Effect of sudden expansions or compressions on the turbulent boundary layer.
- 1 December 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (12) , 2232-2234
- https://doi.org/10.2514/3.3888
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966