********************************************************
RODI.DAT

SHARP-FIN-GENERATED SHOCK WAVE/TURBULENT BOUNDARY
LAYER INTERACTION DATA AT MACH 4.9, INCLUDING
HEAT TRANSFER MEASUREMENTS
********************************************************

                       NOMENCLATURE

ALPHA = fin angle of attack, degrees
BETA = conical angle in plane of test surface, degrees
BETAO = angle of inviscid shock trace, degrees
BETAU = upstream influence angle, degrees
BETAS1 = primary separation angle, degrees
BEVCO = beta angle from VCO, degrees
BEFLE = beta angle from fin leading edge, degrees
BLM = calculated local Mach number within boundary layer
BLP = assumed static pressure within boundary layer, psia
BLP0 = measured total pressure within boundary layer, psia
BLT0 = assumed total temperature within boundary layer, F
CH = Stanton number
CHE = Stanton number at interaction edge
DELTA = incoming boundary layer thickness, 0.25 in.
DELY = local spanwise distance from fin to tap/transducer, inches
LI = length of leading edge inception region, inches
P = static wall pressure, psia
PE = pressure at interaction edge, psia
PO = tunnel total pressure, psia
QDOT = wall heat transfer, BTU/ft^2/sec
R = radial distance from VCO, inches
THETA = plug rotation angle, degree
TO = tunnel total temperature, degrees F
TW = wall temperature, degrees F
VCO= virtual conical origin
VCOp= VCO based upon the wall pressure distribution
VCOv= VCO based upon the surface tracer patterns
X = streamwise distance, inches
XLE = streamwise distance from fin leading edge, inches
Y = spanwise distance, inches
YS = local spanwise distance from fin to inviscid shock, inches
YYS = spanwise distance from fin normalized by the YS
YLE = spanwise distance from fin leading edge, inches
Z = vertical distance above plate, inches

***************************************************************************
                  INCOMING BOUNDARY LAYER DOCUMENTATION
***************************************************************************

The incoming turbulent boundary layer Pitot profile was measured 19.3 in.
(49.0 cm.) downstream of the flat plate leading edge and approximately
0.5 in. (1.27 cm.) upstream of the fin leading edge.  Height above the wall
(Z) and Pitot pressure (BLPO) were measured directly, the local static
pressure distribution (BLP) was assumed to be linear as was the local
total temperature distribution (BLTO).  Local Mach number (BLM) was
calculated.

   INDEX       Z              BLP            BLP0     BLM     BLT0
             (in)            (psia)         (psia)             (F)
     1    0.57008E-01         0.752         7.300     2.68   260.15
     2    0.59449E-01         0.751         7.340     2.69   260.51
     3    0.63031E-01         0.750         7.816     2.78   261.05
     4    0.66614E-01         0.748         8.160     2.84   261.77
     5    0.69449E-01         0.748         8.507     2.91   262.31
     6    0.72008E-01         0.747         8.689     2.94   262.67
     7    0.75866E-01         0.745         8.959     2.99   263.39
     8    0.82834E-01         0.743         9.082     3.02   264.65
     9    0.86260E-01         0.742         9.452     3.08   265.37
    10    0.89291E-01         0.741         9.873     3.16   265.91
    11    0.96575E-01         0.739        10.556     3.27   267.17
    12    0.10024E+00         0.738        10.920     3.33   267.71
    13    0.10571E+00         0.736        10.990     3.35   268.79
    14    0.10866E+00         0.735        11.413     3.42   269.33
    15    0.11327E+00         0.733        11.853     3.49   270.05
    16    0.11949E+00         0.731        12.788     3.63   271.13
    17    0.12524E+00         0.729        13.017     3.67   272.21
    18    0.13209E+00         0.727        13.538     3.75   273.47
    19    0.13776E+00         0.725        13.819     3.80   274.55
    20    0.14559E+00         0.723        15.084     3.98   275.81
    21    0.15303E+00         0.721        15.722     4.07   277.25
    22    0.15929E+00         0.718        15.911     4.10   278.33
    23    0.16587E+00         0.716        16.796     4.22   279.41
    24    0.17480E+00         0.713        17.622     4.34   281.03
    25    0.18327E+00         0.711        18.086     4.40   282.65
    26    0.19091E+00         0.708        18.507     4.46   283.91
    27    0.19795E+00         0.706        18.986     4.53   285.17
    28    0.20594E+00         0.703        19.479     4.60   286.61
    29    0.21563E+00         0.700        19.537     4.61   288.41
    30    0.22791E+00         0.696        20.320     4.72   290.57
    31    0.23752E+00         0.693        20.407     4.74   292.19
    32    0.24787E+00         0.690        20.581     4.77   294.17
    33    0.25882E+00         0.686        20.610     4.79   296.15
    34    0.26827E+00         0.683        20.668     4.81   297.77
    35    0.28004E+00         0.679        20.712     4.83   299.93
    36    0.30000E+00         0.673        20.726     4.85   303.35
    37    0.31067E+00         0.670        20.755     4.87   305.33

***********************************************************************
                        SURFACE PRESSURE DATA
***********************************************************************


Below are the spanwise pressure measurements for fin angles of
attack = 6-, 10-, 12- and 14-degrees.  The 8- and 16-degree spanwise
data are plotted in conical coordinates along with the conical cross-
plane data later.  PE is defined as the edge pressure value along
each spanwise row.


            ALPHA=   6.0                     BETAO=  16.1

        X         Y       DELY       YS      DELY/YS     P        P/PE
      (in.)     (in.)     (in.)     (in.)              (psia)
      2.009     1.852     1.640     0.369     4.450     0.777     1.000
      2.009     1.712     1.500     0.369     4.070     0.770     0.991
      2.009     1.572     1.360     0.369     3.690     0.761     0.979
      2.009     1.432     1.220     0.369     3.311     0.766     0.986
      2.009     1.292     1.080     0.369     2.931     0.765     0.985
      2.009     1.152     0.940     0.369     2.551     0.822     1.058
      2.009     1.012     0.800     0.369     2.171     0.907     1.167
      2.009     0.872     0.660     0.369     1.792     1.001     1.288
      2.009     0.732     0.520     0.369     1.412     1.032     1.328
      2.009     0.592     0.380     0.369     1.032     1.066     1.372
      2.009     0.452     0.240     0.369     0.652     1.142     1.470
      2.009     0.312     0.100     0.369     0.273     1.244     1.601
      2.378     1.852     1.602     0.436     3.670     0.755     1.000
      2.378     1.712     1.462     0.436     3.350     0.759     1.005
      2.378     1.572     1.322     0.436     3.029     0.761     1.008
      2.378     1.432     1.182     0.436     2.708     0.768     1.017
      2.378     1.292     1.042     0.436     2.387     0.827     1.095
      2.378     1.152     0.902     0.436     2.066     0.911     1.207
      2.378     1.012     0.762     0.436     1.745     0.976     1.293
      2.378     0.872     0.622     0.436     1.425     1.019     1.350
      2.378     0.732     0.482     0.436     1.104     1.051     1.392
      2.378     0.592     0.342     0.436     0.783     1.070     1.417
      2.378     0.452     0.202     0.436     0.462     1.178     1.560
      2.009     1.642     1.430     0.369     3.880     0.770     1.000
      2.009     1.502     1.290     0.369     3.501     0.764     0.992
      2.009     1.362     1.150     0.369     3.121     0.792     1.029
      2.009     1.222     1.010     0.369     2.741     0.792     1.029
      2.009     1.082     0.870     0.369     2.361     0.867     1.126
      2.009     0.802     0.590     0.369     1.602     1.034     1.343
      2.009     0.662     0.450     0.369     1.222     1.057     1.373
      2.009     0.522     0.310     0.369     0.842     1.110     1.442
      2.009     0.382     0.170     0.369     0.462     1.224     1.590
      2.009     0.242     0.030     0.369     0.083     1.298     1.686
      2.378     1.642     1.392     0.436     3.189     0.770     1.000
      2.378     1.502     1.252     0.436     2.868     0.764     0.992
      2.378     1.362     1.112     0.436     2.548     0.809     1.051
      2.378     1.222     0.972     0.436     2.227     0.881     1.144
      2.378     1.082     0.832     0.436     1.906     0.961     1.248
      2.378     0.942     0.692     0.436     1.585     1.011     1.313
      2.378     0.802     0.552     0.436     1.264     1.048     1.361
      2.378     0.662     0.412     0.436     0.943     1.056     1.371
      2.378     0.522     0.272     0.436     0.623     1.140     1.481
      2.378     0.382     0.132     0.436     0.302     1.274     1.655


