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

By Satish Chimakurthi, Carlos Cesnik and Bret Stanford
Publisher: American Institute of Aeronautics and Astronautics
Year: 2011
DOI identifier: 10.2514/1.53164
OAI identifier: oai:deepblue.lib.umich.edu:2027.42/90628

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