Turbulence Measurement in Transonic Flow
- 1 September 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (9) , 1368-1370
- https://doi.org/10.2514/3.60794
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Artificial Thickening of High Subsonic Mach Number Boundary LayersAIAA Journal, 1976
- Direct measurements at Mach 6 of turbulent skin-friction reduction by injection from single and multiple flush slotsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Multiple slot skin friction reductionJournal of Aircraft, 1975
- Investigation of the three-dimensional turbulent flow downstream of swept slot injection in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Experimental evaluation of an injector system for powering a high Reynolds number transonic wind tunnelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Multiple slot laminar film coolingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Film cooling effectiveness in hypersonic turbulent flowAIAA Journal, 1970
- An experimental investigation of turbulent slot injection at Mach 6AIAA Journal, 1970
- A comparison between film cooling and transpiration cooling systems in high speed flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950