — oOa— Ow£!-.OfrJ—f_-G3— G-34—.CiiO—C33— 070 --.f,63-. 055 —01S—Ot7_-. 156 —000--.000--.000 .000-.000 -.000 . 000 .000 .000-.000


 -.Olo-.C2C~.o2'l-.Osl-.u5.-l-.Cu9-.Gl'l .171* .CS1 .0<*B .028  .OtJ .070 .000 .000  .000  .000  .OPO .000 .000 .0"0 .000 .000 .000 .000
                  .01>2_.HO_.lolt  .C-00 .OiW)-.ol7 -.Oil -,t-09  .OOO-.OOO-.-OOO-.OOO-.OOO- .000 -.000 .COO .000 -.-00a-.000-.000-.000_.000


                 -.li2-.i5«)-.?^7  .cOrj .CjO .c,00 -OoO .(jOj  -POO .000 .000 .OPO  .000  .000 .000 .COO .000 .COO  .000 .000 .000 .000
 	,^6o_.072_.oS7_.1^2_.i63  .WC  ,0i—t)2l-i<:0 -.0^3-.C-63-..l22^m5_.oOO —COO—00&—000—.000—000--.000 .000 -000 -.000 .000-.000 .000 .OnO_000


 -.jtH-.Ofl-.u3o-.o21  ,00V  ,0^9-.00'*-.C'»l-.c,7o-.Ol9 .COO  .000  .000 .000 .000  -000  .010 .000 .000 .000 .000  .000 .000 .000 .000
- --.U3j-.032-.t)29--.o20--.ulli.0l5--.c-*'1=-li5 . uW-«CoO—.C-DO — 000 — 000-— 000 -.000—.000 — 0"0- .000 -.COO-.000-,000—.000 -.000 .000-. 000
 -.i,2V-.02uOO-.000 -.COO  .000 .000 .000 .flOO-.OOO  ,<>no .000 -.900-.090 -.OOO-.flOO -.000 -.000- ,000
                                                               60

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                                                                                                   ft6C	tt—23 MAR -73.ia:U3:03
         l

          0^       J (     Xi     Y)  JIM  lil'ilTb l.OOoO+OQ
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.l6j ,.1£1 -.086 ^0/4B-.iO<.'^.0<;9-.o6:l-.r.;iy-%ill-.132-.l55--,l79-.2C3-.226-.247--.263. .000 .000  .000 -.000 .000 .000- .000 — 000... 000


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• i1*?  .Ib7  .172  .2j5 .JOJ .CoC .OCO  .CuO  .jOO  .OcO .r.Oo .POO .000 .000  .000  .000 ,pno .000  .000  .000  .000 .000 .000 .000  .000
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• itV .153  ,i£o  .Ib6 .153 .l->7 .239 ,?i»3  .id9  .Ot7 .lOo .POO .000 «OCO  .000  -000 .000 .000 .000 .000  ,000 ^000 .000 .000 .000
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• ib'j .149  ,i<+9  .1H7 .it3 ,!to .131 .H7 .^03  .lal  .103 .309 .pOO .000  .000  .000 .000 .000 .000 .000  .000  .000 .000 .000 .000
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.iU9 .lb .107  ,^d  .t.ol  .J07  ,?y? .20? ,24;> .(,00  .000  .{-Ou  .OCO .000 .000 .OOa  .000 -.0"0 .000 .000 .000  .000  .000  .000 .OOP .OOO


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                                                            61

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             -- L.A.-»lm>fJEI O-rtHAuYilS	--ANAL70 PAGE	S---23 .MAR-73  1B;<43:29
         s=2    .                                         •     •

  6KJDKFUNT  OF      T(      Xi      Y) IN UUITS l.OOCO+02
 - .o4o.<>40  .o40-.640-.o4» .640 .6*e-.640--,6tO-.640 -.640 .640-.640 .6*0  .610  .640-.653 .081 .679 ,6B6-.6fll-.683  .688  .695  ,710  -


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, --.o4j  .640  .o4&  .6^0 .040 .6tO- -6tB .6^0 -.640 -.640 -.f.40 .643 .643  .645  .645  .648 .655 .659 .677 .685-.678 -.683  .686  .693 .702 -


   .64u  ,640  .t.40  .640 «t,4n .640 .669 ,6t>9 .645 .643 .(,44 .642 .{.40  .645  .650  -657 .655 .658 .672 .6f7 .678  .683  .687  .6q4 .7fl2
 -; .o4u  .640  .o4C  -DtO  -o4i-  .61,2 .667 ,6t,a .644 .644 .644 .643 .644 .650  .653  -657 .659 .663 .669 .685 .677  .682  .695  .700  .710


   .64u  .64U  .040  .640  .o40  .6^6 .644 ,6^S .645 .645 .645 .646 .651 .654  .656  .660 .664 .667 .672 .694 ,68Q  .686  .707  .707  ,7i2
                       X
_ .640  .640  .o40  .640  .040—6.4^ .642 .645 .647^.647 .(,4d .650 .651 .655  .660-.666 .671 .675 .677- .678 .679_.7o5  .71?  .'716  .744


   .6,40  .640  .o40  .b40  .o4o  .&40 .6>»1 .640 .651 .651 .651 .650 .652 .657  .663  ,67o .680 .681 .680 .682 .69fl  .701  .702  .732  .752
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	.04^  .640  .o40-.640-.o40  .&-*0—.640 .64^ .643 .644 -.644 .646-.649 .653  .6&0  .666 .674 .677-.681 -.6S6_.691_ .700  .734 -.757 .772



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  .otj  ,640  .o40  .635  .o3i  .6jQ -.6^8-.6^7 .o25 .6^5 .625 .625 .626 .642  .659 -.662 -.665 .672 .675 .678- .690 - .728  .745  .736 .772


  ,t.4u  .640  ,o35  .Aol  .029  .6^7 .6.'i5 .5^3 .o20 .f>ZS .(££ .628 .610 .640  .654  .655 .663 .669 .673 .679 .695  .747  .749  ,7?8 .764


  ,04t>  ,t,3b  ,o31  ,0£6  .024  .-6£4 .6£4 ,632 .636 ,63d -.643 .652  .664-. 667  .665 .677 .681 ,6f>0 .6%  .70^  .725  .713 ,717 .744


   .037  ,63J  ,o26  .t'u9  .,,23  .f,^. ,6i1 .6^7 .640 .641 .6'i4 .651 .66i  .-',67  .670  .66B .672 .680 .*>?! .686  .709  ,7?3  .730 ,7?1 .7S2
        .636  .u3
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--7y9   .-  --U.A. «I,,U'ia.O-WWLYiIi	      	    	  - -	      -   .  ANAL70 PAGF.  —  6-23  MAR-73 lfi:H3!45






           OF    Phl(     X.     Y) IN UNITS  1.0000+02
  «015 -.021 .026 .0-5?. .0-53 .Ct3-.(,H9 . .Os'l  .0&0 .065 .071 .076 .082  .008  .000 .000 .000 .000-.000  .000  .000 ,000 .000






  • U09  .01-5 .ulB -C22 .027 .03] .flif' .C1'!  • ;)"»&  -050  .055 .060 .0&1* -059 .C73  .077  .000 .OnO .000 .000 .000  .000  .000 .000 .000
       .01? ,j2C .C<:4 .j27 .030 .C-5'.' .CJJ -jlB  .OfG  -r-Sj .05t2  .<}'*& ,0'l9 .Q53 .QE6 ,Qb9  ,0f>2  .010 .000 .000 .000 .000  .000  .000 .000 .000
  .1,2-*  .02a ,,,2b .026 .527 .027 .029 .032 -i,35  .039  .p$  .u'J1*  -Cb3  .^bS .0-i3 .0^"3 .Oi& -C58  .Ob's  .000  .000  .000 .000 .000 .000  .000  .000 .000 .000 .000 .000  .000  .000  .000
 .06i  .060  .Ji>9  -GliS .OM-.037 ,0'JS .Cj5 .U57 .00^  -000  .000  .000 -000 .000 .000  .000 -• 000 .000 .000 .000 .000 .000  .000  .000






 .  .000  .QOo .000 .&00 .000  .QOO  .000 .000 .000 .000 .000 .000  .0"0  .000
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 .iO/ .109 .j.lu  .111  .il»  ,lm .li't .)j.t .113 .H3 .112  .000  .O0u  .000 .£00 .000 .000  .000  .000  .000 .000 .000 .000 .0"0  .000






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                                                              63

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                                                                                           JlUALTO-PJleE-  ----- 3-23 KiR .73 18:«3:U6
                                 Y) IN ijUITS l.OCOO-iOP
                                                .-£7»--..i75 ,274 .?75—277-.?79—S?8 —000 — 000—000 -.000—000 --.000 -000 -.000 -000






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 .16.U -loo—16<»  ,lo?. -l6f. -.4J6 .190 —2u.i—210 -.?.l>9-.20<» .203 .19d .lB7-,lf)b  . 1<*9 -.000 -. 000 .000—000  .000  .000 .000 - 000 — 000






