Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds Numbers
- 1 January 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (1) , 50-56
- https://doi.org/10.2514/3.61331
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Incipient separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Supersonic, Turbulent Boundary-Layer SeparationAIAA Journal, 1974
- Sidewall Boundary-Layer Influence on Shock Wave/Turbulent Boundary-Layer InteractionsAIAA Journal, 1973
- Separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Incipient separation pressure rise for a Mach 3.8 turbulent boundarylayer.AIAA Journal, 1973
- Shock Wave/Turbulent Boundary-Layer Interactions in Rectangular ChannelsAIAA Journal, 1973
- Incipient Separation of a Supersonic, Turbulent Boundary Layer, Including Effects of Heat TransferAIAA Journal, 1972
- Shock wave-turbulent boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Reflexion of an oblique shock wave by a turbulent boundary layerJournal of Fluid Mechanics, 1970