WingAreaToTaper:

Path: ACPro/ACPerformance

% Generates the taper and trailing edge angle for a wing.

   s and b are for the entire wing (both sides of the fuselage).
   WingAreaToTaper( c, s, b, sweep ), with no outputs,
   will generate a picture of the wing.

   Since version 4 (ACT).
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   Form:
   [f, omegaT] = WingAreaToTaper( c, s, b, sweep )
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   ------
   Inputs
   ------
   c       (1,1) Root chord length (m)
   s       (1,1) Wing area (m^2)
   b       (1,1) Wing span (m)
   sweep	(1,1) Sweep angle (rad)

   -------
   Outputs
   -------
   f       (1,1) Taper
   omegaT  (1,1) Trailing edge angle (rad)

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Children:

Common: Graphics/NewFig
Common: Graphics/TitleS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS

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