Crossing shock wave-turbulent boundary layer interactions
- 7 January 1991
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
- A hybrid explicit-implicit numerical algorithm for the three-dimensional compressible Navier-Stokes equationsAIAA Journal, 1984
- Flow visualization methods for separated three-dimensional shock wave/turbulent boundary-layer interactionsAIAA Journal, 1983
- Blunt fin-induced shock wave/turbulent boundary-layer interactionAIAA Journal, 1982
- Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression CornersAIAA Journal, 1982
- An experimental study of the interaction between a glancing shock wave and a turbulent boundary layerJournal of Fluid Mechanics, 1982
- Numerical Solution of Three-Dimensional Shock Wave and Turbulent Boundary-Layer InteractionAIAA Journal, 1978
- On the Structure of Three-Dimensional Shock-Induced Separated Flow RegionsAIAA Journal, 1976
- Accurate Difference Methods for Nonlinear Two-Point Boundary Value ProblemsSIAM Journal on Numerical Analysis, 1974
- A modified wall wake velocity profile for turbulent compressible boundary layers.Journal of Aircraft, 1973
- The prediction of laminarization with a two-equation model of turbulenceInternational Journal of Heat and Mass Transfer, 1972