Development of a High Reynolds Number Quiet Tunnel for Transition Research
- 1 March 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (3) , 300-306
- https://doi.org/10.2514/3.49695
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Structure of turbulenceJournal of Sound and Vibration, 1973
- Transition and Hot-wire Measurements in Hypersonic Helium FlowAIAA Journal, 1972
- Influence of measured freestream disturbances on hypersonic boundary-layer transitionAIAA Journal, 1970
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- Effects of freestream disturbances on boundary-layer transition.AIAA Journal, 1968
- Effects of freestream turbulence on boundary- layer transition.AIAA Journal, 1967
- The fluctuating pressure field in a supersonic turbulent boundary layerJournal of Fluid Mechanics, 1963
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961
- Reflection, Transmission, and Amplification of Sound by a Moving MediumThe Journal of the Acoustical Society of America, 1957
- Reflection and Transmission of Sound by a Moving MediumThe Journal of the Acoustical Society of America, 1955