Turbulence in supersonic and hypersonic boundary layers

Alexander J. Smits, M. Pino Martin

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

1 Scopus citations

Abstract

Abstract: A summary is given of the behavior of turbulent boundary layers in supersonic and hypersonic flow where the effects of compressibility have a direct influence on the turbulence. Experimental and DNS results are presented and compared.

Original languageEnglish (US)
Title of host publicationIUTAM Symposium on One Hundred Years of Boundary Layer Research
Subtitle of host publicationProceedings of the IUTAM Symposium Held at DLR-Gottingen, Germany, August 12-14, 2004
Pages221-230
Number of pages10
DOIs
StatePublished - Dec 1 2006

Publication series

NameSolid Mechanics and its Applications
Volume129
ISSN (Print)0925-0042

All Science Journal Classification (ASJC) codes

  • Materials Science(all)
  • Mechanics of Materials
  • Mechanical Engineering

Keywords

  • Boundary layer
  • Hypersonic
  • Shocklets
  • Shocks
  • Supersonic
  • Turbulence

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  • Cite this

    Smits, A. J., & Martin, M. P. (2006). Turbulence in supersonic and hypersonic boundary layers. In IUTAM Symposium on One Hundred Years of Boundary Layer Research: Proceedings of the IUTAM Symposium Held at DLR-Gottingen, Germany, August 12-14, 2004 (pp. 221-230). (Solid Mechanics and its Applications; Vol. 129). https://doi.org/10.1007/978-1-4020-4150-1-21