Wall pressure fluctuations near separation in a Mach 5, sharp fin-induced turbulent interaction
- 7 January 1991
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Inception length to a fully-developed fin-generated shock wave boundary-layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989