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Finit element model for active control of adaptive laminated structures

dc.contributor.authorMoita, José Mateus Simõespt_PT
dc.contributor.authorSoares, Cristovão M. Motapt_PT
dc.contributor.authorSoares, Carlos A. Motapt_PT
dc.date.accessioned2009-02-13T17:09:49Z
dc.date.available2009-02-13T17:09:49Z
dc.date.issued2003
dc.description.abstractA finite element formulation for active vibration control of thin plate laminated structures with integrated piezoelectric layers, acting as sensors and actuators in presented. The finite element model is a nonconforming single layer triangular plate/shell element with 18 degrees of freedom for the generalized displacements and one electrical potential degree of freedom for each piezoelectric element layer, and is based on the kirchhoff classical laminated theory. To achieve a mechanism of active control of the structure dynamic response, a feedback control algorithm is used, coupling the sensor and active piezoelectric layers, and Newmark method is used to calculate yhe dynamic response of the laminated structures. The model is applied in the solution of several illustrative cases, and the results are presented and discussed.pt_PT
dc.formatapplication/pdfpt_PT
dc.identifier.citationXXIV Iberian Latin-American Congress on Computational Methods in Engineering. - Ouro Preto - Brasil, 2003. - 6 fpt_PT
dc.identifier.urihttp://hdl.handle.net/10400.1/137
dc.language.isoengpt_PT
dc.publisherOuro Preto - Brasilpt_PT
dc.relation.urihttp://www.bib.ualg.pt/artigos/DocentesEST/MOIFin.pdfpt_PT
dc.rights.uriopenAccessen
dc.subjectElementos finitospt_PT
dc.subject620pt_PT
dc.titleFinit element model for active control of adaptive laminated structurespt_PT
dc.typejournal article
dspace.entity.typePublication
rcaap.typearticlept_PT

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