TempRatioFromPressure:

Path: ACPro/ACEngine

% Computes temperature ratio
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   Form:
   tau = TempRatioFromPressure( pi, eta, gamma )
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   ------
   Inputs
   ------
   pi         (1,n)   Pressure ratio
   eta        (1,n)   Efficiency
   gamma      (1,n)   Gamma

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

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

Children:

Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

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