CD Nozzle. Axial Mach Number. Pexit = 0.89 psi (Subsonic Flow).
x (in)
M
    1
Analytic Solution        
  51
   0.0000000E+00  0.2305986    
   0.2000000      0.2311824    
   0.4000000      0.2329429    
   0.6000000      0.2359077    
   0.8000000      0.2401235    
    1.000000      0.2456567    
    1.200000      0.2525952    
    1.400000      0.2610493    
    1.600000      0.2711545    
    1.800000      0.2830723    
    2.000000      0.2969925    
    2.200000      0.3131352    
    2.400000      0.3317496    
    2.600000      0.3531143    
    2.800000      0.3775311    
    3.000000      0.4053157    
    3.200000      0.4367796    
    3.400000      0.4721986    
    3.600000      0.5117609    
    3.800000      0.5554809    
    4.000000      0.6030496    
    4.200000      0.6535671    
    4.400000      0.7050224    
    4.600000      0.7532675    
    4.800000      0.7904066    
    5.000000      0.8049845    
    5.200000      0.7999743    
    5.400000      0.7858996    
    5.600000      0.7650277    
    5.800000      0.7398368    
    6.000000      0.7123653    
    6.200000      0.6840839    
    6.400000      0.6559903    
    6.600000      0.6287439    
    6.800000      0.6027672    
    7.000000      0.5783231    
    7.200000      0.5555651    
    7.400000      0.5345717    
    7.600000      0.5153693    
    7.800000      0.4979494    
    8.000000      0.4822819    
    8.200000      0.4683219    
    8.400000      0.4560181    
    8.600000      0.4453161    
    8.800000      0.4361631    
    9.000000      0.4285094    
    9.200000      0.4223110    
    9.400000      0.4175303    
    9.600000      0.4141374    
    9.800000      0.4121103    
    10.00000      0.4114360