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 .t)5ti-.Ot7-j'U—3j3 —o£9—ft*l .0^9 . 1-u'J—l7t—li*3 —132 .1?3 -.1-33 —lia .1CS — 000 — 000 -.000 .000-000  .000 -. 000-000 .000 .000






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                                          ,-ull—.OV1 -o«9 -.000-. 000 -,900— 000--.OHO-.OOO—• 000 .000 .000 -.000—000 — 000 — 000-.000






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           «-L.A.  *H,OF1ELO-AHA1.YSIS	  	    —	ANAL70-PAGE	8 -23 MAR 73 18:143:16


faftlOr'KINT OF       U(      Xi      Y)  IN ONIT^ 1.0000+CO  '
      .175  .125  .070 -.olit-.C37-.0-it-.1.27-..l62-.19 121-. 3-.-J-. 220-. 108-. l-i^-. 2Q7-. 2C2-. ?Co  .000  .166 .000 .000 .000  .000  .000  .000 .000 .000 .000 .000
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                                                             65

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                                                              66

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-709   ---   -~UA.  tvl,,bFlEI 0  hNAuYilS -	 	-       	ANAL70PAGE-   -10 -23-KAR-73 1B:M4:33-
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                                                             67

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                                                              68

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             -l..A.-*I:,ui-lfEL.O -«KALYSI5	.	RNAL70-PAGE	-12—23 -MAR -7



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                                                               69

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                                                                 70

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                                     S-		-/U1AL70-PAGE—  -l«t-i3-MAl -73-18:U5:21. -  _






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                                                               71

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    21	--U.i.-»IW;FIfc.L4> AWAiJfSIS	•	ANAL70-PAGE	J.5—23 KAR 73 -IS-USCIS .
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 -744-	 L,A. *I,.Urin.O-Af:Al.¥iIS	ANAL70 PAGE     16-23 MAR 73 18:145:26
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 .1)7^  .0;;^  ,U87 .CSL.9? .r-j'-i ,j;r .li,.'.  .105  .l^
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                                                                                            AI1AL70-PiGE	19_23-MAR-7-J-aa:«6il7	
  feKIOPfUNT OF      Vt     Xr     Y)  IN UNITS l.OOOC+Cl
              ,i59-.2ba.-.257--.2;>&-255 —2jU—251—256—25iJ-,261-.!?6b_.27i_.277-,.232-.0<>0—000 .000-.000 —000-.000 -.000 .000 -.000






        ,256 .^53 .252 .£53 .2a6  .259  .2ol  .260  .255 .213 .?3S .225 ,201 .166  .057  .QOO  .000 .000 .000 .000 .000 .000 .000  .000
  _.i  .266 .261 .237 .208 .166 . US-.037-. 101  .000 .000 .000 .000 .000 .000 .000 .000  .000
       —.220—217 -JUS—/IT—.231 -239 _3i>U_.316_265-_2J6-^?o9— 156— 101—.C3B-- 050 -.000 -.000 — 000 .000-.000-.000 -000 .000  .000





        .20^'.^03 .191 .181  .liio .237  ,5b&  .319  .238 .222 .?S3 .111 .003  .fl62  .061  .o?5  .000 .000 .000 .000 .000 .000 .000  .000
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             .^02 -1-70 —111-,GOO — 000-00^—1?9--»000 -.o55-.000-.000 .000 -.000





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   .«;8y .261 .«;96 .327 .389 .1-40 -107  .3j7  .151  .106 .101 .071 .051 .031 .010-.0l1-.007  .Q16 .o"5l .072 .000 .000 .000  .000  .000






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   .«;9o .299 .30<> -3lB .332 .340 .337  .267  .135  .112 .0^1 .077 .061 .Oil .019-.011  .Oil  .017 .037 ,000 .000 .000 .000  .000  .000
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—.£6a-.2a6-.^66 .262-,£51--.^ifi  .-162-. 11?-.a79-,«S3-.{v26 .013 .O35-.O02-.000-.135  .010-.011—01S-.OW .000-.000  .000  .000 — 000-






   .t5o .258 .tStJ .262 .«U3 .Io9  .1^1  .lul  .066 .016 .019 .088 .013 .169  .COO  .019  .039 .020 .012 .016 .000 .000  .000  .000  .000






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                                                             76

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                                fJAUfil;.- -			AUAL70 PAGE  — -20—23  MAft-73 -18:»6: 18
           5

            OF      l/(      X.      Y)  IN UNITS 1.0000 + 01
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   .180 ,i70 ,i62 .155  .119  ,l-*6  .l-t9 .Ia5 .163 .166  ,]61  .115  .115 .065-.013-.C50  .010 .000 .000 .000 .000  .000  .000 .000 .000
  -.l9l--.176-.l61 -.153 .. lls  . 14C>  .U3-.154—16B-.176 .174-.l63-.1tl.lOl -.019-, 030 -.000  -.000 -.000 .000-.000  .000-000 .000 .000


   • l9i  ,17ti .i&D .Ibl .137  .125  .1^7 .1 ol .161 .195 . ] 97  . ] 93  .102 .161 .132 .0^5  .000  .000 .COO .000 .000  .000  .000 .000 .000
    l9l  .179 .j.6o — If9 -,12? _( »a  .0,13- .143-.212-.227  .£<23 ,?31-. ?3i>-.2?l4-.J-3G .373 — 000--.000 .000 - 000 .000—. 000 -000 .000 .000


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, — Id*  .186 '.±61-.170 .147  .Il5-.0o0-.0s/e-. 499 -.311-.407 -,000--.355 -.273-.234 -.240 - . ?33 -. flSO -.000 — 000 — 000 _000 -000 — 000 -.000


   .ia/  .193 ,;93 .198 ,i90  .24"  .QOO  .OjO .uOO .551 .330  .J78 .205 .198 .209 .211  .156  .115 .000 .000 .000  .000  .000  ,000 .000
    3-«  .2ol ..^19 .iid..255 -.00" -.QUO  . 0^,0 -• 1^0 --.275 -^ 201  .1'I2-. 1 
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 -20B	-_L»A._tt lOlfliLD-^faLjrSlS	-ANAL70 PAGE	2L_23 .MAR -73 -IflJ 16 :19 . _.
     i£lb=6

 iiKlWRlNT OK       T(      X.      Y) IN IMITS 1.0000+C2


 _^o4-U — bfcO-.o40—640—b40--6<«0—6,40—640—640—640 -»64o—6lfO—640— 640 —640 — 6«0 -,681. .125  .7tt6_,775 —792 —816-.844 ..87?. .9J.O


  ••04U .010 .040  -t40  .o4o • "•*'-> ."41? .640 .640 .640  .640  .640  .640 .640 .640 .640  .674  .717  .754 .781 .797 .819 .845  .873  .904
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  -.o4u .640  -o40  -6tO  .64c  "&40 -657 .7i7 .766 .777  .77d  .777  .783 ,79j .800 -.806  .800  .828 .843 .857 .875 .892 .896  «9/>9 .952


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  .640 .640 »o40  .640  .o4o  .640 -6So .7J.5 .746 .769  .784  .796  .808 .820 .832 .843  .855  .851 .863 .871 .879 .902  •''t*  .966 .976
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                                                              78

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-709        -  L,A.  nI|..rJFitl O .ANALYSIS .   -- -   	 .-   -    	 -         -  -  -  -  --  --  JIMAL70  PAGE .    22 . 23 f'AR 73  1B:U7!10
    bElb-o
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                                                            79

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 .-7,U	- t.A..»I*lDfIEt&-*NAUi>IS	    	  	-ANAU70-PAGC- -  23-25-MAR 73 Ifltll7:ll
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                                                             80

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              L,A.  *ll*ritlO-AlJALYjJS	.	   	ANA1.7C PAGE	ft -23 MftR -73 1B;U7:U
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        2«:0-.<:S3 .Jo^—i^'J -. J j7-.o27 —CWh- .^ft-.Oo?- — {.S1;! -, 007 _. n£2_07-0 -0&1 -OS1--. Q16-.015 ,012-.017-.[|90 -000--000- .000 ..000


       .210 .^3i .iZy  .241  .Iu3 .O'JJ .O^  . ;,.18  .011 -C.S3 .052  .0E3  .053 .Q5? .016  .Q13 .0?6 .011-. 005-. 0?1 .000 .OOn  .000  .000
     / -.20" .«il2 •ili'-,l9i .H*) -0'-r' -.051--.021 -035 .(,33 . 03&-.r>3<* —OlO -.(}39 -.. 036^.fl2& -,037_.flS9 -. 010 ^000 -.000—000  .000 -000


     J .200 •J.'5y .1^1  .173 .1-*'! .Iu7 ,OVi> .ju3  .0-<9 .f3a .032  .n26  .026 .025 .028  .0-39 .051 .o36'.01g  .037 .006 .000  .000  .000
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 .<:0u  .19b .169 .IbO  .ICft  ,l-*9  .117 ,?o6 ,U33  .031 .c2J .D12  .p05  .003 .010 .030  .03H -026 .02? .015-.00?  ,000 .000 .000  .000
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  71      T  jf  'J rc.ACL^:-;' lj r'l  -'1  J7 ~i! 1'" fl tl?                                     )11  6M
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                                                               81

