Calculation of Turbulent Boundary-Layer Shock-Wave Interaction
- 1 November 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (11) , 1592-1594
- https://doi.org/10.2514/3.50646
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Shock Wave/Turbulent Boundary-Layer Interactions in Rectangular ChannelsAIAA Journal, 1973
- A model for inhomogeneous turbulent flowProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1970
- Separation of a Supersonic Turbulent Boundary LayerJournal of the Aeronautical Sciences, 1955