Computational Aeroelasticity Framework for Analyzing Flapping Wing Micro Air Vehicles

Published 2009 View Full Article

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Title
Computational Aeroelasticity Framework for Analyzing Flapping Wing Micro Air Vehicles
Authors
Keywords
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Journal
AIAA JOURNAL
Volume 47, Issue 8, Pages 1865-1878
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2009-07-10
DOI
10.2514/1.38845
References
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