Numerical solution of a three-dimensional shock wave and turbulent boundary-layer interaction
- 16 January 1978
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Numerical Simulation of Supersonic and Hypersonic Turbulent Compression Corner FlowsAIAA Journal, 1977
- Numerical solutions for supersonic corner flowJournal of Computational Physics, 1975
- A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Numerical solution for the inviscid supersonic flow in the corner formed by two intersecting wedgesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary LayerAeronautical Quarterly, 1966
- Sweepback Effects in Turbulent Boundary-Layer Shock-Wave InteractionJournal of the Aerospace Sciences, 1960