Computation of sharp fin and swept compression corner shock/turbulent boundary layer interactions
- 12 June 1989
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Conical similarity of shock/boundary-layer interactions generated byswept and unswept finsAIAA Journal, 1985
- Flowfield scaling in sharp fin-induced shock wave/turbulent boundary-layer interactionAIAA Journal, 1985
- A hybrid explicit-implicit numerical algorithm for the three-dimensional compressible Navier-Stokes equationsAIAA Journal, 1984
- Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression CornersAIAA Journal, 1982
- Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression CornersAIAA Journal, 1980