MachFromPressureRatio:

Path: AC/Aero

% Computes the Mach number from pressure ratio.
--------------------------------------------------------------------------
   Form:
   m = MachFromPressureRatio( gamma, pR, tol )
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   ------
   Inputs
   ------
   gamma          (1,1)       Ratio of specific heats
   pR             (1,:)       Pressure ratio
   tol            (1,1)       tolerance

   -------
   Outputs
   -------
   m              (1,:)       Mach number
--------------------------------------------------------------------------

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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