Pressure Rise Required for Separation in Interaction Between Turbulent Boundary Layer and Shock Wave
- 1 December 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (12), 858-860
- https://doi.org/10.2514/8.2887
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- III. The interaction between an oblique shock-wave and a turbulent boundary-layerJournal of Computers in Education, 1951
- Shock-wave and boundary-layer phenomena near a flat surfaceProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1947
- On the Reaction of an Elastic Wing to Vertical GustsJournal of the Aeronautical Sciences, 1941
- Airfoil Theory for Non-Uniform MotionJournal of the Aeronautical Sciences, 1938