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 -218	--L.A.  (.luOFItLO-ANALYSIS	  —-   	ANAL70 PAGE	25- 23-MAR  73 lBt(t7:il3
oRIOHRINT  OF       Tt      Xt     Yl IN ONUS 1.0000+03
  .Ok*  .064-,(,64  .Oo4-,u6i» .Oo4 .flUI* -.064 .064 -.064.-, 064 .064 .064  .064  -0&4  .064-.fl69 .074 .076 .080 .082  .085  .O^P  ,092 .096






  .061*  .064  ,u64  .064 ,06<1 .Dot .Do1! .fl&4 .064 .Dot .06"* .061 .064  .064  .064  .064 ,0&fl .073 .077 .flSO .083  .085  .08ft  .092 .095
  ,U&4  .064  ,o64  .064  .064 .Oo4 .064- .064 ,c64 .064 .064 .064 .064-.064 -.0&4  .064 ,0&7 .075 .080 .082  .084  ,086  .089  ,0P2 .095






  .u6*t  .064  .064  .Co4  .ubit ,0u4 ,0i4 .064 .364 ,0o4 .064 .064 .064  .064  ,0£4  .064 .069 .075 .080 .083  .0«4  .087  .089  . 0P2 .095
-.064  .064-|.0&4-.C&4 -. 0°4 .Oo4 .0=>4-.0o-l .4- .Ou5 .066 ,o&4 .064 .fl64 .068 .Q71-.073  .074  .075 ,077 .flSO .083 .086  .087  .089-,09l  .0^3 .095






       .064  .0&4  .Cu4  .064 .Oo4 .0&7 ,06d .^67 .QoB ,o7o .074 .080  .078  .078  .079 .QflO .0«1 .084 .068  .QB8  ,o9o  .092  ,0q3 .095
       .064  .0&4  .064^.^64 .065 .0"9 .Ob9-.o7o .072 .074 .076-.079  .080  .oBfl  "081 .0B2 .084 .086 ,0«9  ,Q9o  .091  .093  . Oq4 .096 --






       .064  .o64  .oo4  . fl6!( .065 .0*7 .070 .^72 .074 .()76 .078 .£180  .081  .082  -083 .fl84 .Q85 -0B7 .091  .Q92  .fl92  .095  .Oq5 .096
       .064  .u&<*  .064  .064—<;o4 .fl6.Z-.071 —fl75 .o77-.fl79 .n80 .Oal  .083  .o&t -.095-.Q86 . QS7- .Q89. .090  .091  .094  .095 .0^6 .099






       .Q64  .j64  .064  .gbn  .0^4 .0"6 .073 .u79 .061 -o8l .082 .063  .OE4  .066  .087 ,fl87 .089 .090 .091  .092  .094  .09"5 .098 .100
-.U6<*  .064  .064  .064_.()64~-.<.o4-.o°4_0?4 -.o87-.083-.p83 .083 .084  .065  .087-.089--.o9fl . 090-.091 .092 . .094. .095  .095  .0^9 ,098._.
       .06-*  .U64  .064  .0614  .Oi>4 .0^4 .073 .080 .082 .083 .084 .385  .086  .088  .091  .Q91 .091 .092 .092 .093  .094  .095  .096 .101
 .064 .064  .^64 -.064,.o&4 -C<-4 .066-.073 .fl78- .081 -.082 .084..085  .0^7  .Ofl9  .090 .091 .092-.092 .093 .093-.094  .098 .100 .102 -






 .064 .064  ,uu4  .064  .064 .Co<* .069 .073 .j77 .ObO .082 .084 .Q8B  .087  .088  .090 .091 -092 .092 .Oq3 .093  .096  .100 .102 .103
 .o6n-.064-.0&4  .064-.664-.067 .071-.074 .077-.060 -082 .084 .Q85- .087  -088  .090 -.Q9! .092-.092 .093 - .093-.099  .100  .100 .102






 • 06-*  ,064  ,06'l  ,066  ,U68 .070 .073 .076 .0?8 .061 .0^2 .084 .Q86  .087  .O^O  .091 .fl9] -.093 .092 .093  .094  .096  .099  . Oq9 .102
--.t,6'»  ,064  .004  .OoS-.ti?!  ,073-.0'5-,078 ,o2 ,0u3 .u»4 .064 .085 .086 .087 .089  .069  .089 ,oql ,091 .091-.092  .Q94-.097  .096 .096 .099






 .o74  .07U  .U80  .Oo2  .082 .Oa2 .03? .''-iJ .084 .064 .cn5 .0.16 ,c07 .OflO  .069  ,0fl9 .Q9Q .091 .091  ,092  .095  .096  .097 .097 ,100
       .060  .u"0  .OhO  .Cl?l  ,"u]  ,082 iOo4 .yU4 ,0t]5 .C8S .006 .086  .06U  .QB9  .089 ,o°0 .090 .0°! ,0°2  .095-.096  .097 .09B .102
                                                               82

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         _ --_L,A. --tiOirjei C- AMALYS1S-- -   	  —	  	 —ANAL70 PAGE	2G-,-23 .MA* 73 18:i|B!05
         =7

           OF     Plli(      X.      Y) IN Or.ITS 1.0000+03
       -OiA  .j21  .030—V3:, ^C«, ^tu>5--tuj—G71-.C79-oBa .096-.1 05-.113-. 1^2—1 32-.000 ^000 .000 .000—166—177-.185 .193  .199


       .Old  .027  .035  .o't'l .052 .Col .070 . 079  .067 ."9o .lot .112 .120  .126  .131 .000 .000 .COO .000  .1B7 .1Q1 .194 .1«6  .199
      —024 .U33 .041  .050 -C59 -.oo£..677—066 — 096 .104  .112 -l?u .127 . 13P -. 136 . 139 -000 .000-000-.000  .202 — 200 .199 .198


       .030 . j39 .o-«7  ,[,bj  .r.oS .071 .Od't . L!95  .1L,'I  .113  .121 .126 .135 .l»»o  -I113 .000 .000 .000  .000  .206  .206 .203 .200 .198
   U2o -03o'—04i .0^3 -.,.61 -.(WO -.C-S& .091—.1-03-.11«—123 . I J 1 — 1 3J-. I'.1*- . 149 — 153 - 157—000 -. POO—000  .20B-.207—204 .201 .198

           .<

  • i)3-» "042 .oSfl .Obfl  .0G6  .P/t .0=3 .097 .113  .1^5  .13H .142 .1Mb . I5'l .J59  .162 .1^6 .l7l .]80  .000  .2n6  .205 .203 .201 .199
            .U5u -.U>"»-.J7^  -.«73 .GOO— OuO-.l£a -.13£_. jito-,153- .lS9-.ie3-.lU6-. J69..172 . 175 .. 179. .000  .203 _203 -.202 .201 ,200


            .U63 .1,71  .(,70  .flj3 .000 .3,,J -uOO  -153  .l^d  .It3 .16t> .lf-b .17(j  .17H  ,]7f- .179 .162 .0(10  .199 .200 .200 .200 .200
   ljSt-.Ool .u7o .C73- .U6b  -Cj" -OOP -.OjO-.lW> -lu?  • 1"6  - 1(.S—17& .172 -.175  .177  .179 ,l3l .Ifil . 190 -. 195-. 196 .197 .200 .?01


   U5o .066 ,,,77 .Oo7  .^9^  .twC .139 .lao .163 .167  .[7o  .172 .173 .175 .]77  .179  .iPl .162 . ] 8t ,1B8  .192  .192 .OOn .Iq9 .?02
_-^u6t —071 .jS5 .c*£>-. iC^ —l^S — lH5-.lao ^165 _.1(,9-^ J72 — 1 V»— I7o — 178 ^j79-.lBJ_. jBg _.l83 . l£5 ^ 137 -,.189 — QOO -.OOn .0"0 ,2n2


  • 07u .uSi .u«<; -ij1*  -ilc.  ,1J? .l-»n .loo .!67 ,17C  -573  .376 .178 .179 .jBl  .182  .lf*3 .lP  .J.,6  .lS5-_lo7- .171-.171* -.]7o -.178 .180 . 162 - 183 -. 1^1-.!«'»—166 - Ifld .JS7 , IBS — l9j ... 000 .201 .203


       .l&t .^17 .1^9  .11;  .1 = 1  .162 .lotJ .172 .175  .177  .)79 .180 .18?  .183  .184  .185 .166 .187 .117 .1«8  .000  .19P .201 .201
  .lOo .112 -i?i .lit  .;".'.•  .Iaft-.lu5 -.17j .173-.175  .177-.179-.ISO-.182 -.183-.185-,!h6-.J87- .187_188 ^188-^000-.J9B .2P1 ,2n4


  .lOu .lib .i^9 .liO  . iD]  .lo'-i  .165 .170 .173 .175  .177  .176 ,i6u .181 .163  .186  .1 «7 .1"0 .IBB .1B8  .181  .000 .000 .010 .?(|4
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  •llo .liC .i42 .1^1  .i5j  .to3  .Id7  ,17u .173 .175  .]7o  .178  .179 .1*1 .165 .117  ,]BB .1P9 .119 ,1«9  .IB" .193  .191 ,0"0 ,?05


