Path: ACPro/Airbreathing
% Ramjet jet engine model producing thrust and specific fuel consumption.
Type RamjetKerrebrock for a demo.
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Form:
[t, iSp, tS] = RamjetKerrebrock( m, d, p )
d = RamjetKerrebrock;
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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
.cP (1,1) Specific heat of air
.qR (1,1) Heating value of fuel
.tT4 (1,1) Temperature at station 4
.aInlet (1,1) Inlet area
p (1,1) Standard atmosphere
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Outputs
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t (1,:) Thrust (N)
iSp (1,:) Specific impulse (s)
tS (1,:) Specific thrust
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Reference: Kerrebrock, J.
http://web.mit.edu/16.unified/www/FALL/thermodynamics/notes/node85.html
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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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