Incipient Separation of a Supersonic, Turbulent Boundary Layer, Including Effects of Heat Transfer
- 1 July 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (7), 915-922
- https://doi.org/10.2514/3.50245
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Shock wave-turbulent boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Experimental and theoretical investigations of temperature distributions in supersonic boundary layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Turbulent boundary-layer separation in front of a forward-facing step.AIAA Journal, 1967
- Velocity profiles in turbulent compressible boundary layers.AIAA Journal, 1966