Transonic Shock-Boundary-Layer Interactions in Cryogenic Wind Tunnels
- 1 April 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 16 (4) , 284-287
- https://doi.org/10.2514/3.58519
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Theoretical Investigations of Real Gas Effects in Cryogenic Wind TunnelsAIAA Journal, 1978
- Analytical Theory of Transonic Normal Shock-Turbulent Boundary-Layer InteractionAIAA Journal, 1976
- The prediction of separation of the turbulent boundary layerJournal of Fluid Mechanics, 1959
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953