Laser Velocimeter and Hot-wire Anemometer Comparison in a Supersonic Boundary Layer
- 1 April 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (4) , 512-515
- https://doi.org/10.2514/3.49739
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Turbulence Measurements in a Mach 2.9 Boundary Layer Using Laser VelocimetryAIAA Journal, 1974
- 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
- Fluctuation Measurements in a Supersonic Turbulent Boundary LayerPhysics of Fluids, 1959