On hypersonic flow past of a lift airfoil

DOI10.1016/0021-8928(83)90062-XzbMath0573.76056OpenAlexW2069115574MaRDI QIDQ1062856

O. S. Ryzhov, E. D. Terent'ev

Publication date: 1984

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(83)90062-x

zbMATH Keywords

Laplace equationperfect gasthermal conductivityexternal flowcylindrical coordinate systemviscosity coefficientsasymptotic solutions of the Navier-Stokes equationsCauchy problem for Euler's equationsconstant ratio of specific heatslaminar traillarge distance from a lifting airfoil of finite dimensionslocal vortex vectorlocal vortex zonesRankine-Hugoniot shock conditionsself-similar variablespecific enthalpysubtrailsurrounding shock wave

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Cites Work

• The laminar hypersonic trail downstream of a lift airfoil
• The structure of shock waves in hypersonic flows
• On space hypersonic flows

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