Structure of a Mach 8 turbulent boundary layer Conference Paper uri icon

abstract

  • 1997 American Institute of Aeronautics and Astronautics, Inc. 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.

name of conference

  • 35th Aerospace Sciences Meeting and Exhibit

published proceedings

  • 35th Aerospace Sciences Meeting and Exhibit

author list (cited authors)

  • Baumgartner, M., Erbland, P., Etz, M., Yalin, A., Muzas, B., Smits, A., ... Miles, R.

publication date

  • January 1, 1997 11:11 AM