An Experimental Study of Hypersonic Cavity Flow
- 1 May 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 19 (3) , 195-196
- https://doi.org/10.2514/3.62235
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Separation of a supersonic turbulent boundary layer by a forward facing stepPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971