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: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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