Upstream influence in conically symmetric flow
- 1 June 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (6) , 967-969
- https://doi.org/10.2514/3.9019
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Upstream influence in sharp fin-induced shock wave turbulent boundary-layer interactionAIAA Journal, 1983
- Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression CornersAIAA Journal, 1982
- Computation of three-dimensional turbulent separated flows at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979