Supersonic, Turbulent Boundary-Layer Separation
- 1 June 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (6) , 794-797
- https://doi.org/10.2514/3.49352
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Turbulent boundary layer flow separation measurements using holographic interferometryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Incipient Separation of a Supersonic, Turbulent Boundary Layer, Including Effects of Heat TransferAIAA Journal, 1972
- An experimental study of turbulent separating and reattaching flows at a high Mach numberJournal of Fluid Mechanics, 1972
- Shock wave-turbulent boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971