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Non-linear analysis of piezolaminated structures

2002Journal article Open Access
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dc.contributor.authorMoita, José Mateus Simõespt_PT
dc.contributor.authorSoares, Cristovão M. Motapt_PT
dc.contributor.authorSoares, Carlos A. Motapt_PT
dc.date.accessioned2009-02-13T17:09:56Z
dc.date.available2009-02-13T17:09:56Z
dc.date.issued2002
dc.description.abstractIn the recent years the study of smart structures has attracted significant researchers, due to their potential benefits in a wide range of applications, such as shape control, vibration suppression, noise attenuation and damage detection. The applications in aerospace industry are of great relevance, such as in active control of airplane wings, helicopter blade rotor, space antenna. The use of smart materials, such as piezoelectric materials, in the form of layers or patches embedded and/or surface bonded on laminated composite structures, can provide structures that combine the superior mechanical properties of composite materials and the capability to sense and adapt their static and dynamic response, becoming adaptive structures. The piezoelectric materials have the property of generate electrical charge under mechanical load or deformation, and the reverse, applying an electrical field to the material results in mechanical strain or stresses.pt_PT
dc.formatapplication/pdfpt_PT
dc.identifier.citationPAN American Congress of Applied Mechanics (PACAM VII). - Temuco - Chile, 2002. - p. 397-400pt_PT
dc.identifier.urihttp://hdl.handle.net/10400.1/156
dc.language.isoengpt_PT
dc.publisherInternational Union of Theoretical and Applied Mechanicspt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/2.0en
dc.subjectPiezometriapt_PT
dc.subject620pt_PT
dc.titleNon-linear analysis of piezolaminated structurespt_PT
dc.typejournal article
dspace.entity.typePublication
rcaap.rightsopenAccess
rcaap.typearticlept_PT

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