Path: ACPro/Airbreathing
% Jet engine model producing zero thrust and specific fuel consumption.
The default data structure has the afterburner off. The default
fuel is kerosene.
Type TurbojetNoThrust for a demo.
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Form:
[pT7,pR,pRM] = TurbojetNoThrust( m, d, p )
d = TurbojetNoThrust;
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Inputs
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m (1,:) Mach number
d (1,1) Data structure for engine
.gamma (1,1) Specific heat ratio of air
.tT4 (1,1) Temperature at station 4
.piC (1,1) Compressor pressure ratio
p (1,1) Standard atmosphere
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Outputs
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p7 (1,:) Exit pressure
pR (1,:) pT7/p0
pRM (1,:) Max of compressor or ram
t7 (1,:) Exit temperature
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Reference: Kerrebrock, J.L, "Aircraft Engines and Gas Turbines", MIT
Press, 1992, pp. 36-39
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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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