Investigation of a three-dimensional hypersonic viscous shock layer on blunt bodies around which flow occurs at angles of attack and slippage

DOI10.1016/0021-8928(86)90062-6zbMath0618.76067OpenAlexW2042193706MaRDI QIDQ1089212

V. G. Krupa, V. S. Shchelin, È. A. Gershbeĭn

Publication date: 1986

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(86)90062-6

zbMATH Keywords

multicomponent diffusioncatalytic surfacewings of infinite spanthree-dimensional hypersonic flowapproximate numerical methodchemical non-equilibrium equationsdissociating non-equilibrium airhypersonic, three-dimensional viscous shock layersmooth blunt bodies

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Hypersonic flows (76K05)

Related Items (1)

Three-dimensional thin viscous shock layer in the absence of planes of symmetry in the flow

Cites Work

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• Numerical investigation of the hypersonic viscous shock layer on wings of infinite span at angles of attack and slip
• Investigation of hypersonic three-dimensional flow past blunt bodies within the framework of the parabolized Navier-Stokes equations
• Calculation of metric coefficients for streamline coordinates.

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