Pressure-Gradient Effects on Hypersonic Turbulent Skin-Friction and Boundary-Layer Profiles
- 1 September 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (9) , 1141-1142
- https://doi.org/10.2514/3.50336
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Hypersonic Turbulent Skin-Friction and Boundary-Layer Profiles on Nonadiabatic Flat PlatesAIAA Journal, 1972
- Relationship between temperature and velocity profiles in a turbulent boundary layer along a supersonic nozzle with heat transferAIAA Journal, 1970
- Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental dataAIAA Journal, 1970