Path: ACPro/ACProAerodynamics
% Hypersonic coefficient of pressure. Type CPHypersonic for a demo. -------------------------------------------------------------------------- Form: cP = CPHypersonic( m, gamma ) -------------------------------------------------------------------------- ------ Inputs ------ m (1,:) Freestream Mach number gamma (1,1) Ratio of specific heats (Default = 1.4) ------- Outputs ------- cP (1,:) Pressure coefficient --------------------------------------------------------------------------
AC: Aero/RayleighPitotTube Common: Graphics/Plot2D
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