Path: ACPro/Airbreathing
% Generate engine data from a table.
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Form:
[thrust, sFC] = EngineDataFromTable( m, h, d )
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Inputs
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m (1,:) Mach Number
h (1,:) Altitude (m)
d (1,1) Data structure with thrust and sFC data
.m (1,n) Mach number
.h (1,m) Altitude (m)
.thrust (m,n) Thrust (N)
.sFC (m,n) Specific fuel consumption (kg/N-s)
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Outputs
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t (m,n) Thrust (N)
sFC (m,n) Thrust specific fuel consumption (kg/N-s)
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ACPro: ACProData/EngineData 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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