Flexibility Distribution Tuning by Wing Frame Inner Structure Morphing for Fixed-Wing Unmanned Aerial Vehicle
Author:
Affiliation:
1. University of Texas, Dallas
Publisher
American Institute of Aeronautics and Astronautics
Reference29 articles.
1. The Aerodynamics of Compliant Membrane Wings Modeled on Mammalian Flight Mechanics
2. Aerodynamic Coefficients and Deformation Measurements on Flexible Micro Air Vehicle Wings
3. Impact of flexibility on the aerodynamics of an aspect ratio two membrane wing
4. Aeromechanics of membrane and rigid wings in and out of ground-effect at moderate Reynolds numbers
5. Aerodynamic comparisons of flexible membrane micro air vehicle wings with cambered and flat frames
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1. Decoupled Effects of Localized Camber and Spanwise Bending for Flexible Thin Wing;AIAA Journal;2020-05
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