Supersonic laminar flow on the windward surface of yawed wings of infinite span over a broad range of Reynolds numbers

DOI10.1007/BF01050310zbMath0751.76045OpenAlexW1968328891MaRDI QIDQ1190905

I. V. Vershinin, G. A. Tirskij, Sergey V. Utyuzhnikov

Publication date: 27 September 1992

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

Full work available at URL: https://doi.org/10.1007/bf01050310

zbMATH Keywords

Cauchy problemviscositycompressibilityglobal iteration methodcomplete equations of the viscous shock layerelliptic propertiesmarching coordinate

Mathematics Subject Classification ID

Related Items (1)

Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow

Cites Work

• 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
• Non-Navier Stokes viscous flow computations

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