*****************Kussoy et al, Ogive-Cylinder-Flare, Mach 7********************

*****************Freestream Flow Conditions************************************

Minf = 7.05
Tinf = 81.2 deg K
Pinf = 576 Pa
RHOinf = 0.0252 kg/m**3
Twall = 311 deg K
Uinf = 1274 m/s
Re/m = 5.8E+06

****************Incoming Boundary-Layer Conditions*****************************

DELTA = 2.5 cm
DELTA* = 0.74 cm
THETA = 0.065 cm
Cfinf = 1.22E-03
Chinf = 0.59E-03

Y, cm    M         U/Uinf    TT/TTinf
0.000    0.000     0.000     0.350
0.065    1.547     0.470     0.638
0.093    2.177     0.601     0.690
0.120    2.745     0.699     0.752
0.180    3.111     0.759     0.805
0.250    3.356     0.791     0.830
0.320    3.610     0.822     0.858
0.390    3.835     0.836     0.858
0.460    4.070     0.858     0.877
0.620    4.626     0.896     0.905
0.770    5.248     0.929     0.930
0.940    5.739     0.954     0.954
1.090    6.070     0.967     0.966
1.260    6.340     0.982     0.986
1.450    6.599     0.986     0.986
1.640    6.820     0.992     0.991
1.900    6.962     0.999     1.000
2.150    7.022     1.000     1.000
2.400    7.048     1.000     1.000
2.700    7.050     1.000     1.000
3.000    7.050     1.000     1.000

*************Wall Pressure and Heat Transfer Distributions*********************

Alpha = 20 degrees                     Alpha = 30 degrees

X, cm Pw/Pinf|  X, cm   Qw/Qinf        X, cm   Pw/Pinf |  X, cm    Qw/Qinf
-11.3   0.97 |  12.06   0.98            -11.3   1.00   |  -12.08   0.99
-10.3   0.98 |  -10.8   1.05            -10.3   0.98   |  -10.8    0.99
-9.3    0.96 |  -9.52   1.06            -9.3    0.97   |  -9.52    1.0
-8.3    0.98 |  -8.26   1.02            -8.3    0.98   |  -8.26    1.0
-7.3    0.97 |  -6.98   1.03            -7.3    1.0    |  -6.98    1.01
-6.3    0.99 |  -5.73   1.0             -6.3    1.0    |  -5.73    1.01
-5.3    1.03 |  -4.44   1.03            -5.3    0.98   |  -4.44    1.0
-4.3    1.00 |  -3.18   1.01            -4.3    1.02   |  -3.18    0.99
-3.3    1.02 |  -1.9    0.99            -3.3    1.09   |  -1.9     0.99
-2.3    1.0  |  -0.64   0.86            -2.3    1.39   |  -0.64    1.02
-1.3    1.09 |  1.1     4.79            -1.3    1.73   |  1.1      8.2
1.1     2.02 |  1.6     4.17            1.1     7.75   |  1.6      8.97
1.6     3.68 |  2.1     4.99            1.6     9.58   |  2.1      10.09
2.1     5.31 |  2.6     5.27            2.1     12.85  |  3.1      12.05
2.6     5.96 |  3.1     5.94            2.6     15.06  |  3.6      13.42
3.6     7.42 |  3.6     5.74            3.6     19.51  |  4.6      14.39
4.1     8.27 |  4.6     6.04            4.1     21.33  |  5.1      15.25
4.6     9.10 |  5.1     7.99            4.6     21.94  |  6.1      14.86
5.1     9.95 |  6.1     8.59            6.1     22.82  |  7.1      14.9
6.1     10.8 |  7.1     8.74            7.1     22.88  |  8.1      14.6
7.1     11.3 |  8.1     8.64            8.1     23.71  |  9.1      14.75
10.1    12.14|  9.1     8.77            10.1    24.4   |  10.1     14.45
12.1    12.26|  10.1    9.18            12.1    23.62  |  11.1     14.41
14.1    12.5 |  12.1    9.68            14.1    22.6   |  12.1     13.98
                13.1    9.59                              13.1     13.02
                14.1    9.36                              14.1     12.87
                15.1    8.55                              15.1     12.21

