Structure of a mach 8 turbulent boundary layer

Mark L. Baurngartner, Peter J. Erbland, Michael R. Etz, Azer Yalin, Brian K. Muzas, Alexander J. Smits, Walter R. Lempert, Richard B. Miles

Research output: Contribution to conferencePaperpeer-review

2 Scopus citations

Abstract

Preliminary measurements of the effects of increasing Mach number on the structure of turbulent boundary layers are presented. The data were obtained using a Mach 2.5 pilot tunnel facility and a new Mach 8 boundary layer facility. The principal diagnostic technique was planar Rayleigh scattering. The results shed some light on the effects of Mach and Reynolds number on outer layer intermittency.

Original languageEnglish (US)
StatePublished - 1997
Event35th Aerospace Sciences Meeting and Exhibit, 1997 - Reno, United States
Duration: Jan 6 1997Jan 9 1997

Other

Other35th Aerospace Sciences Meeting and Exhibit, 1997
CountryUnited States
CityReno
Period1/6/971/9/97

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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