Path: ACPro/Airbreathing
% Mixed flow turbofan engine performance. A mixed flow turbofan is one in which the fan and core streams mix in the same nozzle. This model supports afterburning. The outputs are the same as RamjetH2. Only mks units are supported in this function. Type MixedFlowTurbofan for a demo. This function employs a reference model and its outputs are deviations from the reference model. Type ref = MixedFlowTurbofan to get the reference data structure along with the demo. Note that only ref.h0 need be entered for the atmospheric parameters. The following are computed from the Standard Atmosphere and AtmGamma as follows. q = StdAtm( ref.h0 ); ref.p0 = q.pressure; ref.a0 = q.speedOfSound; ref.t0 = q.temperature; ref.rho = q.density; ref.gammaC = AtmGamma( ref.t0 ); -------------------------------------------------------------------------- Form: [t, tSFC, f, M, thR] = MixedFlowTurbofan( action, varargin ) -------------------------------------------------------------------------- ------ Inputs ------ action (1,:) 'initialize' 'update' if action == struct t (.) Default data if action == 'initialize' ref (1,1) Reference conditions See JetEngineDefinitions.m if action == 'update' h (1,1) Altitude v (1,1) Velocity p (1,1) Throttle settings .afterburner (1,1) Afterburner on == 1 .throttleRatio (1,1) Throttle ratio .tT4 (1,1) Combustor temperature (K) .tT7 (1,1) Afterburner temperature (K) ------- Outputs ------- if action == 'initialize' ref (1,1) Full set of reference conditions if action == 'update' t (1,1) Thrust (N/m^2) tSFC (1,:) Thrust specific fuel consumption f (1,1) Fuel air ratio structure .f (1,1) Fuel air ratio .fAB (1,1) Afterburner fuel air ratio .fO (1,1) Mixed fuel air ratio M (1,:) Mach number thR (1,:) Thrust to mass flow ratio -------------------------------------------------------------------------- Reference: Mattingly, "Elements of Gas Turbine Propulsion," McGraw-Hill, 1996, 2005, p.551 --------------------------------------------------------------------------
ACPro: ACEngine/MachFromMassFlowParameter ACPro: ACEngine/MachFromPR ACPro: ACEngine/MassFlowParameterR ACPro: ACEngine/RamRecovery ACPro: ACEngine/TempRatioFromMachAndGamma ACPro: Airbreathing/EngineExample 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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