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SUPPORT SITE |
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Path: ACPro/ACPerformance
% Aerodynamic form factor.
For wings, fuselages and nacelles.
Mach number and sweep ratio must be entered for wings.
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Form:
k = AeroFormFactor( type, r )
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Inputs
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type (1,:) 'wing' 'fuselage' 'nacelle'
m (1,1) Mach number (for wings)
d .r (1,1) Ratio: t/c for wing l/d for others
.lambda (1,1) Quarter chord sweep
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Outputs
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k (1,:) Form factor
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