            ALPHA=  10.0                     BETAO=  19.6

        X         Y       DELY       YS      DELY/YS     P        P/PE
      (in.)     (in.)     (in.)     (in.)              (psia)
      2.002     1.992     1.639     0.360     4.553     0.779     1.000
      2.002     1.852     1.499     0.360     4.164     0.758     0.973
      2.002     1.712     1.359     0.360     3.775     0.753     0.967
      2.002     1.992     1.639     0.360     4.553     0.779     1.000
      2.002     1.852     1.499     0.360     4.164     0.758     0.973
      2.002     1.712     1.359     0.360     3.775     0.753     0.967
      2.002     1.572     1.219     0.360     3.386     0.765     0.982
      2.002     1.432     1.079     0.360     2.997     0.844     1.083
      2.002     1.292     0.939     0.360     2.608     0.992     1.273
      2.002     1.152     0.799     0.360     2.219     1.104     1.417
      2.002     1.012     0.659     0.360     1.830     1.186     1.522
      2.002     0.872     0.519     0.360     1.441     1.184     1.520
      2.002     0.732     0.379     0.360     1.052     1.194     1.533
      2.002     0.592     0.239     0.360     0.663     1.409     1.809
      2.002     0.452     0.099     0.360     0.274     1.762     2.262
      2.371     1.992     1.574     0.426     3.692     0.757     1.000
      2.371     1.852     1.434     0.426     3.363     0.763     1.008
      2.371     1.712     1.294     0.426     3.035     0.757     1.000
      2.371     1.572     1.154     0.426     2.706     0.905     1.196
      2.371     1.432     1.014     0.426     2.378     1.037     1.370
      2.371     1.292     0.874     0.426     2.049     1.119     1.478
      2.371     1.152     0.734     0.426     1.721     1.177     1.555
      2.371     1.012     0.594     0.426     1.393     1.190     1.572
      2.371     0.872     0.454     0.426     1.064     1.182     1.561
      2.371     0.732     0.314     0.426     0.736     1.355     1.790
      2.371     0.592     0.174     0.426     0.407     1.683     2.223
      2.002     1.782     1.429     0.360     3.969     0.757     1.000
      2.002     1.642     1.289     0.360     3.580     0.755     0.997
      2.002     1.502     1.149     0.360     3.191     0.784     1.036
      2.002     1.362     1.009     0.360     2.802     0.900     1.189
      2.002     1.222     0.869     0.360     2.413     1.057     1.396
      2.002     0.942     0.589     0.360     1.635     1.200     1.585
      2.002     0.802     0.449     0.360     1.246     1.196     1.580
      2.002     0.662     0.309     0.360     0.857     1.284     1.696
      2.002     0.522     0.169     0.360     0.468     1.648     2.177
      2.002     0.382     0.029     0.360     0.079     1.899     2.509
      2.371     1.782     1.364     0.426     3.199     0.770     1.000
      2.371     1.642     1.224     0.426     2.871     0.831     1.079
      2.371     1.502     1.084     0.426     2.542     0.993     1.290
      2.371     1.362     0.944     0.426     2.214     1.096     1.423
      2.371     1.222     0.804     0.426     1.885     1.159     1.505
      2.371     1.082     0.664     0.426     1.557     1.197     1.555
      2.371     0.942     0.524     0.426     1.228     1.175     1.526
      2.371     0.802     0.384     0.426     0.900     1.222     1.587
      2.371     0.662     0.244     0.426     0.571     1.509     1.960
      2.371     0.522     0.104     0.426     0.243     1.948     2.530


            ALPHA=  12.0                     BETAO=  21.5

        X         Y       DELY       YS      DELY/YS     P        P/PE
      (in.)     (in.)     (in.)     (in.)              (psia)
      1.995     2.061     1.637     0.362     4.525     0.758     1.000
      1.995     1.921     1.497     0.362     4.138     0.747     0.985
      1.995     1.781     1.357     0.362     3.751     0.745     0.983
      1.995     1.641     1.217     0.362     3.364     0.768     1.013
      1.995     1.501     1.077     0.362     2.977     0.921     1.215
      1.995     1.361     0.937     0.362     2.590     1.095     1.445
      1.995     1.221     0.797     0.362     2.203     1.203     1.587
      1.995     1.081     0.657     0.362     1.817     1.220     1.609
      1.995     0.941     0.517     0.362     1.430     1.217     1.606
      1.995     0.801     0.377     0.362     1.043     1.243     1.640
      1.995     0.661     0.237     0.362     0.656     1.559     2.057
      1.995     0.521     0.097     0.362     0.269     2.114     2.789
      2.364     2.061     1.559     0.429     3.636     0.736     1.000
      2.364     1.921     1.419     0.429     3.309     0.755     1.026
      2.364     1.781     1.279     0.429     2.983     0.863     1.173
      2.364     1.641     1.139     0.429     2.656     1.040     1.413
      2.364     1.501     0.999     0.429     2.330     1.134     1.541
      2.364     1.361     0.859     0.429     2.003     1.211     1.645
      2.364     1.221     0.719     0.429     1.677     1.248     1.696
      2.364     1.081     0.579     0.429     1.350     1.202     1.633
      2.364     0.941     0.439     0.429     1.024     1.220     1.658
      2.364     0.801     0.299     0.429     0.697     1.503     2.042
      2.364     0.661     0.159     0.429     0.371     2.045     2.779
      1.995     1.851     1.427     0.362     3.944     0.764     1.000
      1.995     1.711     1.287     0.362     3.558     0.773     1.012
      1.995     1.571     1.147     0.362     3.171     0.842     1.102
      1.995     1.431     1.007     0.362     2.784     1.042     1.364
      1.995     1.291     0.867     0.362     2.397     1.172     1.534
      1.995     1.011     0.587     0.362     1.623     1.265     1.656
      1.995     0.871     0.447     0.362     1.236     1.218     1.594
      1.995     0.731     0.307     0.362     0.849     1.393     1.823
      1.995     0.591     0.167     0.362     0.462     1.923     2.517
      1.995     0.451     0.027     0.362     0.075     2.295     3.004
      2.364     1.851     1.349     0.429     3.146     0.823     1.000
      2.364     1.711     1.209     0.429     2.819     0.982     1.193
      2.364     1.571     1.069     0.429     2.493     1.130     1.373
      2.364     1.431     0.929     0.429     2.166     1.208     1.468
      2.364     1.291     0.789     0.429     1.840     1.254     1.524
      2.364     1.151     0.649     0.429     1.513     1.261     1.532
      2.364     1.011     0.509     0.429     1.187     1.234     1.499
      2.364     0.871     0.369     0.429     0.860     1.383     1.680
      2.364     0.731     0.229     0.429     0.534     1.793     2.179
      2.364     0.591     0.089     0.429     0.207     2.424     2.945


