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