Separation of a Supersonic Turbulent Boundary Layer
- 1 June 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (6) , 414-430
- https://doi.org/10.2514/8.3358
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause SeparationJournal of the Aeronautical Sciences, 1953
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- Shock-wave and boundary-layer phenomena near a flat surfaceProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1947