Path: ACPro/RDE
% RDE model producing zero thrust and specific fuel consumption.
The default data structure has the afterburner off. The default
fuel is hydrogen.
Type RDE for a demo.
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Form:
[t, iSp, tS] = RDE( m, d, p )
d = RDE;
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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 the fuel
.mDotO2 (1,1) O2 mass flow (kg/s)
.tT4 (1,1) Temperature at station 4
.aInlet (1,1) Inlet area (m^2)
.mDiffuser (1,1) Diffuser
.piC (1,1) Compressor pressure ratio
p (1,1) Standard atmosphere
ACPro: ACEngine/AerodynamicShock ACPro: ACEngine/MachAcrossShock ACPro: ACEngine/StreamlineShockAngle ACPro: Airbreathing/TurbojetNoThrust AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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