Hypersonic viscous shock layer on sweptback wings of infinite span at different angles of attack

DOI10.1007/BF01051666zbMath0435.76040OpenAlexW1992790617MaRDI QIDQ1140489

È. A. Gershbeĭn, I. G. Brykina

Publication date: 1979

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01051666

zbMATH Keywords

successive approximationhypersonicRankine-Hugoniot relationsviscous shock layerinfinite spanslip and discontinuity of temperaturesweptback wings

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (3)

Investigation on the flow past wings of infinite span with a blunt leading edge in the vorticity interaction regime ⋮ Investigation of hypersonic flow of rarefied gas past wings of infinite span ⋮ Extremal problems of heat transfer to three-dimensional bodies at hypersonic speeds

Cites Work

• Integration of hypersonic viscous shock layer equations by a successive approximation method
• Numerical solution of the hypersonic viscous shock-layer equations

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