TempRatioFromMachAndGamma:

Path: ACPro/ACEngine

% Computes the total temperature ratio from Mach number and gamma.
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   Form:
   tR = TempRatioFromMachAndGamma( cP, gamma )
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   ------
   Inputs
   ------
   m          (1,n)   Specific heat
   gamma      (1,1)   Gamma

   -------
   Outputs
   -------
   tR         (1,n)   Temperature ratio

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   Reference: Mattingly, "Elements of Gas Turbine Propulsion,"
              McGraw-Hill, 1996.
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Children:

Common: Graphics/Plot2D

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