Flow Stabilization in a Transonic Wind Tunnel with a Second Throat
Author:
Affiliation:
1. Nagoya University, Nagoya 464-8603, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2708
Reference7 articles.
1. Torngren, L., Grunnet, J., Nelson, D., and Kamis, D. “The New FFA T1500 Transonic Wind Tunnel Initial Operation, Calibration and Test Results,” AIAA 90-1420, June 1990.
2. A new facility and technique for two-dimensional aerodynamic testing
3. Experimental evaluation of an injector system for powering a high Reynolds number transonic wind tunnel
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