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A Regularized Discrete Laminate Parametrization Technique with Applications to Wing-Box Design Optimization

dc.contributor.authorKennedy, Graemeen_US
dc.contributor.authorMartins, Joaquimen_US
dc.date.accessioned2013-04-08T19:59:23Z
dc.date.available2013-04-08T19:59:23Z
dc.date.issued2012en_US
dc.identifier.citationGraeme Kennedy, Joaquim Martins, "A Regularized Discrete Laminate Parametrization Technique with Applications to Wing-Box Design Optimization", 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2012, 10.2514/6.2012-1519 <http://hdl.handle.net/2027.42/97055>en_US
dc.identifier.otherAIAA 2012-1519en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/97055
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleA Regularized Discrete Laminate Parametrization Technique with Applications to Wing-Box Design Optimizationen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/97055/1/AIAA2012-1519.pdf
dc.identifier.doi10.2514/6.2012-1519en_US
dc.identifier.source53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conferenceen_US
dc.owningcollnameAerospace Engineering, Department of


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