Free stream noise and transition measurements in a Mach 3.5 pilot quiet tunnel
- 10 January 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Effects of Wind Tunnel Disturbances on Boundary-Layer Transition with Emphasis on Radiated Noise: A ReviewPublished by Defense Technical Information Center (DTIC) ,1980
- A new technique for reducing test section noise in supersonic wind tunnelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Development of a High Reynolds Number Quiet Tunnel for Transition ResearchAIAA Journal, 1975
- Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer TransitionAIAA Journal, 1975
- A cascade connected electrode scheme for MHD applications.AIAA Journal, 1971
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969