Mean flow and noise measurements in a Mach 3.5 pilot quiet tunnel
- 22 March 1982
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- 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
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969