A study of shock-wave turbulent boundary layer interaction using laser velocimeter and hot-wire anemometer techniques
- 30 January 1974
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- 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
- Fluctuation Measurements in a Supersonic Turbulent Boundary LayerPhysics of Fluids, 1959
- Turbulence in Supersonic FlowJournal of the Aeronautical Sciences, 1953
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950