            ALPHA=  14.0                     BETAO=  23.5

        X         Y       DELY       YS      DELY/YS     P        P/PE
      (in.)     (in.)     (in.)     (in.)              (psia)
      1.986     2.131     1.636     0.368     4.441     0.779     1.000
      1.986     1.991     1.496     0.368     4.061     0.768     0.986
      1.986     1.851     1.356     0.368     3.681     0.777     0.997
      1.986     1.711     1.216     0.368     3.300     0.886     1.137
      1.986     1.571     1.076     0.368     2.920     1.118     1.435
      1.986     1.431     0.936     0.368     2.540     1.250     1.605
      1.986     1.291     0.796     0.368     2.160     1.334     1.712
      1.986     1.151     0.656     0.368     1.780     1.345     1.727
      1.986     1.011     0.516     0.368     1.400     1.267     1.626
      1.986     0.871     0.376     0.368     1.020     1.336     1.715
      1.986     0.731     0.236     0.368     0.640     1.779     2.284
      1.986     0.591     0.096     0.368     0.260     2.600     3.338
      2.355     2.131     1.544     0.437     3.534     0.767     1.000
      2.355     1.991     1.404     0.437     3.214     0.879     1.146
      2.355     1.851     1.264     0.437     2.893     1.095     1.428
      2.355     1.711     1.124     0.437     2.573     1.226     1.598
      2.355     1.571     0.984     0.437     2.252     1.299     1.694
      2.355     1.431     0.844     0.437     1.932     1.336     1.742
      2.355     1.291     0.704     0.437     1.611     1.324     1.726
      2.355     1.151     0.564     0.437     1.291     1.257     1.639
      2.355     1.011     0.424     0.437     0.970     1.351     1.761
      2.355     0.871     0.284     0.437     0.650     1.759     2.293
      2.355     0.731     0.144     0.437     0.329     2.593     3.381
      1.986     1.921     1.426     0.368     3.871     0.769     1.000
      1.986     1.781     1.286     0.368     3.490     0.825     1.073
      1.986     1.641     1.146     0.368     3.110     1.037     1.349
      1.986     1.501     1.006     0.368     2.730     1.212     1.576
      1.986     1.361     0.866     0.368     2.350     1.293     1.681
      1.986     1.081     0.586     0.368     1.590     1.315     1.710
      1.986     0.941     0.446     0.368     1.210     1.270     1.651
      1.986     0.801     0.306     0.368     0.830     1.511     1.965
      1.986     0.661     0.166     0.368     0.450     2.274     2.957
      1.986     0.521     0.026     0.368     0.070     2.753     3.580
      2.355     1.921     1.334     0.437     3.053     1.028     1.000
      2.355     1.781     1.194     0.437     2.733     1.190     1.158
      2.355     1.641     1.054     0.437     2.412     1.291     1.256
      2.355     1.501     0.914     0.437     2.092     1.337     1.301
      2.355     1.361     0.774     0.437     1.771     1.354     1.317
      2.355     1.221     0.634     0.437     1.451     1.277     1.242
      2.355     1.081     0.494     0.437     1.130     1.297     1.262
      2.355     0.941     0.354     0.437     0.810     1.550     1.508
      2.355     0.801     0.214     0.437     0.489     2.162     2.103
      2.355     0.661     0.074     0.437     0.169     2.958     2.877





Next are given the surface pressure data taken with and without the
plug rotated to better match the conical cross-planes.  PE is held fixed
for a given dataset.


Mean surface pressure data for tap rows with plug rotated 15-deg and
fin angle of attack of 8-deg.

  VCOp at X=  -0.891 in.,  Y=  -0.361 in.,   PE = 0.750 psia

         X         Y      BEVCO    BEFLE   DELY/YS      P        P/PE
       (in.)     (in.)    (deg)    (deg)             (psia)
       0.677     1.050    41.99    57.18     7.81     0.763     1.017
       0.713     0.915    38.50    52.05     6.32     0.775     1.033
       0.749     0.780    34.82    46.12     4.98     0.750     1.000
       0.786     0.645    30.96    39.35     3.76     0.796     1.061
       0.822     0.509    26.94    31.77     2.65     0.978     1.304
       0.858     0.374    22.80    23.54     1.64     1.092     1.456
       0.894     0.239    18.58    14.95     0.70     1.248     1.664
       1.533     1.859    42.49    50.49     5.94     0.754     1.005
       1.569     1.724    40.29    47.69     5.31     0.754     1.005
       1.605     1.589    38.00    44.70     4.70     0.749     0.999
       1.641     1.454    35.63    41.52     4.13     0.745     0.993
       1.678     1.319    33.18    38.15     3.57     0.747     0.996
       1.714     1.183    30.66    34.61     3.04     0.772     1.029
       1.750     1.048    28.08    30.91     2.54     0.910     1.213
       1.786     0.913    25.44    27.06     2.05     1.056     1.408
       1.823     0.778    22.76    23.10     1.58     1.094     1.459
       1.859     0.642    20.05    19.06     1.13     1.101     1.468
       1.889     1.955    39.79    45.97     4.95     0.757     1.009
       1.895     0.507    17.31    14.98     0.70     1.217     1.623
       1.925     1.820    37.75    43.37     4.46     0.749     0.999
       1.931     0.372    14.56    10.89     0.29     1.459     1.945
       1.962     1.684    35.64    40.64     3.98     0.752     1.003
       1.998     1.549    33.47    37.78     3.52     0.749     0.999
       2.034     1.414    31.25    34.80     3.07     0.747     0.996
       2.070     1.279    28.97    31.69     2.64     0.828     1.104
       2.107     1.144    26.65    28.49     2.23     0.939     1.252
       2.143     1.008    24.29    25.19     1.83     1.063     1.417
       2.179     0.873    21.90    21.83     1.44     1.106     1.475
       2.215     0.738    19.48    18.42     1.07     1.099     1.465
       2.252     0.603    17.05    14.98     0.70     1.211     1.615


Spanwise surface pressure data for tap rows with plug rotated 0-deg and
fin angle of attack of 8-deg.

