An experimental investigation of the Reynolds number effect on a normal shock wave-turbulent boundary layer interaction on a curved wall

This publication has 11 references indexed in Scilit:

• Separation structures produced by normal shock-wave/turbulent boundary-layer interaction in a narrow wind tunnel
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1987
• Transonic shock-wave/turbulent boundary-layer interactions in a circular duct
  AIAA Journal, 1985
• Topological structures of three-dimensional vortex flow separation
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1983
• Experimental investigation of turbulence properties in transonic shock/boundary-layer interactions
  AIAA Journal, 1983
• An experimental investigation and a numerical prediction of a transonic normal shock wave/turbulent boundary layer interaction
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1982
• Transonic Shock Wave - Boundary Layer Interactions.
  Published by Defense Technical Information Center (DTIC) ,1980
• Experimental investigation of similitude parameters governing transonic shock-boundary layer interactions
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1980
• Comparison of Multiequation Turbulence Models for Several Shock Boundary-Layer Interaction Flows
  AIAA Journal, 1979
• A normal shock-wave turbulent boundary-layer interaction at transonic speeds
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1976
• Reynolds number effects on the shock wave - Turbulent boundary layerinteraction at transonic speeds
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1973