Optimization of Flexible Flapping-Wing Kinematics in Hover
Author:
Affiliation:
1. Department of Mechanical and Aerospace, Ohio State University, Columbus, Ohio 43210
2. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053083
Reference34 articles.
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5. Development of the Nano Hummingbird: A Tailless Flapping Wing Micro Air Vehicle
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