  VCOp at X=  -0.891 in., Y=  -0.361 in.,  PE = 0.760 psia

         X         Y      BEVCO    BEFLE   DELY/YS      P        P/PE
       (in.)     (in.)    (deg)    (deg)             (psia)
       0.971     1.362    42.79    54.52     6.99     0.771     1.014
       0.971     1.222    40.38    51.53     6.19     0.763     1.004
       0.971     1.082    37.78    48.10     5.39     0.751     0.988
       0.971     0.942    34.99    44.13     4.60     0.748     0.984
       0.971     0.802    32.00    39.55     3.80     0.764     1.005
       0.971     0.662    28.79    34.28     3.00     0.870     1.145
       2.007     1.922    38.24    43.76     4.53     0.779     1.025
       2.007     1.782    36.49    41.60     4.14     0.767     1.009
       2.007     1.642    34.66    39.29     3.75     0.763     1.004
       2.007     1.502    32.74    36.81     3.37     0.766     1.008
       2.007     1.362    30.74    34.16     2.98     0.792     1.042
       2.007     1.222    28.65    31.33     2.59     0.888     1.168
       2.007     1.082    26.47    28.33     2.21     1.025     1.349
       2.007     0.942    24.21    25.14     1.82     1.101     1.449
       2.007     0.802    21.87    21.78     1.43     1.131     1.488
       2.007     0.662    19.44    18.25     1.05     1.139     1.499
       2.007     0.522    16.95    14.57     0.66     1.268     1.668
       2.007     0.382    14.38    10.77     0.28     1.494     1.966
       2.376     1.922    34.95    38.97     3.70     0.755     0.993
       2.376     1.782    33.27    36.87     3.38     0.759     0.999
       2.376     1.642    31.52    34.65     3.05     0.764     1.005
       2.376     1.502    29.70    32.30     2.72     0.774     1.018
       2.376     1.362    27.81    29.82     2.40     0.927     1.220
       2.376     1.222    25.85    27.21     2.07     1.021     1.343
       2.376     1.082    23.83    24.48     1.74     1.076     1.416
       2.376     0.942    21.75    21.62     1.42     1.122     1.476
       2.376     0.802    19.60    18.65     1.09     1.132     1.489
       2.376     0.662    17.39    15.56     0.76     1.212     1.595
       2.376     0.522    15.12    12.39     0.44     1.405     1.849



Spanwise surface pressure data for tap rows with plug rotated 0-deg and
fin angle of attack of 8-deg.

  VCOp at X=  -0.891 in.,  Y=  -0.361 in., PE = 0.770 psia

         X         Y      BEVCO    BEFLE   DELY/YS      P        P/PE
       (in.)     (in.)    (deg)    (deg)             (psia)
       0.971     1.292    41.61    53.08     6.59     0.777     1.009
       0.971     1.152    39.10    49.88     5.79     0.741     0.962
       0.971     1.012    36.41    46.19     5.00     0.736     0.956
       0.971     0.872    33.52    41.93     4.20     0.747     0.970
       0.971     0.732    30.42    37.01     3.40     0.798     1.036
       0.971     0.592    27.11    31.37     2.60     0.941     1.222
       0.971     0.452    23.59    24.95     1.80     1.062     1.379
       0.971     0.312    19.87    17.80     1.00     1.150     1.494
       2.007     1.712    35.58    40.46     3.95     0.760     0.987
       2.007     1.572    33.71    38.07     3.56     0.756     0.982
       2.007     1.432    31.75    35.51     3.17     0.767     0.996
       2.007     1.292    29.70    32.77     2.79     0.825     1.071
       2.007     1.152    27.57    29.85     2.40     0.930     1.208
       2.007     0.872    23.05    23.48     1.63     1.103     1.432
       2.007     0.732    20.67    20.03     1.24     1.129     1.466
       2.007     0.592    18.20    16.43     0.85     1.171     1.521
       2.007     0.452    15.67    12.69     0.47     1.388     1.803
       2.007     0.312    13.07     8.83     0.08     1.525     1.981
       2.376     1.712    32.40    35.77     3.21     0.768     0.997
       2.376     1.572    30.62    33.49     2.89     0.775     1.006
       2.376     1.432    28.76    31.08     2.56     0.862     1.119
       2.376     1.292    26.84    28.53     2.23     0.959     1.245
       2.376     1.152    24.85    25.86     1.91     1.037     1.347
       2.376     1.012    22.80    23.07     1.58     1.082     1.405
       2.376     0.872    20.68    20.15     1.25     1.118     1.452
       2.376     0.732    18.50    17.12     0.93     1.121     1.456
       2.376     0.592    16.26    13.99     0.60     1.269     1.648
       2.376     0.452    13.97    10.76     0.27     1.510     1.961




Surface pressure data for tap rows with plug rotated 30-deg and
fin angle of attack of 16-deg.

  VCOp at X=  -0.476 in.,  Y=  -0.227 in., PE = 0.720 psia

         X         Y      BEVCO    BEFLE   DELY/YS      P        P/PE
       (in.)     (in.)    (deg)    (deg)             (psia)
       0.442     0.952    52.08    65.07     9.69     0.712     0.989
       0.512     0.831    46.94    58.33     6.94     0.712     0.989
       0.582     0.709    41.50    50.62     4.84     0.830     1.153
       0.652     0.588    35.85    42.04     3.20     1.206     1.675
       0.722     0.467    30.08    32.88     1.87     1.317     1.829
       0.792     0.346    24.30    23.57     0.78     1.671     2.321
       1.060     1.955    54.86    61.54     8.10     0.723     1.004
       1.130     1.834    52.08    58.36     6.95     0.717     0.996
       1.200     1.712    49.18    54.99     5.93     0.710     0.986
       1.270     1.591    46.17    51.41     5.02     0.707     0.982
       1.340     1.470    43.07    47.66     4.21     0.723     1.004
       1.379     2.139    51.91    57.19     6.57     0.732     1.017
       1.410     1.349    39.88    43.73     3.48     0.977     1.357
       1.449     2.018    49.39    54.32     5.75     0.722     1.003
       1.480     1.227    36.64    39.68     2.82     1.261     1.751
       1.519     1.897    46.79    51.31     5.00     0.719     0.999
       1.550     1.106    33.35    35.52     2.22     1.354     1.881
       1.589     1.776    44.12    48.17     4.32     0.719     0.999
       1.620     0.985    30.04    31.31     1.67     1.328     1.844
       1.659     1.654    41.39    44.92     3.69     0.811     1.126
       1.690     0.864    26.73    27.08     1.17     1.287     1.787
       1.729     1.533    38.60    41.56     3.12     1.132     1.572
       1.760     0.743    23.45    22.88     0.70     1.730     2.403
       1.799     1.412    35.77    38.12     2.59     1.275     1.771
       1.830     0.621    20.20    18.76     0.27     2.760     3.833
       1.869     1.291    32.91    34.63     2.10     1.353     1.879
       1.939     1.170    30.04    31.09     1.64     1.338     1.858
       2.009     1.048    27.16    27.55     1.22     1.266     1.758
       2.079     0.927    24.31    24.03     0.83     1.516     2.106


Spanwise surface pressure data for tap rows with plug rotated 30-deg and
fin angle of attack of 16-deg.

