TempRatioFromPressure:

Path: ACPro/ACEngine

% Computes temperature ratio
--------------------------------------------------------------------------
   Form:
   tau = TempRatioFromPressure( pi, eta, gamma )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   pi         (1,n)   Pressure ratio
   eta        (1,n)   Efficiency
   gamma      (1,n)   Gamma

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

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

Children:

Common: Graphics/Plot2D

Back to the ACPro Module page