Numerical Simulation of Shock Wave - Turbulent Boundary-Layer Interaction
- 1 October 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (10), 1451-1457
- https://doi.org/10.2514/3.61484
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Numerical solutions of the supersonic, laminar flow over a two-dimensional compression cornerPublished by Springer Nature ,2007
- Evolution of a moderately short turbulent boundary layer in a severe pressure gradientJournal of Fluid Mechanics, 1974
- Supersonic, Turbulent Boundary-Layer SeparationAIAA Journal, 1974
- Turbulence-Model Predictions for Turbulent Boundary LayersAIAA Journal, 1974
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973
- Equilibrium and relaxation in turbulent wakesJournal of Fluid Mechanics, 1972
- Calculation of compressible adiabatic turbulent boundary layersAIAA Journal, 1970
- Interactions between shock waves and turbulent boundary layersProgress in Aerospace Sciences, 1970
- Self-induced separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1969