Path: ACPro/ACProAerodynamics
% Aerodynamic wetted area for different structures.
For wings, fuselages and nacelles.
Mach number and sweep ratio must be entered for wings.
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Form:
sW = WettedArea( type, d )
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Inputs
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type (1,:) 'wing' 'fuselage' 'nacelle'
d (1,1) Data structure
.d (1,1) Diameter
.s (1,1) Wing area
.l (1,1) Length
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Outputs
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sW (1,:) Wetted area (m^2)
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