Flowfield scaling in sharp fin-induced shock wave/turbulent boundary-layer interaction
- 1 February 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (2) , 201-206
- https://doi.org/10.2514/3.8895
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- A hybrid explicit-implicit numerical algorithm for the three-dimensional compressible Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
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- Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression CornersAIAA Journal, 1982
- Upstream influence scaling of sharp fin-induced shock wave turbulent boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Computation of three-dimensional turbulent separated flows at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979