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Path: AC/ACActuator
% Thrust model for a gas turbine engine Since version 2 (ACT) -------------------------------------------------------------------------- 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: Graphics/Plot2D Math: Analysis/IntExt
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