Bluntness and incidence effects in hypersonic flows with large separated regions

DOI10.1017/JFM.2022.605OpenAlexW4291605931MaRDI QIDQ5096602

Amna Khraibut, S. L. Gai

Publication date: 18 August 2022

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2022.605

zbMATH Keywords

hypersonic flowboundary layer separationcompressible boundary layers

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

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• Temperature factor effect on the structure of the separated flow within a supersonic gas stream
• Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow
• Laminar hypersonic leading edge separation – a numerical study
• Hypersonic viscous interaction on curved surfaces
• THE BLUNT-LEADING-EDGE PROBLEM IN HYPERSONIC FLOW
• The formation of a blast wave by a very intense explosion I. Theoretical discussion
• Cylindrical Shock Waves Produced by Instantaneous Energy Release

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