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oaioai:deepblue.lib.umich.edu:2027.42/90628

Flapping-Wing Structural Dynamics Formulation Based on a Corotational Shell Finite Element

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Publication date
1 January 2011
Publisher
American Institute of Aeronautics and Astronautics
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    Abstract

    Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90628/1/AIAA-53164-160.pd

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    Last time updated on 25/05/2012

    This paper was published in Deep Blue Documents at the University of Michigan.

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