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Aerostructural design optimization of a continuous morphing trailing edge aircraft for improved mission performance

dc.contributor.authorBurdette, David A.
dc.contributor.authorKenway, Gaetan K.
dc.contributor.authorMartins, Joaquim
dc.date.accessioned2018-01-03T17:17:05Z
dc.date.available2018-01-03T17:17:05Z
dc.date.issued2016-06-10
dc.identifier.citationBurdette, David A.; Kenway, Gaetan K.; Martins, Joaquim (2016). "Aerostructural design optimization of a continuous morphing trailing edge aircraft for improved mission performance." 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
dc.identifier.urihttps://hdl.handle.net/2027.42/140608
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.relation.ispartofseriesAIAA AVIATION Forum
dc.titleAerostructural design optimization of a continuous morphing trailing edge aircraft for improved mission performance
dc.typeConference Paperen_US
dc.subject.hlbsecondlevelAerospace Engineering
dc.subject.hlbtoplevelEngineering
dc.description.peerreviewedPeer Reviewed
dc.description.bitstreamurlhttps://deepblue.lib.umich.edu/bitstream/2027.42/140608/1/6.2016-3209.pdf
dc.identifier.doi10.2514/6.2016-3209
dc.identifier.source17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
dc.owningcollnameAerospace Engineering, Department of


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