  .i3<. .157 .i".7 .!:,<.  . Ib'J  . loi  . Io7  .12 .186 .137  .IBB .189 .190 .190  .190-.000  .000 .OPO. .205


  • l3i .142 . ibO .ljf»  .!•'),-  .loT  -lof-  .lo'J .i7l .173  .175  .177  .179 .!«? .166 .117  . JflO .190 .190 .191  .000  .000  .000 .OHO .Ono
       .14S> .ib2 .IjO .iS1"  .!L2  .luc  . 1 u-i .1/0 .173 .l7b  .177  .179 .1S2 .135 .1*7  . 1"B  .1?!  .191 ,1°2 .000-. 000  .000  .0"0 ,?06


       .11,^ .i5J .ID.. .;:..•  .Jo;  . IMi  .Jj/ .j69 .17"- . • 7-»  .176  .179 .1?2 .185 ,!°7  .l«f  .191  .1«2 .193 .000  ,000  .OOP  .0"0 .206
             ib'l .1-)".'  .;-•'-  .Jo!  .1-1  . lj-i ,j69 .171  ,;7i,  .170  .'.74 .I"! .lt>3 . ! •' &  . 1W.  .190 .193 .196 ,0no ,000  .OOr  .0^0 .206
                                                               83

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—7£1  --  - J--L.A.-*IU;FILLO «NAi_YiIi	— -  -      	—	ANAL70 PAGE -- 27- -23  MAR  73  18:18:05






 SRIDr'RINT OF      v(     X.     Y) IN UNITS l.OOoO + CZ
       -,013-.UU2-.OH2 .ol? .0*2-0*1- .041-.G:'l  .042 .012  .012  .0"*3  .013 .oil .037 .000 .000 .000 .000  .026-. Oil  .038  .031-.030






       .011 .013 .012 .013 .013 .0*1 .011 .oil  .043 .(-U2  .OH  .039  .037 ,o31 ,C12 .000 .000 .000 .000  .031  .011  .011  .012  .015
--.oil .013 .1)13 .013 .(jl3 .015 .0-.6 .017^016  .015  .f.12  .039  .036  .032  .025 .016 .006 .000 .000 .000  .000-.008-.OOB-. 001-.000






  .013 .01-2 -u12 .013 .31114 .016 .0-19 .OD2 .051  .017  ,c12  .038  .031  .029  .022 .011 .000 .000 .000 .000  .027-.012-. 015-. OH-.011
--.fc12 .012-.042 .utl .0'12 .015 ,0'->3 >C°2 ,c57  .019  .t12  .037  ,c3i  .028-.023 .018 ,o?l .000 .000 .000  .000-.010~.0l5-.0l3-.015






  .b1 -o73  .010  -c-37  .033  .021  .020-. Oil .017 .017 .016 .027 .000  .003-.001-.006-. 006-.007






  • OU .013 .oil .037 .331 ,ca6 .03'} .OjJ .000  .023  .C^O  .019  .COU  .013 .Qll .019 .oil .011 .0?B .000  .007  .003  .002  .001  .000
---.l>1o .01,5 .043 .Oj9 .032 .060 .000 .5^0 .aZl  .£).<)  .015  .CjO  .10?  ,0l2  .013 .012 ,0<>e .OlO .018 ,0u5  .006  .003  .015  .008 .007






  .019 .o-)9 .013 .016 ,o3"4 .000 -065 .0/2 .Q25  .016  .ell  .008  .OlO  -010  -009 .OO8 .008 .OOB .010 .028  .QO?  .005  .000  .008 .020
  .^5^ .053-.U51 .06fi .,>71-.li,l .o'/5 ,052 .()26-.Oir>  .{il2-.CH  .OlO  .008 "007-.006 .006-.009 .010 .Oil  .002  .000  .000  .000 .022






  .U5» .056 ,j53 .063 .072 .07" -075 .015 ,&22  .015  -ell  .011  .009  .007 .006 .001 .005 .007 .007 .005  .009  .031  .007  .000 .001
—,j5/ ,05d .059 .«o2 .u66 — Co9 .0^9-.Oi8-.£,l7 - .Ol&  .013  .011  .009  .007--.005-.003-.001 .005-.006 .001  .016-.000  .OlO  .000 .000






  .l)5o .O5t) .j59 .QUJ .jo? .oo3 .0"! .033 .Ul7  .Oil  -C12  .011  .009  .007  .005 .002 .flOl .005 .005 .005  .012  .016  .POO  .018 .013
 -.()Sd-.058 .ySa-.05? .oS9-.C58.oa7.0^9 ,015  .012-.£,11 -.010-.008  .007-.005 .OQ3-.005-.001 .003 .005  .007- .011 ..000  .016 .008






  •fl5o .058 ,jb7 .057 .057 .Ci5 .0'*7 .021 .Ql5  .Oil  .010  -008  -006  .007 .006 .005 ,fl06 .OO3 -002 .003  .005  .000  .022  .015 .012
  • 1)57 ,o57-*,)57-.J56 ,O55-.060 .0-53 .020--.013  .010  .OOft-.OO7  .007  .007-.009 .OO'-.flOS—.002 .002-.002  ,00"-.000  .017 ,016 ,012





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  .u54 ,05
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           --L.A.--.I,.!*IUO-hHAl.YCIS-		. -  		 -AHAL70 PAGC  	28_23 .MAR. 73 .ie:«ia:06  -
   SETS=V

       JT OF      01     X,      Y)  ill  UNITS 1.0000*02
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.G31--.030  .029 ,(.;&-. i,26-.021--. 025  .1.31-.046-Ofal—652—051  .OH9-.-Oia-.W9 . 052 -.0S6 — 000 -000— 000-.003-. 003—001-.002 .002


.H3l  .030..030 .Ofc9 ,j25 .ClB  -Oil  • 031  -031  .023-0^3 .00o--.00tt — 0a6—073 -.0-63 -060 -.(T4-6—. 03H -.025 — 0?8 -. 026 -.017 _. 005 ^ OOO-.-Ol^-^OlS-.OOg-. 003. . 004



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     ,03-1 -.i>36.-C^O -.o11--«CoO -000  .000—031-»C33 ^p2fa -020 —f>la-.019_01fl -010  . OlO -. 009 .005-. 013^. 016-. 019-.012-.DD2 ,P01


     .031  .Q33 .c.i.7 .066 .000 .OJ'1  -Oo9  .flU -OlS .nil .013  ,pl6  -.015 .Oil -008  .On6  '005 .005 .001-. Q11-. 017 .000-.002-.P01
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.L'3U .031 .C'31  .039 .Oi'l .015 .[C6 .ru2  .U01-.000-.p01-.00  .003 .000-.001  .000  ,001 .001 .001 ,007  ,000  .000  .OOP-.000


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     .OJU  .U0d  .OC2-.030-.rc?-.0'c''-.C|^b-.L'0'<-.Ol,"'!-.f.02-.OOl-.rOO-.D03-.005-.no3-.oni-.000  .P01 .010 .000 .000  .000  .000 .003
• liio .Ol."- .{/O^  .OjJ  .LGl-.rCl~.',")".Ci,l-.u'33-.r._'!'-.r03 .002 . "0 J-. B06--.010- .PP9-.()01-.001  .003 .013 .000 .000  .000  .000-.005


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                                                               85

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 	218	--4-,A,-»lN;iFICLD-AtMLVSJS	  	HNAL7.O PAGE	-29—23 MAR 73 18JH8:M
      SE1S=8
  GIUDPRilJT OF       1 <      X.      Y) IN UNITb  1.00CO+C3
      .4—064 ..o64~.t;64-—G&4 -064— Ol>» ..064-.0&U —06»—G&4 ,064-,o64—.064—064.-.;»64 —064 — <-64 -P&<; -0°4 ,0i>4-..o64—064 ^064 ,.064- ,p64 ..06»l — 06^_064 -.068 -.076 _.o82  . 095—087 —0^0 -093 .,096—100


   .1)64 .Dot  .U&4  ,0ot  .064 .Co4 .001 .Out . 0&4  ,064  .C&H .06"» .p6»6t — r.6'l-.<'6'* -.06^— 064_^o6l»-.06fl-»o73--.o7T .062-. 036_ 088-^091 — 09i(_ 097 _100


    U6l« .Ool  .0&1*  .Col  -064 .0611 .061 .Dot .064  .Ool  .064 .064 .064 .067  .069 .tflZ .075 .079 .083  .087 .0«9 .-092 .095  .097  ,100
__ .0&H--.06U-. I)64_fro*-.v6* .Del— .O6b-.&o&-.0o4-^064-.oi4— 067-. 0^9—071—. 073—0-75 ~.o7B-^081_ 086  . OS9_.o9l— .093--095_09B_.100


   ..&64 .ot,i»  .yOl  .Ool  -u61 .Oo'4 .0&7 .OoB  .067  .Oo8  -0&9 ^071 ,c74 .075  .077 .079 .08! .083 .fl87  .091 .092 .095 .096  .OqB  ,100
        ..064- ,U64-,064 _j6l, -.065 .0&9 -,0->9— 07t-.O71 -,c,73-,l>74_.|;76 — 07B_^7-9—.<|8l-.o83-.0B6--.oB9 ^093 -.094—.096-.098-.099--.101
        .064  ,ofa-»  -Ot)4 -.o6i( .Ot>5 «0o7 .070  .073 .075 .C76 .077 .Q79 .081  .of>2 .083 .0B5 .O"8 ,091  .095 .098 ,Q98 .100  .100  .101
                                                                      -.083—.QB1—.366 ..Qfl7 -»o90-*092--.09-*_096—»100—.101-. 101-.101


