Experimental and Theoretical Study of Gust Response for High-Aspect-Ratio Wing
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1691
Reference11 articles.
1. Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow
2. LIMIT-CYCLE OSCILLATIONS IN HIGH-ASPECT-RATIO WINGS
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