Normal shock boundary layer control with various vortex generator geometries

DOI10.1016/J.COMPFLUID.2011.06.003zbMath1271.76147OpenAlexW1965351958MaRDI QIDQ365485

Mohammad Hasan, M. Dambrine

Publication date: 4 September 2013

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

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S0045793011001915

zbMATH Keywords

flow separationflow controlDiffuserimplicit large eddy simulationsupersonic boundary layer interactionvortex generator

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Turbulent boundary layers (76F40) Control of turbulent flows (76F70)

Related Items (1)

Comparative study of boundary layer control around an ordinary airfoil and a high lift airfoil with secondary blowing

Cites Work

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• An implicit finite-difference algorithm for hyperbolic systems in conservation-law form
• Direct numerical simulation of hypersonic turbulent boundary layers. Part 1. Initialization and comparison with experiments
• On the solution of nonlinear hyperbolic differential equations by finite differences

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