Numerical assessment of correlations for shock wave boundary layer interaction

DOI10.1016/J.COMPFLUID.2013.11.011zbMath1391.76286OpenAlexW2062498213MaRDI QIDQ1641178

Bibin John, Vinayak Kulkarni

Publication date: 19 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2013.11.011

zbMATH Keywords

hypersonicscorrelations for laminar flowsshock boundary layer interactions

Mathematics Subject Classification ID

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

Related Items (2)

A Sharp-Interface Immersed Boundary Method for High-Speed Compressible Flows ⋮ Effect of leading edge bluntness on the interaction of ramp induced shock wave with laminar boundary layer at hypersonic speed

Cites Work

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• Convergence to steady state solutions of the Euler equations on unstructured grids with limiters
• Analysis of hypersonic compression ramp laminar flows under sharp leading edge conditions
• Separation length in high-enthalpy shock/boundary-layer interaction
• The hypersonic laminar boundary layer near sharp compression and expansion corners
• Validation procedure for the analysis of shock-wave/boundary-layer interaction problems
• Self-induced separation

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