ACThrust:

Path: AC/ACActuator

% Thrust model for a gas turbine engine

--------------------------------------------------------------------------
   Form:
   thrust = ACThrust( idl, mil, max, yH, xM, h, m, p )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   idl           (alt,mach)  Thrust coefficients for idle power
   mil           (alt,mach)  Military power
   max           (alt,mach)  Max Power
   yH            (alt)       Row coefficient values
   xM            (mach)      Columns of matrices
   h                         Altitude
   m                         Mach number
   p                         Power

   -------
   Outputs
   -------
   thrust                    Thrust

--------------------------------------------------------------------------

Children:

Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Analysis/IntExt

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