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Nonlinear Aeroelastic Framework Based on Vortex-Lattice Method and Corotational Shell Finite Element

dc.contributor.authorSouza, Carlos deen_US
dc.contributor.authorSilva, Roberto Gil daen_US
dc.contributor.authorCesnik, Carlosen_US
dc.date.accessioned2013-04-08T19:59:30Z
dc.date.available2013-04-08T19:59:30Z
dc.date.issued2012en_US
dc.identifier.citationCarlos de Souza, Roberto Gil da Silva, Carlos Cesnik, "Nonlinear Aeroelastic Framework Based on Vortex-Lattice Method and Corotational Shell Finite Element", 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2012, 10.2514/6.2012-1976 <http://hdl.handle.net/2027.42/97077>en_US
dc.identifier.otherAIAA 2012-1976en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/97077
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleNonlinear Aeroelastic Framework Based on Vortex-Lattice Method and Corotational Shell Finite Elementen_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/2027.42/97077/1/AIAA2012-1976.pdf
dc.identifier.doi10.2514/6.2012-1976en_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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