Path: ACPro/ACPerformance
% Sizes a wing for dynamic pull up. Since version 4 (ACT). -------------------------------------------------------------------------- Form: s = WingSizingForPullUp( pullUp, m, h, cLAlpha, alpha, thrust, mass, sweep ) -------------------------------------------------------------------------- ------ Inputs ------ pullUp (1,1) Pull up (g) m (1,1) Mach number cLAlpha (1,1) Lift coefficient for alpha (1/rad) thrust (1,1) Engine thrust (N) alpha (1,1) Angle of attack (rad) mass (1,1) Mass (kg) sweep (1,1) Sweep angle (rad) ------- Outputs ------- s (1,1) Wing area (m^2) --------------------------------------------------------------------------
Common: Atmosphere/StdAtm
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