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.
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Form:
[t, sFC] = Turbofanramjet( m, d, p )
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Inputs
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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
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Outputs
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t (1,1) Thrust (N)
sFC (1,1) Specific Fuel Consumption (kg/N-s)
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ACPro: Airbreathing/Ramjet ACPro: Airbreathing/Turbofan AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS
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