Separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbers
- 16 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Incipient separation pressure rise for a Mach 3.8 turbulent boundarylayer.AIAA Journal, 1973
- Shock wave-turbulent boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Boundary layer separation in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Experimental investigations of the compressible turbulent boundary layer at very high reynolds numbersAIAA Journal, 1965