   -.064 .064  .0&4  ,0o4  .1,64 .Ool .0°6 .074  .jBl  .063 .fB3 .083-084 .085  .fl87 .088 .0^8 .091  .093  .095 ,097 ,Q99  ,()99  ,103 .105
	.^6H_064_.o64^.0o4_-.o64-^4-.85-r687—,e89-,090—.092—.093-.091*—.095—096 -.096 -.098—.103^-. 105--, 104—,107
        .064  .064  .066  .069 .071 .075 .079 ,oB2  .084  .086 .088 .o9fl .091  .093 .095 ,fl95 .096  .096  .096 .098 .101 .103  .103 .107
	.U6-* .064 .064  ,069  .07S- .9l .093-.o93 .093 ,o95--t095--.o96-.097 .099-.101 .100-.101  ,10<»


   ,07o .07« ,j62  .Cd4  .084 .Obf ,025 .Oo6 ,u87  .088  .089 .090 .091 .092  .093 .093 .094 .095  .095  .096 .099 .101 .102  .102  .105
                                                            .089-.fl9l-,09g  ,053 ,093 .o9* ,0°5 -.096 -.097 -.099 ,lol ,102  .lnV.107
                                                                 86

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.709	  L.A.-wlliCFIELa-«NAi.9 .079 .^90 .099-.107  .114  .121  .127  .133 .138. .142 .149 .000 -.000  .180 .177 .174 .171 .167



      .031'  .043  .051  .flSn  .Ot>5 .0"'3 .Dili -u" -lO9 .117  .121  .13o  .137  .113 .It7 ,1M .156 .162 .000  .1«0 .177 .171 .171 .168
 -034 .041  ,049  .056  .062  . OoO .OCQ. .CiO -.112 -121 .123 .134  .140  .145-.l5Q .154 .157-.160 .164 .176  .178 .176 .174 ,l7l .168


 .U39 .047  .i)b4  .062  . 0<><>  -074 .000 .CvO -000 .1^4 .139 .144  .148  .152  .155 .159 ,1M .164 .167 .175  .176 .175 .173 .171 .169
.•.0'tt-.052  .jfco  -06B  .07!>  .000  .000 .Ojfl .139-. 143 .147 .150  .153  .156 -.159 .162 .16M ,166 .168 .173 _. 175-. 174 .173 .171 .169


 .(,49 .05U  .j67  .076  ,(,Kt,  .OSO  .1^? .1J7 .144 .148 .]5l .153  .156  .159  .161 .164 ,lftf, .167 .169 .172  .174  .173 .173 .17] .169
      .flu1* 4U74  .064  .o9i,  .Ii3-.li8  .140 .l46~.15r, .J53 .156.. 158-. 161 - .163 .165 .166 .168..170 .171  .172.,173 .173 .172 .170



      .069 tu6o  .091  .103  .117  .131  .m2 .148 .151 .154 .157 .!&o  .162  .164 .165 .1*7 .168  .l^o .171  .172  .173 .173 .17? ,17o
      .fl7t) .0Bi  .0*7  ,10'J  .]<;!  .134  ,n,l» .149 .152 .ibb .150 .]6o  .163  .164  .166 .167 .168 .170 .171  .172  .J.73 .173 .172 .171


      .080 .j9l  .102  -114  .1*5  .137  .1,6 .l5fl .153 .156 .159 .]6l  .163  .165  .166 .]67 .168 .170 .171  .172  .173 .173 .172 .171
 -y7-» .035 .y^o  .Iy7  .lia  .1^9- .140  .infl .l52-.lb4 .157 .159  ,1&1  .163 ~. 164  . ]66 ,)67 .169 .170 .171  .172-,173 .173 .172 .171


 .079 .090 .101  .112  .123  .U3  .143  ,ln9 .152 .155 .157 .159  .]6l  .163  .164  .166 .167 .169 .170 .171  .172  .173 .175 .173 .172
 ,j8, .09% .XC& .117  .127  .107  .145  .IbO  .153 .155 .157 .159 .160  .162  .164-.166 .167 .169 .170 .170  .172  .173  .17.1 .173 .172



 .089 .ICO .ill .122  .132  .1'tO  .l'»6  ,]:>u  .152 .15* .156 .158 .159  .161  .163  .166 .1*7 .168 .169 .170  .171  .173  .173 .173 .173
 ,(j<3-j .106 .^17  .1^7  .iis  .!,]  .i;t-.l,y  .^52 ,JS4 . ] bS .157 .159-. 16o  .163  .166 . ] 67 .1^8 .lf-9 .170  .171  ,172  .173 .173 .173



 .100 -111 .j.22  .1JO  .137  .14?  , 1-.5  .1,6  .151 .lj' ,1?H .156 .158  .159  .163  .165 ,]fi6 .168 ,lf,9 .170  .171  .172  .173 ,17J ,]73


 .lOj .Ho .l^o  .1^^  ,ii7  ,1-tl  .l«tfc  ,1^7  .149 .Ibl .l')3 .154 .156  .159  .162  .164 , 1*Sb .167 ,lf.« .169  .171  .172  .173 .171) .171,


 .Ho .liJ •i2'i  -1.53  ..3''  . Inr  .1^3  ,1'tb  -147 .149 ,]5i .]53 ,5S5  .150  .161  .162 .]64 .166 .167 .169  .170  .172  .173 . 174 .174


 • lie, .1*3 ,1?'J  .1J3  .j.it,  .JJQ  .1-,]  .]-.-,  .146 .14"? .ibj ^152 .154  ,ir.7  .159  .161 .163 ,165 .166 .168  .17Q  .171  .173 .174 ,)74


 .4.2i .1^>- -i30  .li;.  .Tib  .1.17  .140  .1..K  .J44 ,J46 .14U .150 .152  .155  .lf,7  .159 .1^1 .163 .165 .J66  .169  ,l7Q  .172 .173 .175


 .12V , 1^>I . i30  .10-  . i.'4  . ljf>  ,l.'.r.  ,!,fi  .j42 .m'* .140 .!49 . 1 5l  .1'->J  . 3 i>5  .157 .1 S'l .161 .lf.3 .1^5  .167  .169  .171  .l7j ,)7;,
                                                                87

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                                                                                           AUA1.70.-PAGE	31—23JMR
            OF      Vt     Xi     Y) IN UNITS 1.0000+01
                                       3i»6-.3U7-_>349 -.351  .351-, J57 -.362^366 -.304^,000—.000 -000  .000—27S-.35I1 -.321 -291--262
  _    	                _  ^    ____.-        _J        __       __             __     '_  _
  — 39J .370 ..J63 .3f>l .363 .3o7 .371 .373 .372 .3t>6 .359  .350 .339 .321 .279 .121 .000  .000 .000  .000 .217  .071 .095 .101 .110
  -.370^.371-.J68 ,I09 -;7 -.296 — 246-- 180 -009-.000 -OOO-.OOO-.148-.o96-.072-.043-.029


   .372 .371 .J69 .371 .374 .390 .127 ,4bO .440 .4()9  .376  .348  .321 .290 .215 .174 .007 .000  .000  .OCO-.040-.149-. 1 So-. 126-.130
            ,~.-}66—36Z—,573 .399—«&3_5u7-.500—«32-3flo ~315—3-19—297-_262-.229 -217.-356 _000 .000-^085^. 119-.170-.J63-.18fl


        .372 ,J66 .357 .349 .3^B .<*98 .BoO .b79  .132  .367  .33t  .313 .308 ,2U3 .213 .201 .281  .359 .000-.o92-.12M-.16o-.1&7-.IflS


                                            624—350 -32b_311- .279-^260 —155—lB9_,i7l» _. 158^305- .3H1-.016--093--13S-- 150-.17Q
   -397 .392 .378 .3tB .;9b .255 ,000 .OoO .QOO  «193  .263  .233  .177 .179 .It3 .189 .116 .118  .2*6  .2'55-.o?t-.07o-.Ot»<'-. I2t-. 155
                        309 ,000 .OOt-.CjO-.E31-.lfl3  .17!  .151— .13fr- .15g ..lie .430 .091 ^.099 ,lt7  ,235_.ol7-.057-.0'»lt_.108-. 13&


   .tSo .454 .450 ."t33 .329 .000 -731 .tb2 ,31*7  .167  .137  .126  .117 .139 .11U .0^7 .flSS -086 -091  .207-.0l7-.0m-.038-.o"8-.llilo_.b47_a5o-.55i*—&57-,5b3--520--2^'*~.l;'*5-.12l(_ji7 -.1JO — 100--087-—o74 —058 —o72-.o59-.p51 —OS3-.o56_.013-.017-.Otl-.067
        .5tS .5"m .5^3 .b38 .528 .tfl6 .213 .138  .112  .102  .096  .Q9o .085 .oao .072 -077 .o5"»  .C»8  .052  .fl57 .02H-.006-.o32-.058


