Experimental Analysis and Modeling of Limit Cycles in a Dynamic Wind-Tunnel Rig
Author:
Affiliation:
1. University of Bristol, Bristol, England BS8 1TR, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3158
Reference31 articles.
1. Future fighter technologies
2. A new concept for aircraft dynamic stability testing
3. Development of a Pendulum Support Rig Dynamic Wind Tunnel Apparatus
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