Interaction of an oblique shock wave with a turbulent boundary layer.
- 1 September 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (9) , 1792-1793
- https://doi.org/10.2514/3.4871
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Supersonic separated and reattaching laminar flows- i - general theory and application to adiabatic boundary layer-shock wave interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964