Shock-induced leading-edge separation in hypersonic flows

DOI10.1017/JFM.2022.619OpenAlexW4292590069MaRDI QIDQ5097361

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Publication date: 23 August 2022

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

Full work available at URL: https://doi.org/10.1017/jfm.2022.619

zbMATH Keywords

hypersonic flowboundary layer separationgas dynamics

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

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• Shock wave reflection phenomena
• Some physical aspects of shock wave/boundary layer interactions
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• Separation length in high-enthalpy shock/boundary-layer interaction
• Shock Wave-Boundary-Layer Interactions
• Direct simulation Monte Carlo computations and experiments on leading-edge separation in rarefied hypersonic flow
• Effects of upstream boundary layer on the unsteadiness of shock-induced separation
• Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactions
• On the length scales of hypersonic shock-induced large separation bubbles near leading edges
• Laminar hypersonic leading edge separation – a numerical study
• Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct numerical simulation data
• Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions
• Self-induced separation

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