FuelFromRange:

Path: ACPro/ACPerformance

% Computes the fuel as a function of range.

   Type FuelFromRange for a demo using the Scimitar engine at Mach 5.
--------------------------------------------------------------------------
   Form:
   mF = FuelFromRange( mD, lOverD, r, v, sFC )
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   ------
   Inputs
   ------
   mD          (1,1)  Dry mass (kg)
   lOverD      (1,1)  Lift to drag ratio
   r           (1,:)  Range (km)
   v           (1,1)  Velocity (m/s)
   sFC         (1,1)  Specific Fuel Consumption (kg/N-s)

   -------
   Outputs
   -------
   range       (1,:)  Range (km)

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   Reference: http://web.mit.edu/16.unified/www/FALL/
              thermodynamics/notes/node98.html
--------------------------------------------------------------------------

Children:

ACPro: ACProAerodynamics/LiftToDragFromMach
ACPro: Airbreathing/Scimitar
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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