The Effects of Recessed Lower Surface Shape on the Lift and Drag of Conical Wings at High Incidence and High Mach Number
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SummaryFor lifting re-entry there may be advantages in using wings which give as high a lift coefficient as possible at the design value of the lift/drag ratio. This paper presents the results of an experimental and theoretical study of wings with recessed lower surfaces designed to give high values of CL. The calculations show that a wide range of wing shapes can be found that give values of CL which are much larger than those on a flat wing with the same lift/drag ratio.
2019 ◽
Vol 9
(2)
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pp. 3319-3323
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2020 ◽
pp. 095441002094690
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2014 ◽
Vol 2014
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pp. 1-13
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2006 ◽
Vol 128
(5)
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pp. 931-936
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2021 ◽
Vol 2076
(1)
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pp. 012066
2021 ◽
Vol 2076
(1)
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pp. 012078
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