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SUPPORT SITE |
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Path: ACPro/ACUtils
-------------------------------------------------------------------------- Computes the form factor for a wing. The drag on a lifting surface is k cF S where S is the wetted area and cF is the skin friction coefficient. Type FormFactorWing for demo. Since version 2014.1 -------------------------------------------------------------------------- Form: k = FormFactorWing( m, t, lambda ) -------------------------------------------------------------------------- ------ Inputs ------ m (1,:) Mach number t (1,:) Thickness ratio t/c lambda (1,1) Sweep angle ------- Outputs ------- k (1,:) Form factor -------------------------------------------------------------------------- Reference: http://adg.stanford.edu/aa241/drag/lsformfactor.html --------------------------------------------------------------------------
Common: Graphics/Plot2D
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