Wing:

Path: AerospaceUtils/ComponentModels

% Generates a Wing. The tail points in the z direction.
 You enter the leading and trailing edge locations as a 
 function of z.

 Type Wing for a demo.
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   Form:
   [v, f] = Wing( xLE, xTE, z, lERatio, taper )
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   ------
   Inputs
   ------
   xLE        (1,:) Leading edge position
   xTE        (1,:) Trailing edge position
   z          (1,:) Spanwise position
   lERatio    (1,1) Leading edge x to y ratio
   taper      (1,1) Ratio of root to tip
   tOC        (1,1) Thickness to chord ratio

   -------
   Outputs
   -------
   v          (:,3)  Vertices
   f          (:,3)  Faces

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Children:

Common: ComponentModels/Extrude
Math: Trigonometry/CosD

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