Path: ACPro/Airbreathing
-------------------------------------------------------------------------- Mixed flow turbofan engine performance profile for p, h and v. A mixed flow turbofan is one in which the fan and core streams mix in the same nozzle. This model supports afterburning. This is the same code as in JetEnginePeformance but designed for a single input. The outputs are the same as RamjetH2. Only mks units are supported in this function. Type MixedFlowTurbofanProfile for a demo This function calls MixedFlowTurbofan 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 ); Since version 5. -------------------------------------------------------------------------- Form: [t, tSFC] = MixedFlowTurbofanProfile( ref, p, h, v ) -------------------------------------------------------------------------- ------ Inputs ------ ref (1,1) Reference conditions See MixedFlowTurbofan.m p (1,1) Throttle settings .afterburner (1,:) Afterburner on == 1 .throttleRatio (1,:) Throttle ratio .tT4 (1,:) Combustor temperature (K) .tT7 (1,:) Afterburner temperature (K) h (1,:) Altitude v (1,:) Velocity ------- Outputs ------- t (1,:) Thrust (N/m^2) tSFC (1,:) Thrust specific fuel consumption (kg/N/s) -------------------------------------------------------------------------- Reference: Mattingly, "Elements of Gas Turbine Propulsion," McGraw-Hill, 1996, 2005, p.551 --------------------------------------------------------------------------
ACPro: Airbreathing/EngineExample ACPro: Airbreathing/MixedFlowTurbofan Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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