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- W1976770147 abstract "Results from linearized wing theory are employed to study the planform optimization for supersonic wings with subsonic leading edges. Momentum flux theory in a characteristic control surface is used to minimize the drag of a supersonic nonslender delta-like wing with subsonic leading edges and a supersonic trailing edge producing a given lift. In this paper a method is presented to construct the so-called Hayes-cuts of the optimum lift distribution. The method is applied to wings with two types of trailing edges. The results indicate that in general the optimum lift distribution for minimum total drag differs from the elliptical distribution obtained to produce minimum wave drag. Since the shape of the subsonic leading edges need not be specified in the present method, nonuniqueness of the optimum planform seems to exist. b c" @default.
- W1976770147 created "2016-06-24" @default.
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- W1976770147 date "1986-04-01" @default.
- W1976770147 modified "2023-10-16" @default.
- W1976770147 title "Optimum supersonic wings with subsonic leading edges" @default.
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- W1976770147 doi "https://doi.org/10.2514/3.45307" @default.
- W1976770147 hasPublicationYear "1986" @default.
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