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