Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield

This publication has 12 references indexed in Scilit:

• Prediction of turbulent wall pressure fluctuations in attached boundary layer flow
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1981
• An experimental investigation of the unsteady behavior of blunt fin-induced shock wave turbulent boundary layer interaction
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1981
• Investigation of a Three-Dimensional Shock Wave Separated Turbulent Boundary Layer
  AIAA Journal, 1980
• Comparison of Multiequation Turbulence Models for Several Shock Boundary-Layer Interaction Flows
  AIAA Journal, 1979
• Computation of three-dimensional turbulent separated flows at supersonic speeds
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1979
• Details of a Shock-Separated Turbulent Boundary Layer at a Compression Corner
  AIAA Journal, 1976
• Incipient separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbers
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
• New Diagnostic Technique for the Study of Turbulent Boundary-Layer Separation
  AIAA Journal, 1974
• Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock waves
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1973
• Fluctuating Wall Pressure under a Separated Supersonic Flow
  The Journal of the Acoustical Society of America, 1964