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- W2051248643 abstract "A study has been conducted to explore the use of existing aerodynamic techniques to design a new supersonic cruise wing for an existing fighter wind-tunnel model. In addition to the usual wing design constraints of lift, pitching moment, and minimum drag, a ground rule was imposed that the wing had to fit on the existing fuselage. Experimental wind-tunnel results were obtained for a camber design and a reference flat wing. The flat wing was also fitted with leading-edge flaps which approximate the cruise camber design. The experimental results indicate that significant improvements in supersonic cruise capability can be obtained by a new wing designed using existing supersonic aerodynamic techniques." @default.
- W2051248643 created "2016-06-24" @default.
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- W2051248643 date "1979-01-15" @default.
- W2051248643 modified "2023-09-27" @default.
- W2051248643 title "Design study results of a supersonic cruise fighter wing" @default.
- W2051248643 cites W2316516244 @default.
- W2051248643 doi "https://doi.org/10.2514/6.1979-62" @default.
- W2051248643 hasPublicationYear "1979" @default.
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