Design of a Sliding Morphing Skin with Segmented Rigid Panels
Author:
Affiliation:
1. Ryerson University, Toronto, Ontario M5B 2K3, Canada
2. University of Michigan, Ann Arbor, Michigan 48109
3. Harbin Institute of Technology, 518055 Shenzhen, People’s Republic of China
Funder
International Collaborative Research Fund of Shenzhen, China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034711
Reference40 articles.
1. A Review of Morphing Aircraft
2. Design and Motion Control of Fully Variable Morphing Wings
3. Aircraft Control via Variable Cant-Angle Winglets
4. Aero-structural Design Optimization of a Morphing Wingtip
5. Conceptual study of a morphing winglet based on unsymmetrical stiffness
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