Investigation on the flow past wings of infinite span with a blunt leading edge in the vorticity interaction regime

DOI10.1007/BF01050733zbMath0654.76064OpenAlexW2004379282MaRDI QIDQ1108871

A. A. Legostaev, È. A. Gershbeĭn

Publication date: 1987

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

Full work available at URL: https://doi.org/10.1007/bf01050733

zbMATH Keywords

Navier-Stokes equationsasymptotic analysishypersonic flownumerical solutionthin viscous shock layerinviscid boundary layerwings of infinite spanAnalytic solutionsinviscid shock layervorticity interaction

Mathematics Subject Classification ID

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

Cites Work

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• Hypersonic viscous shock layer on sweptback wings of infinite span at different angles of attack
• Local similarity expansions of the boundary- layer equations

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