Compressible Flow Calculator

Input Data

        M =              Ratio of specific heats (g) =             Turning Angle (d) = deg

Isentropic Flow

     P0/P =            T0/T =            r0/r =

     P/P0 =            T/T0 =            r/r0 =

  A/A*  =            M1* =

Shock Jump Relations

     P2/P1 =           T2/T1 =          r2/ r1 =

  P02/P01 =         P02/P1 =              M2  =         

     m= deg       n(M)= deg      Shock Angle (q) = deg             

Note:  if turning angle is greater than maximum possible, shock jump relations are for detached, normal shock!

Copyright Tom Gally 2003
Contact: gallyt@erau.edu