Design and Testing of a Lattice-based Cellular Component Active Twist Wing
Author:
Affiliation:
1. University of California, Santa Cruz
2. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1085
Reference17 articles.
1. Morphing Aerospace Vehicles and Structures
2. Aeroelastic Modeling of Elastically Shaped Aircraft Concept via Wing Shaping Control for Drag Reduction
3. Aeroelastic Wing Shaping Control Subject to Actuation Constraints
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