Effects of Reynolds Number and Flapping Kinematics on Hovering Aerodynamics
Author:
Affiliation:
1. 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/10.2514/1.32191
Reference40 articles.
1. Flapping and flexible wings for biological and micro air vehicles
2. The mechanisms of lift enhancement in insect flight
3. Vertebrate Flight
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