  VCOp at X=  -0.476 in.,  Y=  -0.227 in., PE = 0.810 psia

         X         Y      BEVCO    BEFLE   DELY/YS      P        P/PE
       (in.)     (in.)    (deg)    (deg)             (psia)
       0.938     1.640    52.86    60.23     7.60     0.789     0.974
       0.938     1.500    50.69    57.98     6.82     0.775     0.957
       0.938     1.360    48.30    55.40     6.04     0.775     0.957
       0.938     1.220    45.66    52.44     5.27     0.779     0.962
       0.938     1.080    42.75    49.02     4.49     0.791     0.977
       0.938     0.940    39.53    45.06     3.72     1.025     1.265
       0.938     0.800    35.99    40.46     2.94     1.280     1.580
       0.938     0.660    32.10    35.13     2.17     1.400     1.728
       1.974     2.200    44.73    48.10     4.30     0.811     1.001
       1.974     2.060    43.03    46.22     3.93     0.801     0.989
       1.974     1.920    41.23    44.20     3.57     0.864     1.067
       1.974     1.780    39.32    42.04     3.20     1.092     1.348
       1.974     1.640    37.31    39.72     2.83     1.287     1.589
       1.974     1.500    35.18    37.23     2.46     1.399     1.727
       1.974     1.360    32.93    34.56     2.09     1.426     1.760
       1.974     1.220    30.57    31.72     1.72     1.415     1.747
       1.974     1.080    28.08    28.68     1.35     1.324     1.635
       1.974     0.940    25.47    25.46     0.98     1.437     1.774
       1.974     0.800    22.74    22.06     0.62     2.008     2.479
       1.974     0.660    19.90    18.49     0.25     3.107     3.836
       2.343     2.200    40.73    43.20     3.39     0.884     1.091
       2.343     2.060    39.05    41.32     3.08     1.093     1.349
       2.343     1.920    37.29    39.33     2.77     1.278     1.578
       2.343     1.780    35.45    37.22     2.46     1.365     1.685
       2.343     1.640    33.52    34.99     2.15     1.423     1.757
       2.343     1.500    31.49    32.63     1.84     1.447     1.786
       2.343     1.360    29.38    30.13     1.53     1.361     1.680
       2.343     1.220    27.17    27.50     1.22     1.335     1.648
       2.343     1.080    24.87    24.75     0.91     1.487     1.836
       2.343     0.940    22.49    21.86     0.59     2.052     2.533
       2.343     0.800    20.02    18.85     0.28     3.209     3.962


****************** Surface Flow Visualization Results ***************

The following table lists the results from the SFVP study.  The inception
length (LI), and angles of upstream influence (BETAU) and primary
separation line (BETAS1) are presented below (DELTA=0.25 in.).

  ALPHA           LI/DELTA               BETAU         BETAS1
  (deg)                                  (deg)           (deg)
   6.0              4.44                  22.            20.
   8.0              4.28                  26.            23.
  10.0              3.76                  29.            27.
  12.0              3.16                  34.            31.
  14.0              2.72                  36.            34.
  15.0 (Gibson)     N/A                   36.            34.



Using the primary separation line (clearly seen on the SFVP) and the inviscid
shock trace (calculated analytically) a VCO can be determined from the
intersection of these two features.


 Location of VCOv from Primary Separation Line and Inviscid Shock Wave

       ALPHA                 X/DELTA                    Y/DELTA
       (deg)
        6.0                   -6.64                      -2.04
        8.0                   -5.48                      -1.76
       10.0                   -4.52                      -1.60
       12.0                   -3.48                      -1.36
       14.0                   -3.24                      -1.40


The locations of the virtual conical origin of the pressure fields, obtained
by matching features of the various cross plane distributions and
extrapolating back to the VCOp, are list below.


             Location of VCOp from Pressure Distributions

  ALPHA               X/DELTA                     Y/DELTA
  (deg)
   8.0                 -3.55                       -1.44
  16.0                 -1.90                       -0.91




****************** Spanwise Heat Transfer Data **********************


Next are given the spanwise heat transfer measurements for fin angles
of attack of 6-, 8-, 10-, 12- ,14- and 16-degrees.  Data from four runs
were combined to produce a distribution with increased spatial resolution.


     ALPHA=  6.000   BETAO=  16.100


   TO=  299.04(F)    CHE= 0.00050
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.009  1.886  1.675  0.369   4.54   78.53   0.696   0.00050   1.000
   2.009  1.324  1.113  0.369   3.02   82.59   0.705   0.00052   1.040
   2.009  1.043  0.832  0.369   2.26   81.23   0.790   0.00058   1.160
   2.009  0.762  0.551  0.369   1.49   92.07   0.841   0.00066   1.320
   2.009  0.481  0.270  0.369   0.73   87.39   1.346   0.00103   2.060


   TO=  301.52(F)    CHE= 0.00050
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.009  1.685  1.474  0.369   4.00   95.15   0.691   0.00055   1.100
   2.009  1.404  1.193  0.369   3.24   94.20   0.632   0.00050   1.000
   2.009  1.123  0.912  0.369   2.47  105.65   0.749   0.00064   1.280
   2.009  0.842  0.631  0.369   1.71   99.27   0.792   0.00065   1.300
   2.009  0.561  0.350  0.369   0.95  101.08   1.036   0.00086   1.720


   TO=  303.45(F)    CHE= 0.00049
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.009  1.746  1.535  0.369   4.16  103.76   0.577   0.00048   0.980
   2.009  1.465  1.254  0.369   3.40  103.72   0.599   0.00050   1.020
   2.009  1.184  0.973  0.369   2.64  105.50   0.685   0.00058   1.184
   2.009  0.903  0.692  0.369   1.88  105.37   0.756   0.00064   1.306
   2.009  0.622  0.411  0.369   1.11  114.88   0.843   0.00077   1.571
   2.009  0.341  0.130  0.369   0.35   98.14   1.281   0.00103   2.102


   TO=  301.94(F)    CHE= 0.00050
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.009  1.816  1.605  0.369   4.35   86.19   0.668   0.00050   1.000
   2.009  1.535  1.324  0.369   3.59   86.80   0.679   0.00051   1.020
   2.009  1.254  1.043  0.369   2.83   89.36   0.724   0.00055   1.100
   2.009  0.973  0.762  0.369   2.07   88.76   0.767   0.00058   1.160
   2.009  0.692  0.481  0.369   1.30   97.39   0.828   0.00067   1.340
   2.009  0.411  0.200  0.369   0.54   86.88   1.411   0.00106   2.120


     ALPHA=  8.000   BETAO=  17.800


   TO=  301.60(F)    CHE= 0.00050
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.007  1.967  1.685  0.362   4.65   95.60   0.624   0.00050   1.000
   2.007  1.405  1.123  0.362   3.10   97.08   0.633   0.00051   1.020
   2.007  1.124  0.842  0.362   2.32   95.74   0.766   0.00061   1.220
   2.007  0.843  0.561  0.362   1.55  108.30   0.804   0.00071   1.420
   2.007  0.562  0.280  0.362   0.77  101.39   1.413   0.00118   2.360


   TO=  300.61(F)    CHE= 0.00049
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.007  1.756  1.474  0.362   4.07   97.62   0.672   0.00055   1.122
   2.007  1.475  1.193  0.362   3.29   96.08   0.613   0.00049   1.000
   2.007  1.194  0.912  0.362   2.52  108.52   0.802   0.00071   1.449
   2.007  0.913  0.631  0.362   1.74  101.06   0.765   0.00064   1.306
   2.007  0.632  0.350  0.362   0.97  104.13   1.179   0.00101   2.061


   TO=  303.74(F)    CHE= 0.00048
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.007  1.817  1.535  0.362   4.24   92.20   0.629   0.00048   1.000
   2.007  1.536  1.254  0.362   3.46   94.04   0.654   0.00051   1.062
   2.007  1.255  0.973  0.362   2.69   95.94   0.788   0.00062   1.292
   2.007  0.974  0.692  0.362   1.91   95.73   0.826   0.00065   1.354
   2.007  0.693  0.411  0.362   1.13  106.70   1.096   0.00094   1.958
   2.007  0.412  0.130  0.362   0.36   89.25   1.699   0.00128   2.667


