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Experimental and Numerical Study of Unsteadiness in Boundary Layer / Shock Wave Interaction

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Turbulence and Interactions

Abstract

The unsteady flowfield induced by an interaction between an impinging shock wave and a turbulent boundary layer is analysed by means of both Large-Eddy simulations and experiments relying on PIV and wall pressure measurements. A simple kinematic model is derived from these analyses and demonstrates a good ability to reproduce the main unsteady features found in the data.

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© 2010 Springer-Verlag Berlin Heidelberg

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Larchevêque, L., Dupont, P., de Martel, E., Garnier, E., Debiève, J.F. (2010). Experimental and Numerical Study of Unsteadiness in Boundary Layer / Shock Wave Interaction. In: Deville, M., Lê, TH., Sagaut, P. (eds) Turbulence and Interactions. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 110. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-14139-3_32

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  • DOI: https://doi.org/10.1007/978-3-642-14139-3_32

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-14138-6

  • Online ISBN: 978-3-642-14139-3

  • eBook Packages: EngineeringEngineering (R0)

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