Development of the NASA-Ames Low-Disturbance Supersonic Wind Tunnel for transition studies at Mach 1.6
- 10 January 1994
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Turbulence reduction by screensJournal of Fluid Mechanics, 1988
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961
- Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind TunnelsJournal of the Aeronautical Sciences, 1954