Path: ACPro/ACPerformance
% Computes takeoff distance.
Type TakeoffDistance for a demo.
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Form:
sLO = TakeoffDistance( m, vLO, t, cL, cD0, muR, hB, d, rho )
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Inputs
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m (1,1) Mass (kg)
vLO (1,1) Lift off velocity (m/s)
cL (1,1) Lift coefficient
cD0 (1,1) Drag coefficient
muR (1,1) Rolling resistance
hB (1,1) Altitude/wing span
d (.) Drag data structure
rho (1,1) Atmospheric density (kg/m^3)
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Outputs
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sLO (1,:) Takeoff distance (m)
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Reference: Anderson, J. D., "Introduction to Flight 3rd Edition,",
McGraw-Hill 1989, pp 318-324.
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