Wind tunnel noise reduction at Mach 5 with a rod-wall sound shield
- 1 May 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (5) , 643-644
- https://doi.org/10.2514/3.8129
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Fluctuating Disturbances in a Mach 5 Wind TunnelAIAA Journal, 1977
- Development of a High Reynolds Number Quiet Tunnel for Transition ResearchAIAA Journal, 1975
- A comparison of disturbance levels measured in hypersonic tunnels using a hot-wire anemometer and a pitot pressure probePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Hypersonic boundary-layer transition in the presence of wind-tunnel noise.AIAA Journal, 1971
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969