An experimental investigation and a numerical prediction of a transonic normal shock wave/turbulent boundary layer interaction
- 7 June 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Experimental investigation of similitude parameters governing transonic shock-boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical Investigation of Turbulence Models for Shock-Separated Boundary-Layer FlowsAIAA Journal, 1978
- Wall Shear in Strongly Retarded and Separated Compressible Turbulent Boundary LayersAIAA Journal, 1974
- Shock wave-turbulent boundary layer interactions in rectangular channelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Use of Coles' universal wake function for compressible turbulent boundary layersJournal of Aircraft, 1970
- Interactions between shock waves and turbulent boundary layersProgress in Aerospace Sciences, 1970
- Step-induced separation of a turbulent boundary layer in incompressible flowJournal of Fluid Mechanics, 1967