FormDragCoeff:

Path: ACPro/ACProAerodynamics

% Computes form drag including wave drag.

   Type FormDragCoeff for a demo.
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   Form:
   cF = FormDragCoeff( d, machNo, altitude, p )
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   ------
   Inputs
   ------
   d            (.)   Aircraft parameters
                         .length         (1,1) Representative length (m)
                         .thickness      (1,1) Thickness ratio
                         .zetaTrans      (1,1) Transonic damping factor
                         .formDragCoeff	(1,1) Form drag merging coefficient          
   machNo      (1,:)  Mach number
   p            (.)   Standard atmosphere structure

   -------
   Outputs
   -------
   cF          (1,:)  Form drag coefficient

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   See also: PrandtlGlauertCorrection, SkinFrictionCoeff
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   Reference: Miller, R. "16.751 Class Notes," MIT, 1977.
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Children:

ACPro: ACProAerodynamics/CDSkinFriction
ACPro: ACProAerodynamics/PrandtlGlauertCorrection
AerospaceUtils: AeroData/AtmData
Common: Atmosphere/StdAtm
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Analysis/Logistic

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