Reynolds Stress Measurements in a Hypersonic Boundary Layer
- 1 November 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (11) , 1594-1596
- https://doi.org/10.2514/3.50647
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Shock Wave/Turbulent Boundary-Layer Interactions in Rectangular ChannelsAIAA Journal, 1973
- Hot-wire measurements of hypersonic boundary-layer turbulencePhysics of Fluids, 1973
- Development of a Hot-Wire Anemometer for Hypersonic Turbulent FlowsReview of Scientific Instruments, 1972
- Theory of hot-wire correlation measurements in compressible flow with application to wakesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- 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