Fabrication and testing of the Purdue Mach-6 quiet-flow Ludwieg tube
Author:
Affiliation:
1. Purdue Univ., West Lafayette, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-295
Reference69 articles.
1. Fluctuating Disturbances in a Mach 5 Wind Tunnel
2. 90-1391, AIAA, June 1990.
3. PI I. Beckwith, T. Creel, F. Chen, and J. Kendall. Freestream noise and transition measurements on a cone in a Mach-3.5 pilot low-disturbance tunnel. Technical Report NASA-TP-2180, NASA Technical Paper, 1983.
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