Alpha = 32.5 degrees                   Alpha = 35 degrees

X, cm Pw/Pinf|  X, cm   Qw/Qinf         X, cm  Pw/Pinf |  X, cm     Qw/Qinf
-11.3   1.01 |  -12.06  1.0             -11.3   0.97   |  -12.06    0.99
-10.3   0.99 |  -10.8   0.99            -10.3   0.98   |  -10.8     1.07
-9.3    0.98 |  -9.52   1.0             -9.3    1.0    |  -9.52     1.0
-8.3    1.01 |  -8.26   1.01            -8.3    1.15   |  -8.26     1.04
-7.3    0.97 |  -6.98   1.03            -7.3    1.45   |  -6.98     1.02
-6.3    1.01 |  -5.73   1.01            -6.3    2.01   |  -5.73     1.26
-5.3    1.03 |  -4.44   1.05            -5.3    2.53   |  -4.44     1.83
-4.3    1.12 |  -3.18   1.09            -4.3    3.25   |  -3.18     2.39
-3.3    1.23 |  -1.9    1.33            -3.3    3.63   |  -1.9      2.63
-2.3    1.71 |  -0.64   2.16            -2.3    4.41   |  -0.64     2.55
-1.3    2.56 |  1.05    6.79            -1.3    4.56   |  1.07      6.4
0.55    5.85 |  1.55    7.44            1.07    6.95   |  1.57      7.9
1.05    7.50 |  2.05    9.23            1.57    8.82   |  2.07      9.65
1.55    8.42 |  2.55    10.64           2.07    11.07  |  2.57      11.75
2.05    12.02|  3.05    12.82           2.57    14.05  |  3.07      13.82
2.55    14.4 |  3.55    14.55           3.07    18.45  |  3.57      16.1
3.55    21.19|  4.55    16.28           3.57    21.79  |  5.07      20.03
4.05    23.57|  5.05    17.05           4.07    25.71  |  6.07      21.96
4.55    25.83|  6.05    17.05           4.57    28.93  |  7.07      21.37
6.05    27.14|  7.05    16.67           7.07    33.68  |  9.07      19.72
7.05    27.74|  8.05    16.41           8.07    33.69  |  10.07     19.97
8.05    27.62|  9.05    16.54           10.07   30.04  |
10.05   27.74|  10.05   15.90
                11.05   15.77

*****************************Flowfield Surveys*********************************

Alpha = 20 degrees, X = 5.5 cm

Y, cm    M         P/Pinf    U/Uinf    TT/TTinf
0.000    0.000     10.539    0.000     0.350
0.053    2.768     10.539    0.763     0.881
0.096    2.800     10.539    0.778     0.907
0.145    2.878     10.539    0.797     0.931
0.195    2.983     10.539    0.812     0.939
0.290    3.266     10.539    0.851     0.968
0.395    3.701     10.120    0.895     0.992
0.495    3.980      9.760    0.914     0.998
0.590    4.043      9.461    0.918     1.000
0.790    7.050      1.000    1.004     1.006
0.990    7.050      1.000    1.004     1.006
1.175    7.050      1.000    1.003     1.004
1.360    7.050      1.000    1.003     1.004

Alpha = 20 degrees, X = 10.3 cm

Y, cm    M         P/Pinf    U/Uinf    TT/TTinf
0.000    0.000     11.976    0.000     0.350
0.055    2.250     11.976    0.718     0.938
0.100    2.859     11.976    0.806     0.955
0.140    3.107     11.976    0.835     0.963
0.185    3.157     11.976    0.840     0.965
0.270    3.253     11.976    0.856     0.980
0.360    3.336     11.976    0.865     0.986
0.450    3.417     11.976    0.875     0.994
0.650    3.605     11.976    0.892     1.000
0.850    3.763     11.976    0.902     1.000
1.050    3.835     11.976    0.904     0.995
1.200    4.089      9.581    0.916     0.989
1.420    7.052      1.000    1.001     1.001
1.620    7.052      1.000    1.001     1.001

Alpha = 20 degrees, X = 15.5 cm

Y, cm    M         P/Pinf    U/Uinf    TT/TTinf
0.000    0.000     12.335    0.000     0.350
0.065    2.533     12.335    0.735     0.881
0.083    2.747     12.335    0.772     0.906
0.100    2.997     12.335    0.810     0.933
0.138    3.121     12.335    0.832     0.954
0.169    3.168     12.335    0.844     0.972
0.198    3.216     12.335    0.852     0.980
0.250    3.286     12.335    0.862     0.988
0.300    3.354     12.335    0.873     0.999
0.400    3.431     12.335    0.880     1.002
0.520    3.486     12.335    0.884     1.001
0.660    3.540     12.335    0.887     1.000
0.710    3.566     12.335    0.889     1.000
0.800    3.613     12.335    0.892     1.000
0.900    3.676     12.335    0.897     1.000
1.000    3.737     12.335    0.901     1.000
1.100    3.777     12.335    0.903     1.000
1.200    3.777     12.335    0.903     1.000

**********************End of File********************
