Investigation of aspect ratio and dynamic effects due to rotation for a revolving wing using high-fidelity simulation
Author:
Affiliation:
1. Air Force Research Laboratory
2. University of Cincinnati
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-86
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1. The novel aerodynamics of insect flight: applications to micro-air vehicles
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