WettedArea:

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
   ------
   type       (1,:) 'wing' 'fuselage' 'nacelle'
   d          (1,1)  Data structure
                     .d    (1,1)  Diameter
                     .s    (1,1)  Wing area
                     .l    (1,1)  Length
   -------
   Outputs
   -------
   sW         (1,:)  Wetted area (m^2)

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