A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock Wave
- 1 November 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (11), 1578-1579
- https://doi.org/10.2514/3.50637
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Hypersonic viscous interaction on slender conesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary LayerAeronautical Quarterly, 1966
- Shock-wave and boundary-layer phenomena near a flat surfaceProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1947