On the theory of a three-dimensional, viscous hypersonic shock layer in the neighbourhood of the plane of symmetry

DOI10.1016/0021-8928(84)90060-1zbMath0587.76109OpenAlexW2059331959MaRDI QIDQ1072861

S. A. Yunitskiĭ, È. A. Gershbeĭn

Publication date: 1985

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(84)90060-1

zbMATH Keywords

asymptotic analysisnumerical solutionhypersonic viscous shock layerperipheral pressure gradientthree-dimensional flow past a blunt body

Mathematics Subject Classification ID

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

Cites Work

• Unnamed Item
• Numerical investigation of the hypersonic viscous shock layer on wings of infinite span at angles of attack and slip
• Investigation of a three-dimensional hypersonic viscous shock layer in the stagnation point neighborhood in the presence of injection or suction
• Three-dimensional laminar boundary layer on a permeable surface in the neighborhood of a symmetry plane
• Theory of the hypersonic viscous shock layer at high Reynolds numbers and intensive injection of foreign gases
• Calculation of the three-dimensional supersonic flow of a viscous and heat-conducting gas past blunt bodies

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