Turbulence stress measurements in a nonadiabatic hypersonic boundarylayer
- 1 December 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (12), 1607-1613
- https://doi.org/10.2514/3.7038
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- A study of shock-wave turbulent boundary layer interaction using laser velocimeter and hot-wire anemometer techniquesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Turbulence measurements in an equilibrium hypersonic boundary layerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Reynolds Stress Measurements in a Hypersonic Boundary LayerAIAA Journal, 1973
- Turbulent properties of a compressible boundary layer.AIAA Journal, 1972
- Statistical Characteristics of Reynolds Stress in a Turbulent Boundary LayerPhysics of Fluids, 1972