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SUPPORT SITE |
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Path: ACPro/ACEngine
% Computes the jet engine efficiency for an engine. -------------------------------------------------------------------------- Form: [etaO, etaT, etaP] = JetEngineEfficiency( f, hPR, v0, fOverMDotA, v9, units, v19, alpha ) -------------------------------------------------------------------------- ------ Inputs ------ f (1,1) Fuel/air ratio hPR (1,1) Fuel heating value v0 (1,:) Velocity fOverMDotA (1,:) Specific thrust v9 (1,:) Exit velocity units (1,:) 'eng' or 'mks' v19 (1,:) Exit velocity second exhaust alpha (1,1) Bypass ratio ------- Outputs ------- etaO (1,:) Total efficiency etaT (1,:) Thermal efficiency etaP (1,:) Propulsive efficiency --------------------------------------------------------------------------
Common: Graphics/Plot2D
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