The effects of streamline curvature and pressure gradient on the behavior of turbulent boundary layers in supersonic flow

Douglas R. Smith, Alexander J. Smits

Research output: Contribution to conferencePaperpeer-review

9 Scopus citations

Abstract

Turbulence measurements in distorted supersonic flows are reviewed in the interest of elucidating the effects of curvature, pressure gradients and shockwaves on the boundary layer turbulence structure.

Original languageEnglish (US)
StatePublished - 1994
EventAIAA Fluid Dynamics Conference, 1994 - Colorado Springs, United States
Duration: Jun 20 1994Jun 23 1994

Other

OtherAIAA Fluid Dynamics Conference, 1994
CountryUnited States
CityColorado Springs
Period6/20/946/23/94

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Engineering (miscellaneous)

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