            -.t>»0- .533-.S2fr-.463-.293--.104-, 121-^ 1<)2- -.e^o -^086-. |>83--. 082--.O'1* -.095-»o70—o53-.OtS--.0»7-.06&--028 —003--023-. 049
   ,b4t> .b4H ,b38 .522 .486 .335 .232 .162 .117  .09U  .p8o  .078  .081 .078 .125 .126 .flSBioSO  .0*7  .018  .068 .039 .012-.011-.OUO


   .t^->-.i>51 -.&43- .479-.J60-.a*e-^.l4i»-.144-Tioa-.OB8  .072 -.081-. 078- . 107-.159-.o95-.o53-.o51  .0^9 -. 0«9  ,o««t .0«» - .019-.006-.031


   ,b64 .b60 .505 .365 .<;7:> .212 .168 .131 .100  .04>6  .072  .102  .071 .126 .127 .074 .0&6 .057  .053  .053  .110 .0*6 .025 .012-.022


   .011-.54& ,397 .230-.215-.177- .1<>8 .121 ,»94  .OS9-.001  .105-.085-.203 .108 .071 .088 .062 -.058- .059  .119 -,018 .031 .011-.Oil


   .bO<* .444 .J13 .213 .172 .151 .133 .116 .fl99  .095  .088  .099  .105 .224 .099 .073 .124 .061  .063  .061  .161 .050 .040 ,0?4 .004


   .jflo .347 .^32 .158-.147 .Ii4-.l24 .113 ,103  ,lc2  .c92^.093-. 117- . 155 . lll-.O™-. 110 -.077-.065 -.071  ,166 .060 .055 ,0«2 .024


   .24a .232 .145 .1^3 .,.24 .118 .112 .111 .106  .Ic8  .r94  .097  .123 .126 .112 .088 . o°6 .101  .P'4  .082  .100 .080 .076 .0^8 .053
	.i2?  .077  .085 .C9B- .10c .Iu2-.lt)3 .lut> ,1-Ofr .lcA  .107  .lo*  .105 .097 .101-. IC'6-. 101  .Ie3—1{)6-. 107 ~.09O~.1CO . 100 .099-.095-
                                                                 88

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             -. L.A.-nlUUrTCI a -AUALYSli		  - --  -   -  -ANAL70-PAGE  —32—23-KAR 73-


 6R10PR1NT  OF      U(      X.      Y) IN wIlTS  l.OOJO-lOZ
       —02A -.fe2!>- .0.1D--J2V.—OtO —031—.033 — S36 ~,<)3S-_ 039--.039 — 03B_.03 ,c^i> .u^1*  .0^3 ..<)2«_0il-. 0*2 -,0".7-.0*7- .017 .<.«&  .O'i7-,nlt9 ,052 .Q5G..03& -. COO —000 ^C01-.00'*-.00';_.0n3  .001


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 --.,,23 -.Oil -.(,3i . C,J9--. uHc— 015— Oi5 -.C13 —<,!»-. OO9  -C-09 -.010 -• 009 -.007--006 -OO1*-—0"3-.002 -.002-. 00"*-. 006--001r.OOO .001- .002


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  .U2i-.027  ,02r) -u27-.o2S-.OiO  .Ci"1  -.OjJ -uC't .OtA  .801 .003-.003~.002  .002 -.001 ,o"0-.001—OOO-.OOO  .002- -001-~nOO .001 -.002


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  -.o£7 .013  .00-»-.0'j3-. OOh-.3-j7-.fiOS-.C jd-.-j09-.036-.o06-, 007-.o06-.007-. 009-. 008-.oOB-.006-.006-.OOt>-.on1— .091-. 00?-.001 .002


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                                                                   89

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                                       	_	_	==			:  -ANAL70  PAGE	33-23-MAR 73 1B;U9!37--






 toRIDHRiNT OF      T(     X.     Y) IN UNITS  1.0000+03
       .Oo* .^ .Ob*-.u6* -.OoU-.O"* «06*  .U&U-.06*  .(16*  .06*  .O61-.0ht-.o6* '0&* • 0&9 ,075  .078..032-.085-.089 .093 .097 .102






       .06* . u6» .ub* . C'6l .Cot .0&* *0o*  . 06*  .06*  .06*  .06*  . 06*  .06* '0»* .06* . Ofi9 >fl7*  .079  . QH3  .086 . OB9 .093 .097 .101
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-.4,64 ^ 06*—06* -.00* .u6i( .Ou5-.069  .Ot>9-.Q69  .071-072  .07*  .075 .077 .079 .flSO .083  .085  .089  .093 .Q95-.097 .099 .100 .102






  • fl6n .fl6* «U6* .Oo* .0&U .Oo5 .0<=7  .070  -u72  -07*  -o75  .076  .Q76 .Oflfl -O8! .0S2 .0s*  '0B7  .090  .096 ,Q99 .Q98 .101 .101 .102
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       .Out .06* .06* .06* .Oo* .0°6 «C7U .4,80  .081  -cB2  .082  .083 .O8* .065 .086 ,086  .090  .09? .095 .097 .099 .100 .10*  .106
       ,06* «06*--0-.oa9—085-.08*  -08*  .Q8S .086-.088 - .089 .o9o  .Q92-.09*  .096. .o98_ .100-.101 - .10*  .10*






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  ,i&4 .06t .06* .OLt .06* .Oo* .070  .075  .079  .083 .C85 .087 .083 .090 -092 .093  .095  .095 .096 .097 .Q98 .101 .105 .107  .109
       .06*- .06*-.Oo* .o6*_eoft -073  .077-»o80-«083 .o8fr .088-^089 .091—.Q92 - .09*-.o95-.o96--.o97- .097 -.098- ,lo*-.106  . 105  . 10B  -
       .Ob* .06* .Ol>6 .069 .072 .075  .079  .(j82  .085  .087  .089 .091 .092 .09* .096  .Q96. .098  .097 .098 .099 .102 .10*  .10*  .108
 -.fe6"»-.Ou*- ,u6*-.069-.G72 ,075—.0*6 .Oofc-.tffiS—-067  .089  .091  ,Q9i: .09* .095-.096 .096-.097 .097 .098. .099 .103-. 105 .10*  .108






  • U&-, .Out .1)68 .072 .u7b .078 .0 .080 .iititt .cBb .Oo5 .flof' -087 .Q69-.090  .c9fl  .091  .092 .09*-.o9* .09* .096-.096 .0«7 ,o<>8 ,100 .102 .101  .102  .105






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-  «t,(U .OS2 ,o82-.0tl3 .uu3-.C»*-tO'>3 .Ob7  ,067  .Ob«  .C>i9-.090 -09£ .092-.093 .09*  .f)9*  ,095 .096 ,0q8 .100 .102  .103  .10*  .108
                                                                 90

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 -709  -  - - --L,,ft,-«JwW ICI.B-ANAL^SIS	   		   	-— 	ANAL70PAGE  - .31—23-V»R 73 .18:50: 00






 OHJDr'RIf.T Of    fnl (      X.      Y)  IN UNITS 1.0000+03
 ...oO.i-010 . U17—C.;J-.,j3o—036 -{M3--.CJO—.OS6 _ Ct.3 —c&9-.n76 ..032 -.089. .096 — 104 — 000  .OCO-.COO .000-.132...140 _«146 -.152 -158






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                                       	.	-	-AMAL70-PAGE	37 _23-««R J3 1B:50!33-

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                                                                 95

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                                                                                                          -39_23 -MftR J73-18J50J57
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  GRIDMUNT OF      V(     X,     Y) IN UNITS 1.0000+01
  —43d—363—357—JS6^354--.363—3&l_.350--35&-352--.353-,:S56-.3t,o-.364-.369--.306-.oOO-.000—COO—000—281—362—332—301—273



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                                                                96

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                                                                                              ANAL70. PA.6E ---- HD -23 -MAR -73 1RJ50:57
  toKiOHRINT OF       U(      X>     Y)  IN  UNITS 1.0000+P2
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_7Hl	--UA. WJIUFICIO ANAUT5IS				ANAL70  PAGE-  -.-•»»_ 23 MAR 73 16:51:53  _
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                         \

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                                                                  101

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—Z1&	~4~A,-»U£FIEL0-ANAto*StS	•	JWAL70-P-A6E	15—23 MAR -73-l8j52t27  .






