Path: ACPro/Airbreathing
-------------------------------------------------------------------------- Models a turbofanramjet. Uses Ramjet and Turbofan. An earlier version used a table lookup. It matches the ramjet thrust and turbfan thrust at machTransition. Type Turbofanramjet for a demo. -------------------------------------------------------------------------- Form: [t, sFC] = Turbofanramjet( m, d, p ) -------------------------------------------------------------------------- ------ Inputs ------ m (1,1) Mach number d (1,1) Data structure .machTransition (1,1) Transition to ramjet M .ramjet (1,1) Ramjet data structure .turbofan (1,1) Turbofan data structure .aInlet (1,1) Inlet area p (1,1) Standard atmosphere ------- Outputs ------- t (1,1) Thrust (N) sFC (1,1) Specific Fuel Consumption (kg/N-s) --------------------------------------------------------------------------
ACPro: Airbreathing/Ramjet ACPro: Airbreathing/Turbofan Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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