Flutter-Boundary Prediction of a Morphing Wing in the Process of Adaptation
Author:
Affiliation:
1. Nagoya University, Nagoya 465-0012, Japan
2. Meijo University, Nagoya, 468-8502, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051202
Reference36 articles.
1. Theoretical and Experimental Aeroelastic Study for Folding Wing Structures
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