   TO=  303.88(F)    CHE= 0.00048
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.007  1.897  1.615  0.362   4.46   98.64   0.603   0.00048   1.000
   2.007  1.616  1.334  0.362   3.68   97.71   0.613   0.00049   1.021
   2.007  1.335  1.053  0.362   2.91  100.58   0.676   0.00055   1.146
   2.007  1.054  0.772  0.362   2.13  100.04   0.727   0.00059   1.229
   2.007  0.773  0.491  0.362   1.36  108.73   0.934   0.00081   1.688
   2.007  0.492  0.210  0.362   0.58   99.36   1.565   0.00126   2.625


     ALPHA= 10.000   BETAO=  19.600


   TO=  302.85(F)    CHE= 0.00050
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.002  2.028  1.675  0.360   4.65   98.30   0.619   0.00050   1.000
   2.002  1.466  1.113  0.360   3.09   99.48   0.638   0.00052   1.040
   2.002  1.185  0.832  0.360   2.31   98.29   0.772   0.00062   1.240
   2.002  0.904  0.551  0.360   1.53  111.23   0.927   0.00083   1.660
   2.002  0.623  0.270  0.360   0.75  104.30   1.582   0.00134   2.680


   TO=  304.07(F)    CHE= 0.00049
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.002  1.817  1.464  0.360   4.07  112.22   0.611   0.00054   1.102
   2.002  1.536  1.183  0.360   3.29  109.42   0.565   0.00049   1.000
   2.002  1.255  0.902  0.360   2.51  122.55   0.791   0.00077   1.571
   2.002  0.974  0.621  0.360   1.73  115.34   0.764   0.00070   1.429
   2.002  0.693  0.340  0.360   0.94  118.23   1.251   0.00117   2.388


   TO=  304.30(F)    CHE= 0.00049
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.002  1.878  1.525  0.360   4.24  105.29   0.567   0.00048   0.980
   2.002  1.597  1.244  0.360   3.46  105.97   0.586   0.00050   1.020
   2.002  1.316  0.963  0.360   2.68  108.40   0.818   0.00071   1.449
   2.002  1.035  0.682  0.360   1.89  107.93   0.741   0.00064   1.306
   2.002  0.754  0.401  0.360   1.11  119.63   1.146   0.00108   2.204
   2.002  0.473  0.120  0.360   0.33  102.61   1.786   0.00148   3.020


   TO=  304.04(F)    CHE= 0.00049
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   2.002  1.968  1.615  0.360   4.49   92.27   0.637   0.00049   1.000
   2.002  1.687  1.334  0.360   3.71   93.57   0.645   0.00050   1.020
   2.002  1.406  1.053  0.360   2.93   96.99   0.756   0.00060   1.224
   2.002  1.125  0.772  0.360   2.15   95.99   0.741   0.00058   1.184
   2.002  0.844  0.491  0.360   1.36  105.81   1.096   0.00093   1.898
   2.002  0.563  0.210  0.360   0.58   97.12   1.929   0.00153   3.122


     ALPHA= 12.000   BETAO=  21.500


   TO=  303.24(F)    CHE= 0.00048
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.995  2.079  1.655  0.362   4.57   97.46   0.594   0.00048   1.000
   1.995  1.798  1.374  0.362   3.80   98.46   0.591   0.00048   1.000
   1.995  1.517  1.093  0.362   3.02  101.83   0.675   0.00056   1.167
   1.995  1.236  0.812  0.362   2.24  101.86   0.721   0.00060   1.250
   1.995  0.955  0.531  0.362   1.47  112.75   1.096   0.00099   2.062
   1.995  0.674  0.250  0.362   0.69  108.37   1.757   0.00153   3.188


   TO=  303.11(F)    CHE= 0.00052
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.995  1.898  1.474  0.362   4.07  120.99   0.544   0.00053   1.019
   1.995  1.617  1.193  0.362   3.30  117.53   0.550   0.00052   1.000
   1.995  1.336  0.912  0.362   2.52  131.11   0.680   0.00072   1.385
   1.995  1.055  0.631  0.362   1.74  124.72   0.919   0.00092   1.769
   1.995  0.774  0.350  0.362   0.97  127.23   1.308   0.00134   2.577


   TO=  305.38(F)    CHE= 0.00047
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.995  1.959  1.535  0.362   4.24  108.89   0.550   0.00047   1.000
   1.995  1.678  1.254  0.362   3.47  111.07   0.571   0.00050   1.064
   1.995  1.397  0.973  0.362   2.69  113.89   0.862   0.00077   1.638
   1.995  1.116  0.692  0.362   1.91  113.74   0.793   0.00071   1.511
   1.995  0.835  0.411  0.362   1.14  125.03   1.279   0.00126   2.681
   1.995  0.554  0.130  0.362   0.36  109.17   2.004   0.00173   3.681


   TO=  306.20(F)    CHE= 0.00047
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.995  2.029  1.605  0.362   4.44  112.46   0.531   0.00047   1.000
   1.995  1.748  1.324  0.362   3.66  113.21   0.538   0.00048   1.021
   1.995  1.467  1.043  0.362   2.88  117.31   0.818   0.00075   1.596
   1.995  1.186  0.762  0.362   2.11  115.95   0.668   0.00061   1.298
   1.995  0.905  0.481  0.362   1.33  126.00   1.173   0.00116   2.468
   1.995  0.624  0.200  0.362   0.55  117.67   1.900   0.00175   3.723


     ALPHA= 14.000   BETAO=  23.500


   TO=  305.11(F)    CHE= 0.00049
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.986  2.150  1.655  0.368   4.49   96.90   0.617   0.00049   1.000
   1.986  1.869  1.374  0.368   3.73   97.57   0.614   0.00049   1.000
   1.986  1.588  1.093  0.368   2.97  101.80   0.949   0.00078   1.592
   1.986  1.307  0.812  0.368   2.20  100.79   0.756   0.00061   1.245
   1.986  1.026  0.531  0.368   1.44  117.21   1.312   0.00121   2.469
   1.986  0.745  0.250  0.368   0.68  104.87   2.037   0.00170   3.469


   TO=  303.24(F)    CHE= 0.00052
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.986  1.969  1.474  0.368   4.00  120.47   0.553   0.00053   1.019
   1.986  1.688  1.193  0.368   3.24  117.60   0.669   0.00063   1.212
   1.986  1.407  0.912  0.368   2.48  130.81   0.668   0.00071   1.365
   1.986  1.126  0.631  0.368   1.71  124.59   1.071   0.00107   2.058
   1.986  0.845  0.350  0.368   0.95  127.04   1.381   0.00141   2.712


   TO=  305.97(F)    CHE= 0.00047
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.986  2.030  1.535  0.368   4.17  108.02   0.545   0.00046   0.979
   1.986  1.749  1.254  0.368   3.40  110.57   0.592   0.00051   1.085
   1.986  1.468  0.973  0.368   2.64  113.16   0.796   0.00071   1.511
   1.986  1.187  0.692  0.368   1.88  113.99   0.988   0.00088   1.872
   1.986  0.906  0.411  0.368   1.12  125.19   1.432   0.00141   3.000
   1.986  0.625  0.130  0.368   0.35  109.26   2.304   0.00198   4.213


   TO=  307.09(F)    CHE= 0.00047
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.986  2.110  1.615  0.368   4.38  128.55   0.447   0.00045   0.957
   1.986  1.829  1.334  0.368   3.62  128.67   0.469   0.00047   1.000
   1.986  1.548  1.053  0.368   2.86  132.56   0.656   0.00068   1.447
   1.986  1.267  0.772  0.368   2.10  131.53   0.704   0.00073   1.553
   1.986  0.986  0.491  0.368   1.33  140.63   1.165   0.00131   2.787
   1.986  0.705  0.210  0.368   0.57  132.58   1.794   0.00187   3.979


