Path: ACPro/ACPerformance
% Computes the required roll distance and liftoff velocity.
To see a demo, run with no inputs: [s,v,def] = Takeoff;
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Form:
[sTotal, vLiftoff, def] = Takeoff( d, altitude )
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Inputs
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d (1,1) See "ConcordeProperties.m"
altitude (1,1) Altitude (m)
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Outputs
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sTotal (1,1) Ground roll (m)
vLiftoff (1,1) Liftoff velocity (m/s)
def {12,3} Data structure definition
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Reference: Mair, W. A. and D. L. Birdsall, "Aircraft Performance,"
Cambridge, p. 139.
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ACPro: ACPerformance/VStall 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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