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

Chimakurthi, Satish Kumar; Cesnik, Carlos E. S.; Stanford, Bret Kennedy

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

dc.contributor.author	Chimakurthi, Satish Kumar	en_US
dc.contributor.author	Cesnik, Carlos E. S.	en_US
dc.contributor.author	Stanford, Bret Kennedy	en_US
dc.date.accessioned	2012-04-05T20:35:13Z
dc.date.available	2012-04-05T20:35:13Z
dc.date.issued	2011	en_US
dc.identifier.citation	Chimakurthi, Satish; Cesnik, Carlos; Stanford, Bret (2011). "Flapping-Wing Structural Dynamics Formulation Based on a Corotational Shell Finite Element." AIAA Journal, vol. 49 no. 1 (128-142). <http://hdl.handle.net/2027.42/90628>	en_US
dc.identifier.issn	0001-1452	en_US
dc.identifier.uri	https://hdl.handle.net/2027.42/90628
dc.publisher	American Institute of Aeronautics and Astronautics	en_US
dc.title	Flapping-Wing Structural Dynamics Formulation Based on a Corotational Shell Finite Element	en_US
dc.type	Article	en_US
dc.subject.hlbsecondlevel	Aerospace Engineering	en_US
dc.subject.hlbtoplevel	Engineering	en_US
dc.description.peerreviewed	Peer Reviewed	en_US
dc.contributor.affiliationother	University of Michigan; University of Michigan; U.S. Air Force Research Laboratory	en_US
dc.description.bitstreamurl	http://deepblue.lib.umich.edu/bitstream/2027.42/90628/1/AIAA-53164-160.pdf
dc.identifier.doi	10.2514/1.53164	en_US
dc.identifier.source	AIAA Journal	en_US
dc.owningcollname	Aerospace Engineering, Department of

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