Aeroelastic Response of a Z-Shaped Folding Wing During the Morphing Process
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061138
Reference26 articles.
1. Flutter suppression and stability analysis for a variable-span wing via morphing technology
2. Morphing Aircraft Systems: Historical Perspectives and Future Challenges
3. Vibration and Flutter Characteristics of a Folding Wing
4. Modeling and Flight Control of Large-Scale Morphing Aircraft
5. Aeroelastic deployable wing simulation considering rotation hinge joint based on flexible multibody dynamics
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