Shock-Wave-Boundary-Layer Interaction Effects on Aerodynamic Heating
- 1 January 1977
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 14 (1) , 25-31
- https://doi.org/10.2514/3.57157
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Aerodynamic heating in gaps in the presence of protuberances and shock wave impingementPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Interference heating due to shock wave impingement on laminar boundary layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Shock wave-turbulent boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transferJournal of Fluid Mechanics, 1964