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Path: ACPro/Airbreathing
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A simple jet engine model.
Specific Fuel Consumption is constant in this model.
Thrust varies with altitude and Mach number.
Type JetEngine for a demo.
Since version 2014.1
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Form:
[t, i] = JetEngine( m, d, q )
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Inputs
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m (n,1) Mach number
d (1,1) Data structure for engine
.tStatic (1,1) Static thrust
.kM (1,1) Mach number coefficient, thrust
.kI (1,1) Mach number coefficient, impulse
.iSp0 (1,1) Specific Impulse at Mach = 0
q (1,1) Standard atmosphere
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Outputs
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t (1,1) Thrust
i (1,1) Specific Impulse
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Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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