Minimal Drag for Wings with Prescribed Lift, Roll Moment and Yaw Moment.
Technical summary rept.,
WISCONSIN UNIV-MADISON MATHEMATICS RESEARCH CENTER
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Let L, R, Y be arbitrary real constants. A wing with fixed span which produces lift L, roll moment R, yaw moment Y and which has minimal induced drag D is wanted. This problem arises in airplane engineering. It is solved by means of Prandtls lifting line theory combined with computation. Author
- Numerical Mathematics
- Fluid Mechanics