Leading-Edge Separation of Laminar Boundary Layers in Supersonic Flow
- 1 December 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 28 (12) , 957-961
- https://doi.org/10.2514/8.9265
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- An experimental investigation of the interaction between shock waves and boundary layersProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1954