     ALPHA= 16.000   BETAO=  25.600


   TO=  307.76(F)    CHE= 0.00048
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.974  2.241  1.675  0.380   4.41  112.58   0.554   0.00048   1.000
   1.974  1.960  1.394  0.380   3.67  110.93   0.557   0.00048   1.000
   1.974  1.679  1.113  0.380   2.93  115.65   0.882   0.00079   1.646
   1.974  1.398  0.832  0.380   2.19  114.25   0.585   0.00052   1.083
   1.974  1.117  0.551  0.380   1.45  130.01   1.353   0.00137   2.854
   1.974  0.836  0.270  0.380   0.71  120.91   1.907   0.00178   3.708


   TO=  304.50(F)    CHE= 0.00051
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.974  2.050  1.484  0.380   3.91  126.36   0.514   0.00052   1.020
   1.974  1.769  1.203  0.380   3.17  125.88   0.758   0.00076   1.490
   1.974  1.488  0.922  0.380   2.43  138.95   0.694   0.00079   1.549
   1.974  1.207  0.641  0.380   1.69  133.34   1.184   0.00127   2.490
   1.974  0.926  0.360  0.380   0.95  135.05   1.335   0.00145   2.843


   TO=  307.23(F)    CHE= 0.00047
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.974  2.101  1.535  0.380   4.04  112.88   0.529   0.00046   0.979
   1.974  1.820  1.254  0.380   3.30  113.70   0.750   0.00066   1.404
   1.974  1.539  0.973  0.380   2.56  116.11   0.746   0.00067   1.426
   1.974  1.258  0.692  0.380   1.82  117.84   1.151   0.00105   2.234
   1.974  0.977  0.411  0.380   1.08  128.62   1.427   0.00143   3.043
   1.974  0.696  0.130  0.380   0.34  113.87   2.487   0.00220   4.681


   TO=  306.80(F)    CHE= 0.00047
     X      Y    DELY    YS   DELY/YS   TW     QDOT      CH     CH/CHE
   (in.)  (in.)  (in.)                  (F) (BTU/FT^2sec)
   1.974  2.171  1.605  0.380   4.23  114.05   0.531   0.00047   1.000
   1.974  1.890  1.324  0.380   3.49  115.62   0.572   0.00051   1.085
   1.974  1.609  1.043  0.380   2.75  119.62   0.734   0.00068   1.447
   1.974  1.328  0.762  0.380   2.01  118.72   0.866   0.00080   1.702
   1.974  1.047  0.481  0.380   1.27  128.88   1.315   0.00133   2.830
   1.974  0.766  0.200  0.380   0.53  121.11   2.133   0.00201   4.277


*************** Heat Transfer along Concial Cross-planes *************

Next are given the heat transfer data taken in conical cross-plane
coordinates for the 8- and 16-degree cases.  Each row of data (either row 2
or row 4) is normalized by the local edge value.  Data from four runs were
combined to increase the spatial resolution.  Since no VCO could be
found to collapse the heat transfer data, VCO and BEVCO are not listed.  Also,
the spanwise data for the 8- and 16-degree cases are listed along with the
other spanwise data and not included here.


            ALPHA=8.0                           THETA=15.0

    TO=  299.49(F)
    CHE(row2)=  0.00060   CHE(row4)=  0.00053
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.676    1.053   57.28    7.84   93.40    0.753   0.00060   0.99714
      0.749    0.782   46.21    5.00   93.11    0.742   0.00059   0.98052
      0.822    0.510   31.83    2.66   95.23    0.927   0.00075   1.24398
      0.894    0.239   14.95    0.70   97.47    1.405   0.00115   1.91691
(row 4)
      1.888    1.960   46.06    4.97   89.98    0.695   0.00054   1.01674
      1.961    1.688   40.72    3.99   93.33    0.655   0.00052   0.98141
      2.033    1.417   34.86    3.08   95.04    0.677   0.00054   1.02709
      2.106    1.146   28.53    2.23   96.29    0.834   0.00068   1.27693
      2.179    0.874   21.85    1.44   95.88    0.778   0.00063   1.18760
      2.252    0.603   14.98    0.70   98.09    1.400   0.00115   2.17245

    TO=  300.43(F)
    CHE(row2)=  0.00060   CHE(row4)=  0.00054
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.731    0.850   49.31    5.66   96.05    0.749   0.00060   1.00551
      0.803    0.579   35.76    3.21   96.71    0.883   0.00071   1.19117
      0.876    0.308   19.33    1.16   97.12    1.024   0.00083   1.38555
(row 4)
      1.942    1.757   42.12    4.23   94.42    0.679   0.00054   1.00086
      2.015    1.486   36.39    3.30   96.00    0.689   0.00055   1.02732
      2.088    1.214   30.17    2.44   98.74    0.810   0.00067   1.23248
      2.160    0.943   23.57    1.64   99.17    0.725   0.00060   1.10676
      2.233    0.671   16.72    0.89  100.36    1.085   0.00090   1.67125

    TO=  298.61(F)
    CHE(row2)=  0.00058   CHE(row4)=  0.00052
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.712    0.918   52.16    6.35   97.46    0.691   0.00057   0.98045
      0.785    0.647   39.45    3.78   98.08    0.701   0.00058   0.99936
      0.858    0.375   23.60    1.64  100.23    1.114   0.00094   1.61417
(row 4)
      1.924    1.825   43.47    4.47   97.57    0.628   0.00052   0.99477
      1.997    1.553   37.87    3.53   98.68    0.616   0.00051   0.98393
      2.070    1.282   31.76    2.65  100.04    0.737   0.00062   1.18946
      2.142    1.010   25.24    1.83  100.58    0.799   0.00067   1.29487
      2.215    0.739   18.44    1.07  101.25    0.916   0.00078   1.49217

    TO=  299.46(F)
    CHE(row2)=  0.00061   CHE(row4)=  0.00055
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.694    0.986   54.82    7.08   88.68    0.828   0.00064   1.04304
      0.767    0.714   42.94    4.38   88.61    0.766   0.00059   0.96445
      0.840    0.443   27.78    2.14   89.31    0.961   0.00074   1.21590
      0.913    0.171   10.63    0.26   92.69    1.544   0.00122   2.00115
(row 4)
      1.906    1.892   44.78    4.72   85.39    0.726   0.00055   0.99147
      1.979    1.621   39.31    3.76   88.25    0.711   0.00054   0.99033
      2.051    1.349   33.33    2.86   89.84    0.734   0.00057   1.03389
      2.124    1.078   26.90    2.03   90.15    0.814   0.00063   1.14909
      2.197    0.806   20.15    1.25   92.30    0.949   0.00075   1.36034



             ALPHA=16.0                           THETA=30.0

    TO=  300.64(F)
    CHE(row2)=  0.00062   CHE(row4)=  0.00053
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.441    0.955   65.20    9.76   96.17    0.768   0.00062   0.99732
      0.581    0.711   50.73    4.87   97.20    0.830   0.00067   1.08607
      0.722    0.468   32.95    1.88   98.17    0.875   0.00071   1.15319
(row 4)
      1.377    2.144   57.29    6.60   95.01    0.690   0.00055   1.03935
      1.517    1.900   51.40    5.02   96.14    0.641   0.00052   0.97360
      1.658    1.657   44.99    3.71   99.15    0.656   0.00054   1.01878
      1.798    1.414   38.17    2.60  100.28    0.823   0.00068   1.28910
      1.939    1.170   31.12    1.65  102.90    1.231   0.00104   1.96708
      2.079    0.927   24.03    0.83  105.72    1.774   0.00154   2.89759

