*********************Coleman Mach 9 Compression Corner Data********************

Minf = 9.22
Re_inf/cm = 4.7E+05
ReL = 26.2E+06
Tstagnation = 1070 deg K
Tinf = 64.5 deg K
Twall = 295 deg K
Twall/Trecovery = 0.28
Pinf/Pstagnation = 0.45
Delta = 0.72 cm

   Alpha = 15 degrees                     
   Qinf = 6.07 W/cm**2                    

   X, cm   Pw/Pinf |   X, cm    Qw/Qinf   
   -1.9    0.99    |   -4.2     1.06      
   -1.4    1.0     |   -3.65    1.11      
   -0.9    1.02    |   -3.1     0.96      
   -0.4    1.04    |   -2.6     0.96      
   0.3     3.47    |   -2.05    1.03      
   0.84    4.7     |   -1.65    0.86      
   1.1     5.86    |   -1.35    0.94      
   1.6     7.4     |   -1.1     1.0       
   1.87    7.4     |   -0.85    0.92      
   2.4     10.4    |   -0.6     0.8       
   2.67    11.5    |   0.35     3.16      
   3.2     11.8    |   0.6      2.91      
   3.45    11.9    |   0.85     3.78      
   4.24    11.9    |   1.35     4.27      
                       1.6      4.68      
                       1.85     5.42      
                       2.1      6.3       
                       2.35     6.67      
                       2.6      6.65      
                       3.15     7.69      
                       3.4      8.05      
                       3.9      8.5       
                       4.4      8.44      
                       4.9      8.61      
                       6.7      8.65      
                       7.2      8.04      

    Alpha = 30 degrees
    Qinf = 6.17 W/cm**2

    X, cm   Pw/Pinf |   X, cm    Qw/Qinf
    -1.65   1.05    |   -5.7     0.99
    -.14    1.05    |   -4.85    0.96
    -1.14   1.06    |   -4.4     1.09
    -0.89   1.08    |   -4.2     0.94
    -0.64   1.11    |   -3.65    1.0
    -0.38   1.28    |   -3.1     0.94
    0.25    7.45    |   -2.6     0.95
    0.56    15.8    |   -2.35    0.87
    0.84    24.2    |   -2.05    0.95
    1.15    31.8    |   -1.9     0.95
    1.73    34.2    |   -1.35    0.93
    2.0     36.0    |   -1.1     0.94
    2.61    36.2    |   -0.85    0.96
    2.89    36.4    |   -0.6     0.81
    3.5     36.4    |   -0.35    0.77
    3.8     36.0    |   0.25     5.8
    4.65    36.0    |   0.45     6.7
    5.6     36.4    |   0.7      8.6
                        1.0      10.6
                        1.2      13.1
                        1.5      15.6
                        1.7      15.7
                        2.05     17.7
                        2.24     18.1
                        2.5      19.6
                        2.7      18.6
                        3.0      18.5
                        3.3      17.7
                        3.6      17.5
                        3.7      17.0
                        4.1      15.9
                        4.25     16.6
                        4.7      17.1
                        5.3      16.3
                        6.1      14.8
                        6.6      15.4

   Alpha = 34 degrees
   Qinf = 6.29 W/cm**2

   X, cm   Pw/Pinf |   X, cm    Qw/Qinf
   -2.67   1.02    |   -7.6     -0.95
   -2.4    1.02    |   -6.65    1.03 
   -2.16   1.33    |   -5.7     0.98 
   -1.9    1.9     |   -5.15    1.03 
   -1.65   2.55    |   -4.65    1.03 
   -1.4    3.36    |   -4.2     1.0  
   -1.15   4.56    |   -3.9     0.89 
   -0.88   4.98    |   -3.65    0.93 
   -0.64   4.75    |   -3.35    0.77 
   -0.38   5.31    |   -3.1     0.9  
   0.25    6.97    |   -2.85    1.74 
   0.56    9.9     |   -2.6     1.35 
   0.87    12.6    |   -2.35    1.79 
   1.17    19.1    |   -2.05    2.24 
   1.47    26.9    |   -1.9     2.16 
   1.78    53.0    |   -1.65    2.08 
   2.08    62.3    |   -1.35    1.8  
   2.4     49.3    |   -1.1     1.67 
   3.0     51.0    |   -0.85    1.71 
   3.63    46.8    |   -0.6     1.52 
   3.94    46.2    |   -0.35    2.14 
                       0.25     3.22 
                       0.45     2.85 
                       0.7      5.85 
                       1.0      6.04 
                       1.2      9.91 
                       1.5      11.1 
                       1.7      14.3 
                       2.05     18.0 
                       2.24     21.1 
                       2.5      26.4 
                       2.7      27.6 
                       3.0      29.3 
                       3.3      24.3 
                       3.6      23.9 
                       3.7      21.8 
                       4.25     20.3 
                       4.7      21.4 
                       5.3      21.4 
                       7.1      19.2 

    Alpha = 38 degrees
    Qinf = 6.56 W/cm**2

    X, cm   Pw/Pinf |   X, cm    Qw/Qinf
    -4.7    1.03    |   -11.2    0.9
    -4.45   1.11    |   -10.2    0.9
    -4.2    1.24    |   -7.6     1.0
    -3.93   1.46    |   -7.1     1.02
    -3.68   1.44    |   -6.65    0.95
    -3.43   2.54    |   -6.1     1.1
    -3.18   2.67    |   -5.7     0.86
    -2.92   4.45    |   -5.45    1.22
    -2.66   5.25    |   -5.15    1.86
    -2.41   5.7     |   -4.85    1.8
    -2.16   5.7     |   -4.65    2.22
    -1.9    5.7     |   -4.4     2.4
    -1.4    6.2     |   -4.2     2.05
    -1.14   6.2     |   -3.9     2.24
    -0.89   6.2     |   -3.65    2.15
    -0.64   6.6     |   -3.35    2.18
    -0.38   6.7     |   -2.85    1.92
    0.25    7.2     |   -2.6     1.82
    0.5     8.5     |   -2.35    1.65
    0.75    11.4    |   -2.05    1.93
    1.0     15.1    |   -1.9     1.83
    1.25    20.8    |   -1.65    1.7
    1.5     29.0    |   -1.35    1.89
    1.75    49.0    |   -1.1     1.88
    2.0     59.0    |   -0.85    1.98
    2.25    75.5    |   -0.6     1.94
    2.54    86.0    |   0.25     2.86
    2.8     93.0    |   0.45     3.25
    3.05    77.5    |   0.70     4.16
    3.3     69.5    |   1.0      4.82
    3.81    59.0    |   1.2      6.47
    4.06    61.5    |   1.6      10.0
    4.32    59.6    |   1.7      10.6
    4.57    57.5    |   2.24     16.4
    5.33    59.0    |   2.5      18.7
                        2.7      23.3
                        3.0      29.0
                        3.15     27.2
                        3.3      31.3
                        3.6      31.0
                        3.7      28.5
                        4.25     25.1
                        4.4      23.7
                        4.65     25.2
                        4.7      23.7
                        4.9      24.3
                        5.2      22.9
                        5.3      23.4
                        5.45     22.5
                        5.75     22.4
                        6.7      22.7

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