LiftAndDragJonesSearsHaack:

Path: ACPro/ACProAerodynamics

% Lift and drag using the R.T. Jones, Sears, and Haack model.
 This is for the minimum drag of a supersonic body with fixed 
 lift, span, length, and volume. Either d.h or d.p is needed.

 if cL is not entered it will compute the optimal cL.

 Volume and surface area includes fuselage and wings.

 Type LiftAndDragJonesHaackSears for a demo.

--------------------------------------------------------------------------
   Forms:
   d = LiftAndDragJonesSearsHaack;  % default data structure
   [lift, dragTotal, qCL, cD] = LiftAndDragJonesSearsHaack( m, d )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   m           (1,1) Mach number  
   d            (.)  Data structure
                     .l      (1,1) Aircraft length (m)
                     .h      (1,:) Altitude (m)
                     .p       (.)  Standard Atmosphere struct
                     .b      (1,1) Span (m)
                     .s      (1,1) Surface area (m^2)
                     .v      (1,1) Volume (m^3)
                     .sL     (1,1) Lifting surface  (m^2)
                     .cL     (1,1) Lift coefficient
                     .alpha  (1,1) Angle of attack

   ------
   Outputs
   -------
   lift        (1,1) Lift (N)
   dragTotal   (1,1) Drag (N)
   qCL         (1,1) Dynamic pressure times lift coefficient (N/m^2)
   cD          (1,1) Drag coefficient

--------------------------------------------------------------------------
   Reference: "Applied Aerodynamics: A Digital Textbook", Version 5.0, 
               January 2007, Desktop Aeronautics, Inc.
--------------------------------------------------------------------------
   See also: ConcordeLD, SurfaceAreaEllipsoidRevolution, StdAtm,
   CDSkinFriction
--------------------------------------------------------------------------

Children:

ACPro: ACProAerodynamics/CDSkinFriction
ACPro: ACProAerodynamics/ConcordeLD
ACPro: ACUtils/SurfaceAreaEllipsoidRevolution
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

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