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High-fidelity Aerostructural Optimization of a High Aspect Ratio Tow-steered Wing
dc.contributor.authorBrooks, Timothy R.
dc.contributor.authorKennedy, Graeme
dc.contributor.authorMartins, Joaquim
dc.date.accessioned2018-01-03T17:16:19Z
dc.date.available2018-01-03T17:16:19Z
dc.date.issued2016-01-01
dc.identifier.citationBrooks, Timothy R.; Kennedy, Graeme; Martins, Joaquim (2016). "High-fidelity Aerostructural Optimization of a High Aspect Ratio Tow-steered Wing." 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
dc.identifier.urihttps://hdl.handle.net/2027.42/140574
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.relation.ispartofseriesAIAA SciTech Forum
dc.titleHigh-fidelity Aerostructural Optimization of a High Aspect Ratio Tow-steered Wing
dc.typeConference Paperen_US
dc.subject.hlbsecondlevelAerospace Engineering
dc.subject.hlbtoplevelEngineering
dc.description.peerreviewedPeer Reviewed
dc.description.bitstreamurlhttps://deepblue.lib.umich.edu/bitstream/2027.42/140574/1/6.2016-1179.pdf
dc.identifier.doi10.2514/6.2016-1179
dc.identifier.source57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
dc.owningcollnameAerospace Engineering, Department of


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