An Adjoint-based Derivative Evaluation Method for Time-dependent Aeroelastic Optimization of Flexible Aircraft

Kennedy, Graeme; Martins, Joaquim

An Adjoint-based Derivative Evaluation Method for Time-dependent Aeroelastic Optimization of Flexible Aircraft

dc.contributor.author	Kennedy, Graeme	en_US
dc.contributor.author	Martins, Joaquim	en_US
dc.date.accessioned	2014-04-10T14:50:51Z
dc.date.available	2014-04-10T14:50:51Z
dc.date.issued	2013	en_US
dc.identifier.citation	54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <http://hdl.handle.net/2027.42/106483>	en_US
dc.identifier.other	AIAA2013-1530
dc.identifier.uri	https://hdl.handle.net/2027.42/106483
dc.publisher	Peer Reviewed	en_US
dc.title	An Adjoint-based Derivative Evaluation Method for Time-dependent Aeroelastic Optimization of Flexible Aircraft	en_US
dc.type	Article	en_US
dc.subject.hlbsecondlevel	Article	en_US
dc.subject.hlbsecondlevel	Aerospace Engineering	en_US
dc.subject.hlbtoplevel	Engineering	en_US
dc.description.peerreviewed	Peer Reviewed	en_US
dc.description.bitstreamurl	http://deepblue.lib.umich.edu/bitstream/2027.42/106483/1/AIAA2013-1530.pdf
dc.identifier.doi	10.2514/6.2013-1530	en_US
dc.identifier.source	American Institute of Aeronautics and Astronautics	en_US
dc.owningcollname	Aerospace Engineering, Department of

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