    TO=  301.42(F)
    CHE(row2)=  0.00068   CHE(row4)=  0.00054
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.546    0.773   54.76    5.87  102.33    0.805   0.00068   0.99331
      0.686    0.529   37.64    2.52  104.26    0.979   0.00083   1.22601
      0.827    0.286   19.08    0.31  104.20    1.407   0.00120   1.76126
(row 4)
      1.482    1.962   52.94    5.39   98.90    0.660   0.00054   0.99933
      1.622    1.719   46.65    4.02  102.16    0.658   0.00055   1.02108
      1.763    1.475   39.93    2.86  105.62    1.010   0.00087   1.60975
      1.903    1.232   32.91    1.87  107.51    0.923   0.00081   1.49314
      2.044    0.989   25.81    1.02  110.20    1.392   0.00124   2.30107

    TO=  297.97(F)
    CHE(row2)=  0.00059   CHE(row4)=  0.00052
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.511    0.833   58.48    6.99   94.05    0.737   0.00059   1.00631
      0.651    0.590   42.17    3.22   96.33    1.054   0.00086   1.46363
      0.792    0.347   23.64    0.78   96.50    1.407   0.00115   1.95632
(row 4)
      1.447    2.023   54.42    5.78   93.62    0.649   0.00052   1.00226
      1.587    1.779   48.26    4.34   95.66    0.634   0.00052   0.99394
      1.728    1.536   41.64    3.13   98.65    1.001   0.00083   1.60499
      1.868    1.292   34.68    2.11   99.36    0.998   0.00084   1.60880
      2.009    1.049   27.58    1.22  102.99    1.363   0.00118   2.25983

    TO=  299.75(F)
    CHE(row2)=  0.00066   CHE(row4)=  0.00054
        X        Y     BEFLE    YYS     TW      QDOT      CH      CH/CHE
      (in.)    (in.)   (deg)           (F)  (BTU/FT^2sec)
(row 2)
      0.476    0.894   61.97    8.27   99.43    0.796   0.00066   1.00033
      0.616    0.651   46.54    4.00  101.21    1.106   0.00093   1.40878
      0.757    0.407   28.28    1.31  101.93    1.308   0.00111   1.67538
(row 4)
      1.412    2.083   55.87    6.18   95.42    0.673   0.00054   1.00332
      1.552    1.840   49.85    4.67   98.68    0.651   0.00054   0.99429
      1.693    1.596   43.32    3.41  101.72    0.931   0.00079   1.45514
      1.833    1.353   36.43    2.35  101.98    0.818   0.00069   1.28106
      1.974    1.110   29.35    1.43  107.72    1.433   0.00127   2.34795



************* Heat Transfer Along Rays from the VCOp *****************


The radial distance from the VCOp, r, is measured in inches.  CHU is the
undisturbed turbulent boundary layer heat transfer measured by the particular
Schmidt-Boelter gage in use.

For the ALPHA=8.0 fin angle, five transducers were positioned along each
of two rays.  The ten transducers were all measured during the same run.
The identical configuration of transducer pattern and individual gage
placement was used four runs (run# 122-125).


             Location of VCOp from Pressure Distributions

  ALPHA=8.0           X/DELTA                     Y/DELTA
   8.0                 -3.55                       -1.44


           ALPHA=8.0,                   BEVCO=18.0

       r=2.5 in.     r=3.0 in.    r=3.5 in.      r=4.0 in.     r=4.5 in.
run    CH CH/CHU     CH CH/CHU    CH CH/CHU      CH CH/CHU     CH CH/CHU
 #   (X10^5)       (X10^5)      (X10^5)        (X10^5)       (X10^5)
__________________________________________________________________________

122   103  1.72     105  1.81     88  1.60       99  1.77     104  1.73
123   102  1.70     104  1.79     86  1.56       97  1.73     102  1.70
124   103  1.72     108  1.86     91  1.65      103  1.84     109  1.82
125   101  1.68      99  1.71     88  1.61       97  1.73     108  1.80


           ALPHA=8.0,                   BEVCO=28.0

       r=2.5 in.     r=3.0 in.    r=3.5 in.      r=4.0 in.     r=4.5 in.
run    CH CH/CHU     CH CH/CHU    CH CH/CHU      CH CH/CHU     CH CH/CHU
 #   (X10^5)       (X10^5)      (X10^5)        (X10^5)       (X10^5)
__________________________________________________________________________

122    70  1.25      68  1.21     65  1.20       64  1.16      67  1.20
123    70  1.25      68  1.21     64  1.19       63  1.15      67  1.18
124    72  1.29      70  1.25     67  1.24       66  1.20      70  1.25
125    72  1.29      68  1.21     63  1.17       62  1.13      67  1.20



For the ALPHA=16.0 fin angle, again five transducers were positioned along
each of two rays and the transducers were all measured during the same run.
The identical configuration of transducer pattern and individual gage
placement was used the first three runs (runs# 134-136).  The gages were
removed from the ten transducer positions and redistributed.  Three runs
were made with the second gage distribution (runs# 138-141).  This permitted
a two different gages to measure the heat transfer at each transducer position.


             Location of VCOp from Pressure Distributions

  ALPHA=16.0          X/DELTA                     Y/DELTA
                       -1.90                       -0.91

           ALPHA=16.0,                   BEVCO=27.0

       r=2.5 in.     r=3.0 in.    r=3.5 in.      r=4.0 in.     r=4.5 in.
run    CH CH/CHU     CH CH/CHU    CH CH/CHU      CH CH/CHU     CH CH/CHU
 #   (X10^5)       (X10^5)      (X10^5)        (X10^5)       (X10^5)
__________________________________________________________________________

134   113  2.02     121  2.16    123  2.28      129  2.35     124  2.21
135   113  2.02     121  2.16    124  2.30      130  2.36     124  2.21
136   112  2.00     121  2.16    124  2.30      132  2.40     126  2.25

138   128  2.13     N/A   N/A    130  2.36      129  2.22     136  2.27
140   127  2.12     N/A   N/A    130  2.36      129  2.22     136  2.27
141   122  2.03     N/A   N/A    125  2.27      125  2.16     132  2.20


           ALPHA=16.0,                   BEVCO=33.0

       r=2.5 in.     r=3.0 in.    r=3.5 in.      r=4.0 in.     r=4.5 in.
run    CH CH/CHU     CH CH/CHU    CH CH/CHU      CH CH/CHU     CH CH/CHU
 #   (X10^5)       (X10^5)      (X10^5)        (X10^5)       (X10^5)
__________________________________________________________________________

134    79  1.32      74  1.28     70  1.27      N/A  N/A       81  1.35
135    79  1.32      73  1.26     69  1.25      N/A  N/A       79  1.32
136    80  1.33      73  1.26     68  1.24      N/A  N/A       78  1.30

138    77  1.38      80  1.45     75  1.39       84  1.50      80  1.43
140    76  1.36      79  1.44     74  1.37       83  1.48      79  1.43
141    72  1.29      73  1.33     68  1.26       76  1.39      71  1.27

*****************************END OF FILE*********************************
