Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge

DOI10.1134/S0965542516060051zbMath1381.76143OpenAlexW2470614748MaRDI QIDQ317226

M. F. Engulatova, S. V. Matyash, V. V. Vlasenko, A. A. Babulin, S. V. Mikhailov, S. M. Bosnyakov

Publication date: 30 September 2016

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0965542516060051

zbMATH Keywords

supersonic flowboundary layer separationcompression wedgeturbulence modelvalidation of models

Mathematics Subject Classification ID

Turbulent boundary layers (76F40) Supersonic flows (76J20)

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Uses Software

• Spalart-Allmaras
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Cites Work

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• Turbulence model assessment for shock wave/turbulent boundary-layer interaction in transonic and supersonic flows.
• Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction

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