A wing with the maximum lift/drag ratio at supersonic velocity

DOI10.1016/0021-8928(66)90071-2zbMath0168.23202OpenAlexW2312417923MaRDI QIDQ5553986

G. I. Maikapar

Publication date: 1966

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(66)90071-2

zbMATH Keywords

fluid mechanics

Related Items (6)

Optimum lifting body shapes in hypersonic flow at high angles of attack ⋮ The shapes of bodies with maximum lift-to-drag ratio in supersonic flow ⋮ The mode of attached compression shock at edges of a V-shaped wing ⋮ Waveriders of complicated shape ⋮ Improving the aerodynamic performance of small-aspect-ratio wings at hypersonic speeds ⋮ Aerodynamic characteristics of \(V\)-shaped wings with shock waves detached from leading edges at hypersonic speeds

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