CD Nozzle. Axial Static Pressure. Pexit = 0.16 psi (Supersonic Flow).
x (in)
p (psi)
    1
Analytic Solution        
  51
   0.0000000E+00  0.9608492    
   0.2000000      0.9606546    
   0.4000000      0.9600656    
   0.6000000      0.9590641    
   0.8000000      0.9576204    
    1.000000      0.9556900    
    1.200000      0.9532128    
    1.400000      0.9501103    
    1.600000      0.9462820    
    1.800000      0.9416005    
    2.000000      0.9359082    
    2.200000      0.9290103    
    2.400000      0.9206690    
    2.600000      0.9105966    
    2.800000      0.8984537    
    3.000000      0.8838449    
    3.200000      0.8663263    
    3.400000      0.8454205    
    3.600000      0.8206479    
    3.800000      0.7915765    
    4.000000      0.7578946    
    4.200000      0.7194992    
    4.400000      0.6765875    
    4.600000      0.6297246    
    4.800000      0.5798628    
    5.000000      0.5286468    
    5.200000      0.4983042    
    5.400000      0.4686222    
    5.600000      0.4395775    
    5.800000      0.4114938    
    6.000000      0.3846425    
    6.200000      0.3592383    
    6.400000      0.3354384    
    6.600000      0.3133435    
    6.800000      0.2930009    
    7.000000      0.2744158    
    7.200000      0.2575561    
    7.400000      0.2423654    
    7.600000      0.2287681    
    7.800000      0.2166777    
    8.000000      0.2060031    
    8.200000      0.1966533    
    8.400000      0.1885405    
    8.600000      0.1815824    
    8.800000      0.1757052    
    9.000000      0.1708438    
    9.200000      0.1669425    
    9.400000      0.1639555    
    9.600000      0.1618473    
    9.800000      0.1605926    
    10.00000      0.1601759