Turbulence Models: Data from Other Experiments: Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers

Description

Shock Wave / Turbulent Boundary Layer Flows at High Mach Numbers. This web page provides data from experiments that may be useful for the validation of turbulence models. This resource is expected to grow gradually over time. All data herein arepublicly available.

Resources

Name Format Description Link
33 Turbulent-SWTBL-paper.pdf http://www.cubrc.org/_iassets/docs/Turbulent-SWTBL-paper.pdf

Tags

  • layer
  • experiment
  • shockwave
  • validation
  • boundary
  • turbulence
  • models
  • mach

Topics

Categories