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The Shock-Wave/Turbulent Boundary-Layer Interaction on Curved Surface at Transonic Speed

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Turbulent Shear-Layer/Shock-Wave Interactions

Part of the book series: International Union of Theoretical and Applied Mechanics ((MANUTECH))

Summary

Detailed experimental measurements have been made of the shockwave/ turbulent boundary-layer interaction on curved surface at transonic speed. The flow field is calculated by a wide range of numerical methods including two boundary-layer methods, two shock/boundary-layer interaction methods and one Euler-solver inviscid method.

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References

  1. Baker C.J. (1980) The prediction of boundary layer development through a normal shock wave turbulent boundary-layer interaction, Cambridge University, CUED/A-AERO/TR.10 (1980)

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Author information

Authors and Affiliations

  1. Engineering Department, Cambridge University, UK

    X. Liu & L. C. Squire

Authors
  1. X. Liu
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  2. L. C. Squire
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Editor information

Editors and Affiliations

  1. Direction de L’Aérodynamique, ONERA, B.P. 72, 29. Av. de la Division Leclerc, F-92322, Châtillon Cedex, France

    J. Délery

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© 1986 Springer-Verlag Berlin, Heidelberg

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Liu, X., Squire, L.C. (1986). The Shock-Wave/Turbulent Boundary-Layer Interaction on Curved Surface at Transonic Speed. In: Délery, J. (eds) Turbulent Shear-Layer/Shock-Wave Interactions. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-82770-9_8

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  • DOI: https://doi.org/10.1007/978-3-642-82770-9_8

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-82772-3

  • Online ISBN: 978-3-642-82770-9

  • eBook Packages: Springer Book Archive

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