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SUPPORT SITE |
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Path: Propulsion/Gas
% Computes isentropic expansion. Type IsentropicExpansion for a demo. Since version 8. -------------------------------------------------------------------------- Form: [pR, rhoR, tR] = IsentropicExpansion( M, gamma ) -------------------------------------------------------------------------- ------ Inputs ------ M (1,:) Mach number gamma (1,1) Ratio of specific heats ------- Outputs ------- pR (1,1) p0/p rhoR (1,1) rho0/rho tR (1,1) t0/t --------------------------------------------------------------------------
Common: Graphics/Plot2D
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