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SUPPORT SITE |
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Path: Propulsion/Gas
% Computes the area ratio from Mach Number. Type AreaRatioFromMach for a demo. Since version 8. -------------------------------------------------------------------------- Form: M = AreaRatioFromMach( aR, gamma ) -------------------------------------------------------------------------- ------ Inputs ------ M (1,:) Mach number gamma (1,1) Ratio of specific heats ------- Outputs ------- aR (1,:) Area ratio Exit Area/Throat Area --------------------------------------------------------------------------
Common: Graphics/Plot2D
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