4RJOHRJNT OF      T(      Xi      Y)  IN UNITS 1.0000+03
	.U6l4 -,064—^4—064--0&4-~Oo4--0&4-.0<>4—.u64--.«64--.0&1-..06»-,O&1-.06U_,o64- ,064-»o6a-•074_.077_.081 _OB« -.087 _o9l _09l_099






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                                                                                                               089_092_.095 -.098






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                     * — ^61;-,Oc5-.0*>B-.«>&--.068-,069 —07o -.072-^073-.075—077 -,079 -,ofll -,OB3 -037  ,06 .071 -075 .076 .077 .078  .079 .080 .082 .081 .086 .088  .090  .092 .fl91 .097 .097 .101  .103






                                                                                o35-.oa7-,oa9 _091_,013—095_.097_098—,101—.101
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                                             76-.07a—fr8&—0*1  ,a3-.e85  .OSfr— 0^7 -,0«9- .091—092-,093— 091 -.095-. 1O1 -.103--, 102  .105
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  .1,64 .064 .06S .071  .C.74  .076 .0/9 .Obi .C35 .066 .C86  .080  ,o8U  .089 .090 .090 .091  .092  .093  .094 .096 .101 .102  .100  .101






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  •004 .070 «u74 .0/8  
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 _JZV9	J-_U,A.-.-J,twtF.IEU>-HMAUr.SI-S>	AIUL70 PAGE	16 -23-MAR 73 46:52!51  _





 faKlDr-RllJT OF    PHK     Xr     Y)  IN UNITS 1.0COO+C3





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                                                  ££,5-,210 -.211--217^220-.223 -.22&-.226^.2?8 -,2?9—.230 .232 — 236 -239-.211  .2"*2






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                                                                 103

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                              ANAWSi-S	.	—	—	ANAL70-PAGE	U7	23-MAR-73-16:52:52	


 >6fUDrtUNT OF      V(     X.     Y) IN UNITS  1.0000+02                  •  .
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                                                                 104

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	7i,»	--L.A. ,,]NliFIELa^4ALTSIS		— ANAL70 .PAGE -_. 48 -23- MAR. 73 1B:52!53-.


  feFUCVKINT OF      U(     Xi     Y)  IN  UNITS  1.0000+02
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                                                                 105

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    218	-«-L.A. i.lhOfJEtO-ANALYSIS	—	AHAU70 PAGE.- -<»» *061 .0&1 .06"* .l,64-,o -061* . 0&1 .061 »0fi7  .071  .079  .031  .082-.085 .087 .090.,093


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 	.4,6-4 .061-.o61--.Oo1-.o6l-.Coil-.Oo1—C61..061-.061-.0&1 —061-.064 .061 .061 .067 .o71-.071 -.079 _,082 .083 .086 .088 .090 .093 _ .


    • u6t .06H .061 .061 .O6t .061 .061  .Ool  ,o61  .061  .cf'1  .061  .1361 .066 .067 .070 .073  .076  ,079  .083 ,Q81 .086 .088 .091 .093
	,4,61* .061 .(j61-.0o1-.ob1-.061 ..Gt]5-.0o5_t  .061  .1 .064— .Cfe1-»o&8 .Oo7-.o67-.0o8  '069 ^071  .072 .073 .fl75 .076 .fl78 .080-. 083  .087- . 088- .089 .0^1 .092 .091


    •U6-» -061 >o61 .Obi .061 .065 .O66 >0b?  .O69  "070  -c71  .072  .071 .075 .076 .078 .o"0 «P82  .081  .089  .fl91  ,Q9l .093 .093 .091
                                                    72-.o73-.071 -.075 .076 .Q77-.079 - .flBl -.<)83 ..065  . 057. .fl89- .092 .093'. 0?1 .097 .


    • U61 .061 .Q61 .Uol >o6it .061 .0&5  .069 .g73  .071  .fl71  .075  .Q76 .077 .078 .080 «082 .081  .086  .088  .Q9o .092 .092 .096 .098


    »<»64 .061 .061 :-061- .064-.O61 .0°ll-.07S-,o77  ,075- .075  .076  ,{t77 .078 .079-. .080 -,0fi3 -.085 -.086 -.088  .091- .092 -.093 .097 . 096 ._
    • u(>t .061 .0&1 .uol .36u .Obi .Q°1  .070  .p71  .075  -076  .077  .078 .079 .fl8o .0"0 .083  .085  .087  .088 .Q9o .091 .093 «fl9l .099
         .061 .(,61 .Ool .O6n-.0o4-.0o6-.070 .073-.075-.076  »077-.o7B .080 .0^1 .082 - .081-.OS6  ,087-.089 .fl90-.091 .&95 .098 .100
    • U&1* .061 .061 >0o1 .Q61 .Col .Ob8 .071 .o73  .075  .C77  .078  ,fl79 .080 .082 .083 .085  .086  .088  ,089  ,o9fl .093 .097 ,099 ,101
         .061 ..«61^ .061 .064-.9e7- .ot.9 ^072-.Q71  .076-.()78-r079 .0^0- .081- .083 .OS1-»0B&-«088_.o88-.089-.09O-.096-.098 .097 .100
    • 064 .061 .061 .065 .067 .Ou9 ,oV2 .074 -o76  .078  .079  .080  .C8l  .082 .085 .087 .flST  .090  .089  .089  .Q9o .091 .096 .096 ,ln6


	.1,64-,061 .061 ,0o7 .069-^071 .071 .07o-,o7»  .079-io8u-.081 -.082  .083 -.085-.086-.087-.088.,089  ,089  ,.091- .095 .097-.096 .100


    .064 .061 .067 .069 .071 .073 '.076 .076 .08!  .Obi  .081  .082  .082  .081 .035 .005 .087  .088  .088  .089  .091 .097 .097 .095 .099


	.1,64 .066 ,U69 .071 .073-.07B .077 .030-.085  .OfaJ-.082  .C82  .083  .085-.085 .085 .087-.087-,088  .089'.091 .013 -.096 .095 .099


    ,0b4 .066 ,071 .071 .J75 .076 .078 .060 . QB2  .Oo2  .082  .082  .083  .085 .085 .085 .087  .087  .088  .089  ,092 ,093 .095 .091 .097
—  .Il6o .070 .073 .078 .076-.077 .0/8 .079 ,081  .061  .ft8l-.062  .083 ,085 .085 .085 .087-.088-.088 -.089 .o'l .091 .093 . Q9i» .097


    .u7o .072 .074 .075 ,o76 .076 .077 .C76 .079  .080  .001  .C82  .06,5 .081 .085 .085 .Ofl6  ,0".7  .088  ,089 ,Q92 ,09i» .095 .095 .098
         .073 .i>73 .074 ,U75 .075 .0"/7 ,078 ,Q79  . Oi30 -*060--tBl  .083 .081 .065 .086 .086-.087  ,088  .089 .Q9? ,093 .095 .096 .100
                                                               106

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    7-1.9
             OF    PHI!      X.      Y) IN UMTS  1.0000+03
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         ,013 .019  .025  .0^1  .036 .Oil .050  .056  .063 .069 .075 .p£l .066  .091 .095 .000 .000 .000  .000 .000-. 138 .139 .1*0 .111
	.OH -.017 -.U23-.C29 -.035 - Oil—-OiB— Ob*.— t|6l -06a-,r7<* -C80-.oe&-.091 — OSS -p98 -.100 — 000 — 000 -.000- .000—116 .111 -1<42—111
    .1,1" .022 .027  .053  .f.3^  .045 .0^2 .Os9 -C66  .073 ,p8o .OP6 .091 .096  .100 .103 .000 -000  .000  .000 .000 .119 .116 .!«<(  .1M1
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      2i> .630 -035  .011  .1/16  .C^O -0^6 .Ct,7 .fl70  .086 .r,92 .p99 .lob .110  .115 .118 .122 ,1?6 .000  .000 .152 .150 .111  .1«5  .111
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                                                                     l-.133—135-, 136-^ 137_-,1J8. , 110-. 11-1-^HP-^OOO -000 -.000^000






         .OL5 .066 .C71 .(,S3  .0^1  .101  . U1 .120 .121*  -127  .130 .132 .13« .136  .137 .13E .139 .110  .111  .1H  .113 .111 .000 .000
          06i .o71-^C'79-.08,l- ,0^7—.Ij7_116-,1-2l-,125 ^.)28  . 131—133 .135 — 137-.138 - ] 39-. 139_ Hi J_ 111_ooO -000 -POO -OHO -.000






         >06B .07t> .Ofat .jS .'in .liV  .121  .1^6 .1^1 ,l?o  .1?B  .000  .131-.132 .131  .J.V.  .137-. H9 ,i«l .000-.000  -Ono ,000 ,11B
                                                               107

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     iETS=13
-6R1DPRINT OF      V(     Xt     Y) -IN UNITS -1.0000+01
  .320 .310 .J03 .3fl2 .30t -3o8 ..313 .316 .315 ,3il .305 .297 .286 .267 .227 .0'5 .000 -.000 .000 -000 .000  .056 .047 .0*3 .0"*9
. -.i89 .233 .287 .£68 .295 .3j.t .3*5 ,3o9 .362 ^3"»0 .319 .297 .265 .224 .167 .063  .000-.000  .000  .000  .000-.114-.152-.l35-. 143




                                 365— 4Ji3_40tt^.352—323—311-. 267-. 228_J.9o~. 160— 363— 000—. OOa—OOO—^OM--. 105^159^.158-. 179
  .270 .268 .^62 .E53 .243 .EH?. .311 ,7l3 .144 ,327 .320 -368 .259 .231 .203 .180 .1«2  .192  .000 .000-.051-.o96-.144-.l5l-.171




