New Technique for Reducing Test Section Noise in Supersonic Wind Tunnels
- 1 January 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (1) , 5-6
- https://doi.org/10.2514/3.50721
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- A new technique for reducing test section noise in supersonic wind tunnelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Fluctuating Disturbances in a Mach 5 Wind TunnelAIAA Journal, 1977
- Nozzle Wall Boundary-Layer Transition and Freestream Disturbances at Mach 5AIAA Journal, 1975
- Development of a High Reynolds Number Quiet Tunnel for Transition ResearchAIAA Journal, 1975
- Hypersonic boundary-layer transition in the presence of wind-tunnel noise.AIAA Journal, 1971
- 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
- The Mach wave field radiated by supersonic turbulent shear flowsJournal of Fluid Mechanics, 1965
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961
- On the generation of sound by supersonic turbulent shear layersJournal of Fluid Mechanics, 1960