Upstream influence in sharp fin-induced shock wave turbulent boundary-layer interaction
- 1 January 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (1) , 143-145
- https://doi.org/10.2514/3.8041
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Upstream influence scaling of 2D and 3D shock/turbulent boundary layer interactions at compression cornersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Incipient separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Sweepback Effects in Turbulent Boundary-Layer Shock-Wave InteractionJournal of the Aerospace Sciences, 1960
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953