BEHAVIOUR OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER UNDER INCIPIENT SEPARATION CONDITIONS.

K. C. Muck, A. J. Smits

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Abstract

This paper presents an experimental study of a turbulent boundary-layer/shock-wave interaction. The interaction was generated by a two-dimensional compression corner, and the flow was on the point of separating. Measurements were made using both normal and inclined hot wires, and the data include measurements of the longitudinal mass-flow fluctuation intensity and the mass-weighted Reynolds shear stress. Refs.

Original languageEnglish (US)
Title of host publicationUnknown Host Publication Title
PublisherSpringer Verlag
Pages235-245
Number of pages11
ISBN (Print)3540137440, 9783540137443
DOIs
StatePublished - 1985

All Science Journal Classification (ASJC) codes

  • Engineering(all)

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    Muck, K. C., & Smits, A. J. (1985). BEHAVIOUR OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER UNDER INCIPIENT SEPARATION CONDITIONS. In Unknown Host Publication Title (pp. 235-245). Springer Verlag. https://doi.org/10.1007/978-3-642-69996-2_19