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- W637298727 abstract "Exact analytical solutions in terms of induced drag influence coefficients can be attained which define the spanwise loading with minimized induced drag, subject to specified constraint conditions, for any nonplanar wing shape or number of lift plus wing bending moment about a given wing span station. Example applications of the theory are made to a biplane, a wing in ground effect, a cruciform wing, a V-wing, a planar-wing winglet, and linked wingtips in formation flying. For minimal induced drag, the spanwise loading, relative to elliptic, is outboard for the biplane and is inboard for the wing in ground effect and for the planar-wing winglet. A spinoff of the triplane solution provides mathematically exact equations for downwash and sidewash about a planar vorticity sheet having an arbitrary loading distribution." @default.
- W637298727 created "2016-06-24" @default.
- W637298727 creator A5022436415 @default.
- W637298727 date "1979-06-01" @default.
- W637298727 modified "2023-09-27" @default.
- W637298727 title "Minimization theory of induced drag subject to constraint conditions" @default.
- W637298727 hasPublicationYear "1979" @default.
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