Turbulence measurements in hypersonic shock-wave boundary-layer interaction flows
- 1 May 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (5) , 568-575
- https://doi.org/10.2514/3.7127
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Turbulence stress measurements in a nonadiabatic hypersonic boundarylayerAIAA Journal, 1975
- Mean and fluctuating flow measurements of a fully-developed, non-adiabatic, hypersonic boundary layerJournal of Fluid Mechanics, 1975
- Turbulence in a Shock-Wave Boundary-Layer InteractionAIAA Journal, 1975
- Numerical Study of Separated Turbulent FlowsAIAA Journal, 1975
- New Diagnostic Technique for the Study of Turbulent Boundary-Layer SeparationAIAA Journal, 1974
- Numerical solution of the interaction of a strong shock wave with a hypersonic turbulent boundary layerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974