CDCLHypersonic:

Path: ACPro/ACProAerodynamics

% Hypersonic lift and drag coefficients for a flat plate.

 Includes pressure effects, skin friction and parasitic drag.

 The default Standard Atmosphere is at 1000 m.

 Type CDCLHypersonic for a demo. One demo shows the variation of
 cD and cL with respect to Mach. The other shows the variation with
 respect to angle of attack. This function includes the pressure
 correction with Mach for cP. It also includes skin friction and
 parasitic drag.

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   Form:
   [cD, cL] = CDCLHypersonic( m, alpha, p, l, cParasitic )
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   ------
   Inputs
   ------
   m           (1,:)	  Freestream Mach number
   alpha       (1,:)   Angle of attack (rad)
   p            (.)    Standard atmosphere data structure
   l           (1,1)   Characteristic length
   cParasitic	(1,1)   Parasitic drag

   -------
   Outputs
   -------
   cD          (1,:) 	Drag coefficient
   cL          (1,:) 	Lift coefficient
  
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   See also CPHypersonic, CDSkinFriction
--------------------------------------------------------------------------

Children:

ACPro: ACProAerodynamics/CDSkinFriction
ACPro: ACProAerodynamics/CPHypersonic
AeroUtils: AtmosphericCalculations/AtmGamma
Common: Atmosphere/StdAtm
Common: Graphics/Plot2D

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