Mach and reynolds number effects on turbulent boundary layer behavior

Alexander J. Smits

Research output: Contribution to conferencePaper

1 Scopus citations

Abstract

The effects of varying Mach and Reynolds numbers on the behavior of turbulent boundary layers is discussed. The emphasis is on the evaluating the relevance of subsonic experience to the interpretation of supersonic flows.

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

Other

Other33rd Aerospace Sciences Meeting and Exhibit, 1995
CountryUnited States
CityReno
Period1/9/951/12/95

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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    Smits, A. J. (1995). Mach and reynolds number effects on turbulent boundary layer behavior. Paper presented at 33rd Aerospace Sciences Meeting and Exhibit, 1995, Reno, United States. https://doi.org/10.2514/6.1995-578