A new hypersonic boundary layer facility

M. L. Baumgartner, A. J. Smitst, T. Nau, C. W. Rowley

Research output: Contribution to conferencePaperpeer-review


A new Mach 8 blowdown facility for the study of transition, turbulence, and shock wave/boundary layer interactions at high Mach numbers is being built. This paper describes the design and construction of the facility.

Original languageEnglish (US)
StatePublished - 1995
Event33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States
Duration: Jan 9 1995Jan 12 1995


Other33rd Aerospace Sciences Meeting and Exhibit, 1995
Country/TerritoryUnited States

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering


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