Turbulence in a Shock-Wave Boundary-Layer Interaction
- 1 July 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (7) , 884-889
- https://doi.org/10.2514/3.60464
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Laser Velocimeter and Hot-wire Anemometer Comparison in a Supersonic Boundary LayerAIAA Journal, 1975
- Turbulent Boundary-La yer Shear Stress Distributions for Compressible Adverse Pressure Gradient FlowAIAA Journal, 1974
- Sidewall Boundary-Layer Influence on Shock Wave/Turbulent Boundary-Layer InteractionsAIAA Journal, 1973
- Insensitivity of single particle time domain measurements to laser velocimeter 'Doppler ambiguity.'AIAA Journal, 1973
- Turbulence measurements in a compressible boundary layer subjected to a shock-wave-induced adverse pressure gradientPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Laser Doppler velocity measurements in a supersonic flow without artificial seedingPhysics Letters A, 1972
- A Laser Velocimeter for Reynolds Stress and Other Turbulence MeasurementsAIAA Journal, 1972
- Shock-wave reflection from a turbulent boundary layer with mass bleed.Journal of Aircraft, 1968
- Turbulence in Supersonic FlowJournal of the Aeronautical Sciences, 1953
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950