Comparison of gas-dynamic models for hypersonic flow past bodies

DOI10.1016/0021-8928(92)90130-ZzbMath0788.76055OpenAlexW2095900857MaRDI QIDQ1315569

V. G. Shcherbak, V. S. Shchelin, S. V. Zhluktov, Sergey V. Utyuzhnikov

Publication date: 22 March 1994

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(92)90130-z

zbMATH Keywords

Navier-Stokes equationscritical pointheat fluxthin viscous shock layerBuranchemically non-equilibrium flowscomplete viscous shock layerlocally self- similar approximationsSpace Shuttle

Mathematics Subject Classification ID

Classical flows, reactions, etc. in chemistry (92E20) Reaction effects in flows (76V05) Hypersonic flows (76K05)

Cites Work

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• A comparison of the models of a thin and a complete viscous shock layer in the problem of the supersonic flow of a viscous gas past blunt cones
• Merged stagnation shock layer of nonequilibrium dissociating gas.
• Numerical solution of the hypersonic viscous shock-layer equations

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