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SUPPORT SITE |
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Path: ACPro/ACEngine
% Ram recovery in an inlet. This computes the loss of pressure due to shocks. It is based on Military Specification 5008B. -------------------------------------------------------------------------- Form: etaR = RamRecovery( machNo ) -------------------------------------------------------------------------- ------ Inputs ------ machNo (1,:) Mach number ------- Outputs ------- etaR (1,:) Ram recovery --------------------------------------------------------------------------
Common: Graphics/Plot2D
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