deprecated
-------------------------------------------------------------------------- Computes the induced drag coefficient. Type SkinFrictionCoeff for a demo. -------------------------------------------------------------------------- Form: kI = kInduced( d, machNo ) -------------------------------------------------------------------------- ------ Inputs ------ d (1,1) Aircraft parameters .oswaldEff (1,1) Oswald efficiency factor (0.9 to 1.0) .aspectRatio (1,1) Aspect ratio for wing (length/mean chord) machNo (1,:) Mach number ------- Outputs ------- kI (1,:) Induced drag coefficient -------------------------------------------------------------------------- Reference: Miller, R. "16.751 Class Notes," MIT, 1977. --------------------------------------------------------------------------
Common: Graphics/Plot2D