                                                                                         110—.0
       .267 .^52 .223 .177 .119 .000 ..000 -000 .086 .297 .140 .117 .146 .125 .190  .Q85  .flB2 .200  .000-.0?0-.056-.B6'(-.o79-.o97
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  .312 .310 .302 .378 .161 .060 .000 «*72 .223 .197 .162 .129 . 15Q .134 .Q96 .074  .060  .059  -o65  .000-.0*6-.o30 -000-.on4-.o51
  .i4fl-.343-.35o -.375^487 .7^6-,621— 374—239-. 164— 456— 145— . 136-.1Q1— .pfl2  .Qftl  .Q45  .Q63  .Qfi7^.oa4-^.
 .366 .370  .385 .419  ,49i  .5o3 .525 .390 .217 ,lt,3 .162 .131 .111 .091 .074 .tlSl .040  .055  .041  .009 .016  .178 .003 .000 .000
                                                        -. 124_105— .087— .068-^O4~.e92-^SO-.<)69—.050-.959_^1—.019-.023-^831-.O25— 000 — 000-.051
  .394 .395 .397 .399 ,4oo .397 .373 .235 .153 .119 .101 .091 .085 .oBl .077  .063  ,fl6l  .021  .009 .Oil .012 .000 .000 .fl4o-.0l4




                -.392-.-39a—.379-,2a9—. Wl—^33-.103-^87—060^^78-,878-.o94-.091-.fl49—.017—,^04'».003-^003—.000—000--ono— 023
  .380  .387  .388 .385 .382 .310 .223 .Ib9 .114 .089 .072 .070 .076 .073 .141 .131  .028- .OCB-.001-.010-.004 .000 .000 .000 .058




 -.a8i_.333-,3fi4 .37fr-.328-.2j6-.181-.145-.697—.076 -.058-.072 -.067-. MS-.190 .078 -.0-15-,005-.0«3~.OW-^003-.«00-.OOn .000 .066
  .37-4  .370 .301  .123 ,i:47 .192 .Ii3 .117 .082 .069 .054 .102 .053 .116 .122  .040  .026  .011-.00l-.011 .016 .000 .000 .000 .070




— .357  .3b5 .J46  .i45 .188 .l!>6 .131-.-1U4 .071 .073-.O65 .106 .076-, 269 ^86  ,032 -.051-.015-.O04-.OOi- .031 -.000 -.000 .000 .000




  .k93  .339 .277  .162 .146 .129 .114 .096 .078 .078 .072 .095 .llfl .000 .0?!  .031  .093  .015  .010-. 002 .000 .000 .000 .000 .000
  .1,56  .339 .208 .13O-.122 ~.ii2--.103- .093 2 . 0=*3-,0dl>- «T)H5-.OS6 -, fB7 .CB9 -«10e .071 .i»79 .086  .0"0-«081 -,p87—,035-^DOO .000 -.500 -.000 .076









                             '            '•'•'.          •'      '        .'    "    '        *        (
                                                             108

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   	7l»<4  	- L.A.-»lMJI=-IElO-ANAl.riIS		ANAL70 £AGE   -52 -23 MAR 73 Ifl:53:i5
        bE.TS=13
    GH10PKINT OF      Ut      Xi      Yl  IM UNITS 1.0000401
 __  .I9o ,ia7-.i95 .195  .195-.1*9-.21,8..2i2-.£37 .219- .256-. 253  .236- .196 ..091-.127 .000 .000 .000-.000  .67 .213 .202 .140 .173  .170  .178  .212 .253 .278 .29fl .299  .702  .301  .30* .333 .000 .000 .000  .000  .000  .107 .OBfl .051 .008
	.Z2j--.21lt-.l03 -187 .165  .137  .125  .2oO .231 .3fl7-.310 .328-. 311 -.311  -361  .107 .379 .000 . OOO-.OOO  .069 .. 016 .026 .0?5 .017



     .t2t .217 ,^C7 .191 .161  .CvP-.o"  -1^1 -387 .353 .306 .371  .?9fl  .371  .379  .359 .321 .239 .000  .000-.015-.010-.017 .001 ,0?1
     .^2i .222-.<119 ,2j3-.i83  .149- .000-.8«0 -.59*- ,331—190 .000 .132 -»319--.27o -.271 .?53 .207 ..000- .000-.093-.o78-.016-.on8 .029



     .*2u .229 ,237 .259 ,230  .2J7  .000  -OuO -uOU .651 .151 .226 .?69  .237  .231 .?33 .173 .113 .1Q9  . 000-.1?0~.105-.071-.017 .031
 	,6l -.OoS .051 .018 ,013-.038-.032  .027 ,o?2- .0^*- -033- .035 -.000  .000  .000 .000 .000



     .«:2i .225 .^27 .223 .^Q8  -lei  .I*16  .121  .101 .071 ,c52 .039 ,o3o  .026  .021  .027 .035 .018 .023 .0?6  .001-.012  .000 .000 .000
          .221 .219 .Jii .ioi  .Io3  .lol  .115 .070 -057 ,011 .027 .017 -.013-.01& .022 .QlO-.0?l -010 .001-.019-.023  .000 .000 .017



          .219 .215 .2p9 .I99  ,C32  . t,Oo-,C jf -. C22-.C31-. 031-.031  .018  .069  .0?9 .008 .002-.001-. 005  .000  .000  .000 .016
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                                                               109

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      18	»-L.A.-«UiD«EUO^NAi.*SIS	—	'.	—--	.	—	ANAL70-PAGE	S3_2J-HAR-73 18154:12-
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    GR1DHRINT OF      T<      Xi     Y) IN UNITS 1.0000+02
      bdtf .640-^o4a .640 .04&-.640-.640--.640—.640- .640—^4e-.640—.640-.&4*  .640  .640-.655-.674-_.669-_.672 .665- .663..665 .668-.6BO -
     .64o .640 .040 .6tO -6'»0 .640 .640 .640 .640 .*40 .640 .640 .639  .641  .644  .650  .658  .666 .658 .660 .66] .665 .670



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     .till  .640  .640  .640  .b4o .£40 .657 .636 .641 .638 .638 .635 .630 <636  .641  .647  .643 .644 .655 .667 .655 .658 .660 .666 .672


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                                                              110

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                                                                                                ANALIO PAGE	5U—-23 MAR-JZi_18J5«30
    GfUDHRINT OF    PHK     X.      Y)  IN UNITS 1.0000+02
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                                                                111

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                                                                      113

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                                   TECHNICAL REPORT DATA
                            (Please read Instructions on the reverse before completing)
1. REPORT NO.
  EPA-650/4-73-001
                             2.
                                                           3. RECIPIENT'S ACCESSION-NO.
4. TITLE AND SUBTITLE
  A  Mesoscale Windfield Analysis  of The Los Angeles
  Basin
                                            5. REPORT DATE
                                                 June 1973
                                            6. PERFORMING ORGANIZATION CODE
7. AUTHOR(S)


  G.  E.  Anderson
                                                           8. PERFORMING ORGANIZATION REPORT NO.
                                                 CEM 4121-01-490C
9. PERFORMING ORGANIZATION NAME AND ADDRESS
  The  Center for the Environment  & Man, Inc.
  275  Windsor Street
  Hartford, Connecticut  06120
                                             10. PROGRAM ELEMENT NO.

                                                 1A1009
                                             11. CONTRACT/GRANT NO.
12. SPONSORING AGENCY NAME AND ADDRESS
                                                           13. TYPE OF REPORT AND PERIOD COVERED
  Environmental  Protection Agency
  National  Environmental Research Center
  Meteorology Laboratory
  Research  Triangle Park, North  Carolina  27711
                                             14. SPONSORING AGENCY CODE
15. SUPPLEMENTARY NOTES
16. ABSTRACT
       The  rationale, derivation,  and use of a mesoscale  windfield analysis  is
  presented.   In the program  reported on herein, the  analysis was applied  to a
  specific  region - the Los Angeles  Basin.  This application is in support of
  a multi-phased effort of modelling ground level and/or  three dimenstnal  air
  pollution distributions in  the  region.  Los Angeles  air pollution modelling
  efforts supported by the Environmental Protection Agency are using data
  collected during an experimental  program carried out during the fall of  1969.
  The mesoscale windfield analysis  described here was  specifically applied to
  13 hourly periods from 5:00 am  to 5:00 pm on 29 September 1969, and one
  period at 6:00 am on 30 September 1969.
17.
                                KEY WORDS AND DOCUMENT ANALYSIS
                  DESCRIPTORS
                               b.lDENTIFIERS/OPEN ENDED TERMS  C.  COS AT I Field/Group
  Thesaurus  Descriptors
  99 Meteorology and Climatology
  ATmospheric Motion
  Sea Breeze
  Temperature
  Wind
      144  Sanitary Engineering
      Atmospheric Pol 1ution
Atmosphere Models	
Los Angeles  Windfield
  Analysis
Topographic  Effects
Divergence Analysis
                                                           04 (Atmos. Sci)/
                                                           01  (Atmos. Pfosics
             STATEMENT
                                              19. SECURITY CLASS {ThisReport)
                                                 Unclassified
                                                          21. NO. OF PAGES
                                                              120
  Unlimited
                               20. SECURITY CLASS (Thispage)

                                   Unclassified
                                                                         22. PRICE
EPA Form 2220-1 (9-73)
                                             114

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