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Path: ACPro/Airbreathing
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Models a turboramjet.
Uses Ramjet and JetEngine. An earlier version used a table lookup. It
matches the ramjet thrust and turbofan thrust at machTransition.
Type TurboRamjet for a demo.
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Form:
[t, iSp] = TurboRamjet( m, d, p )
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Inputs
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m (1,1) Mach number
d (.) 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 (.) Standard atmosphere struct
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Outputs
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t (1,1) Thrust (N)
iSp (1,1) Specific Impulse (sec)
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ACPro: Airbreathing/JetEngine ACPro: Airbreathing/RamjetKerrebrock Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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