Path: ACPro/ACProAerodynamics
-------------------------------------------------------------------------- Computes the L/D ratio from Mach number. This is an empirical relationship developed by Dietrich Kuchemann for predicting the L/D ratio at high Mach (M>1). Type LiftToDragFromMach for a demo. Since version 5. -------------------------------------------------------------------------- Form: lOverD = LiftToDragFromMach( m ) -------------------------------------------------------------------------- ------ Inputs ------ m (1,:) Mach number ------- Outputs ------- lOverD (1,:) L/D ratio -------------------------------------------------------------------------- Reference: John D. Anderson, Jr. "Introduction to Flight", 3rd Edition, McGraw-Hill, 1989. Ch. 10, Hypersonic Vehicles, Eq. 10.15, p. 552 --------------------------------------------------------------------------
Common: Graphics/Plot2D
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