Path: ACPro/Airbreathing
% 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
.turbojet (1,1) Turbojet data structure
.aInlet (1,1) Inlet area
p (.) Standard atmosphere struct
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Outputs
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t (1,:) Thrust (N)
iSp (1,:) Specific impulse (s)
tS (1,:) Specific thrust (N/kg/s)
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ACPro: Airbreathing/RamjetKerrebrock ACPro: Airbreathing/Turbojet AerospaceUtils: AeroData/AtmData 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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