CD Nozzle. Axial Mach Number. Pexit = 0.16 psi (Supersonic Flow).
x (in)
M
    1
Analytic Solution        
  51
   0.0000000E+00  0.2395428    
   0.2000000      0.2401525    
   0.4000000      0.2419912    
   0.6000000      0.2450882    
   0.8000000      0.2494931    
    1.000000      0.2552769    
    1.200000      0.2625332    
    1.400000      0.2713805    
    1.600000      0.2819642    
    1.800000      0.2944594    
    2.000000      0.3090735    
    2.200000      0.3260485    
    2.400000      0.3456640    
    2.600000      0.3682380    
    2.800000      0.3941266    
    3.000000      0.4237210    
    3.200000      0.4574398    
    3.400000      0.4957166    
    3.600000      0.5389794    
    3.800000      0.5876219    
    4.000000      0.6419665    
    4.200000      0.7022194    
    4.400000      0.7684249    
    4.600000      0.8404243    
    4.800000      0.9178230    
    5.000000      0.9997698    
    5.200000       1.049278    
    5.400000       1.099540    
    5.600000       1.150450    
    5.800000       1.201643    
    6.000000       1.252754    
    6.200000       1.303419    
    6.400000       1.353288    
    6.600000       1.402030    
    6.800000       1.449334    
    7.000000       1.494914    
    7.200000       1.538515    
    7.400000       1.579906    
    7.600000       1.618885    
    7.800000       1.655275    
    8.000000       1.688924    
    8.200000       1.719701    
    8.400000       1.747494    
    8.600000       1.772210    
    8.800000       1.793771    
    9.000000       1.812114    
    9.200000       1.827187    
    9.400000       1.838950    
    9.600000       1.847373    
    9.800000       1.852435    
    10.00000       1.854124