Path: ACPro/Airbreathing
% Model of the Pratt & Whitney F135 Engine. The afterburner temperature was scaled to produce the correct thrust with reheat. The mass flow was set to produce the correct thrust without reheat. -------------------------------------------------------------------------- References: [1] www.f-16.net/f-16_forum_viewtopic-t-6295.html [2] www.f135engine.com/proven-tech/engine_chacter.shtml [3] www.turbokart.com/about_f135.htm --------------------------------------------------------------------------
ACPro: ACEngine/MachFromMassFlowParameter ACPro: ACEngine/MachFromPR ACPro: ACEngine/MassFlowParameterR ACPro: ACEngine/RamRecovery ACPro: ACEngine/TempRatioFromMachAndGamma ACPro: ACEngine/WriteEngineData ACPro: ACProData/EngineData ACPro: Airbreathing/EngineExample ACPro: Airbreathing/EngineTable ACPro: Airbreathing/MixedFlowTurbofan ACPro: Airbreathing/Ramjet AerospaceUtils: AeroData/AtmData AerospaceUtils: AtmosphericCalculations/AtmGamma Common: Atmosphere/RFromCPAndGamma Common: Atmosphere/StdAtm 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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