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SUPPORT SITE |
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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: Graphics/Plot2D
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