Effects of Mach number on upstream influence in sharp fin-induced shock wave turbulent boundary layer interaction
- 9 January 1984
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- 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
- Upstream influence scaling of sharp fin-induced shock wave turbulent boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Three-Dimensional Shock Wave-Turbulent Boundary Layer Interactions at Mach 6Published by Defense Technical Information Center (DTIC) ,1975