Three-dimensional thin viscous shock layer in the absence of planes of symmetry in the flow

DOI10.1007/BF01075162zbMath0691.76075OpenAlexW2022691435MaRDI QIDQ583026

A. I. Borodin, S. V. Peĭgin

Publication date: 1989

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

Full work available at URL: https://doi.org/10.1007/bf01075162

zbMATH Keywords

high supersonic speedsthin viscous shock layer modelviscous homogeneous gas flow

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05)

Cites Work

• Investigation of a three-dimensional hypersonic viscous shock layer on blunt bodies around which flow occurs at angles of attack and slippage
• Investigation of stationary flow of viscous gas in a thin three- dimensional shock layer
• Three-dimensional laminar boundary layer on a permeable surface in the neighborhood of a symmetry plane
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