Supersonic and hypersonic quiet tunnel technology at NASA Langley
- 6 July 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 17 references indexed in Scilit:
- Experiments on the stability of supersonic laminar boundary layersJournal of Fluid Mechanics, 1990
- Transition Research in Low-Disturbance High-Speed Wind TunnelsPublished by Springer Nature ,1990
- Aerothermodynamics and Transition in High-Speed Wind Tunnels at NASA LangleyAnnual Review of Fluid Mechanics, 1990
- Boundary-layer transition on a cone and flat plate at Mach 3.5AIAA Journal, 1989
- Effects of Nozzle Design Parameters on the Extent of Quiet Test Flow at Mach 3.5Published by Springer Nature ,1985
- Wind tunnel noise reduction at Mach 5 with a rod-wall sound shieldAIAA Journal, 1983
- The aerodynamic design of blower tunnels with wide-angle diffusersProgress in Aerospace Sciences, 1979
- Fluctuating Disturbances in a Mach 5 Wind TunnelAIAA Journal, 1977
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- On Transition Experiments at Moderate Supersonic SpeedsJournal of the Aeronautical Sciences, 1957