Evolution of large-scale structures in a supersonic turbulent boundary layer

S. Cogne, J. Forway, W. Lempert, R. B. Miles, Alexander Smits

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

11 Scopus citations

Abstract

The evolution of the large-scale density structure in a turbulent boundary layer at Mach 2.9 was studied using double-pulsed Rayleigh scattering. Pairs of images of the instantaneous density field ware obtained with time delays ranging from 12 μsec to 60 μsec, and they were used to determine qualitatively the changes in the structures as they move downstream. Instantaneous convection velocities were also measured.

Original languageEnglish (US)
Title of host publicationTransitional and Turbulent Compressible Flows - 1993
PublisherPubl by ASME
Pages229-237
Number of pages9
Volume151
ISBN (Print)0791809595
StatePublished - Jan 1 1993
EventFluids Engineering Conference - Washington, DC, USA
Duration: Jun 20 1993Jun 24 1993

Other

OtherFluids Engineering Conference
CityWashington, DC, USA
Period6/20/936/24/93

All Science Journal Classification (ASJC) codes

  • Engineering(all)

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  • Cite this

    Cogne, S., Forway, J., Lempert, W., Miles, R. B., & Smits, A. (1993). Evolution of large-scale structures in a supersonic turbulent boundary layer. In Transitional and Turbulent Compressible Flows - 1993 (Vol. 151, pp. 229-237). Publ by ASME.