Wall-Pressure Measurements in a Mach 3 Shock-Wave Turbulent Boundary Layer Interaction at a DNS Accessible Reynolds Number

  • Matthew Ringuette, Alexander Smits
  • June 2007, American Institute of Aeronautics and Astronautics (AIAA)
  • DOI: 10.2514/6.2007-4113

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http://dx.doi.org/10.2514/6.2007-4113

The following have contributed to this page: Professor Alexander J Smits