Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.

Detalhes bibliográficos
Ano de defesa: 2000
Autor(a) principal: Adriano Luiz de Carvalho Neto
Orientador(a): Não Informado pela instituição
Banca de defesa: Não Informado pela instituição
Tipo de documento: Dissertação
Tipo de acesso: Acesso aberto
Idioma: eng
Instituição de defesa: Instituto Tecnológico de Aeronáutica
Programa de Pós-Graduação: Não Informado pela instituição
Departamento: Não Informado pela instituição
País: Não Informado pela instituição
Palavras-chave em Português:
Placas (membros estruturais)
Laminados
Piezoeletricidade
Estruturas
Método de elementos finitos
Materiais compósitos
Engenharia estrutural
Engenharia mecânica
Link de acesso: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2380
Resumo: A formulation of a finite element for a composite plate containing distributed piexoelectric layers that can be either bonded to the surface or embedded within the structure, considering the Classical Laminated Plate Theory (CLPT), is presented. Temperatures effects are neglected. The finite element has a rectangular shape with four nodal points, flexural and membrane stiffness, six mechanical degrees of freedom per nodal point (u; v; w; W,x; W,y; W,xy) and one electrical potential degree of freedom per piezoelectric layer ( f ). This element presents continuity C0 in the in-plane displacements, continuity C1 in the transversal displacement and the electric potentials are constants throughout the plane of the piezoelectric layer but varying linearly thru the thickness. Two comparison case studies are presented and the present formulation shows a good agreement with the results available in the literature.
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spelling Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.Placas (membros estruturais)LaminadosPiezoeletricidadeEstruturasMétodo de elementos finitosMateriais compósitosEngenharia estruturalEngenharia mecânicaA formulation of a finite element for a composite plate containing distributed piexoelectric layers that can be either bonded to the surface or embedded within the structure, considering the Classical Laminated Plate Theory (CLPT), is presented. Temperatures effects are neglected. The finite element has a rectangular shape with four nodal points, flexural and membrane stiffness, six mechanical degrees of freedom per nodal point (u; v; w; W,x; W,y; W,xy) and one electrical potential degree of freedom per piezoelectric layer ( f ). This element presents continuity C0 in the in-plane displacements, continuity C1 in the transversal displacement and the electric potentials are constants throughout the plane of the piezoelectric layer but varying linearly thru the thickness. Two comparison case studies are presented and the present formulation shows a good agreement with the results available in the literature. Instituto Tecnológico de AeronáuticaMaher Nasr Bismarck-NasrAdriano Luiz de Carvalho Neto2000-00-00info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/masterThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2380reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:04:46Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2380http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:38:58.199Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
title Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
spellingShingle Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
Adriano Luiz de Carvalho Neto
Placas (membros estruturais)
Laminados
Piezoeletricidade
Estruturas
Método de elementos finitos
Materiais compósitos
Engenharia estrutural
Engenharia mecânica
title_short Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
title_full Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
title_fullStr Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
title_full_unstemmed Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
title_sort Formulation of a rectangular finite element for a laminated composite plate with piezoelectric layers.
author Adriano Luiz de Carvalho Neto
author_facet Adriano Luiz de Carvalho Neto
author_role author
dc.contributor.none.fl_str_mv Maher Nasr Bismarck-Nasr
dc.contributor.author.fl_str_mv Adriano Luiz de Carvalho Neto
dc.subject.por.fl_str_mv Placas (membros estruturais)
Laminados
Piezoeletricidade
Estruturas
Método de elementos finitos
Materiais compósitos
Engenharia estrutural
Engenharia mecânica
topic Placas (membros estruturais)
Laminados
Piezoeletricidade
Estruturas
Método de elementos finitos
Materiais compósitos
Engenharia estrutural
Engenharia mecânica
dc.description.none.fl_txt_mv A formulation of a finite element for a composite plate containing distributed piexoelectric layers that can be either bonded to the surface or embedded within the structure, considering the Classical Laminated Plate Theory (CLPT), is presented. Temperatures effects are neglected. The finite element has a rectangular shape with four nodal points, flexural and membrane stiffness, six mechanical degrees of freedom per nodal point (u; v; w; W,x; W,y; W,xy) and one electrical potential degree of freedom per piezoelectric layer ( f ). This element presents continuity C0 in the in-plane displacements, continuity C1 in the transversal displacement and the electric potentials are constants throughout the plane of the piezoelectric layer but varying linearly thru the thickness. Two comparison case studies are presented and the present formulation shows a good agreement with the results available in the literature.
description A formulation of a finite element for a composite plate containing distributed piexoelectric layers that can be either bonded to the surface or embedded within the structure, considering the Classical Laminated Plate Theory (CLPT), is presented. Temperatures effects are neglected. The finite element has a rectangular shape with four nodal points, flexural and membrane stiffness, six mechanical degrees of freedom per nodal point (u; v; w; W,x; W,y; W,xy) and one electrical potential degree of freedom per piezoelectric layer ( f ). This element presents continuity C0 in the in-plane displacements, continuity C1 in the transversal displacement and the electric potentials are constants throughout the plane of the piezoelectric layer but varying linearly thru the thickness. Two comparison case studies are presented and the present formulation shows a good agreement with the results available in the literature.
publishDate 2000
dc.date.none.fl_str_mv 2000-00-00
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/masterThesis
status_str publishedVersion
format masterThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2380
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2380
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
publisher.none.fl_str_mv Instituto Tecnológico de Aeronáutica
dc.source.none.fl_str_mv reponame:Biblioteca Digital de Teses e Dissertações do ITA
instname:Instituto Tecnológico de Aeronáutica
instacron:ITA
reponame_str Biblioteca Digital de Teses e Dissertações do ITA
collection Biblioteca Digital de Teses e Dissertações do ITA
instname_str Instituto Tecnológico de Aeronáutica
instacron_str ITA
institution ITA
repository.name.fl_str_mv Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáutica
repository.mail.fl_str_mv
subject_por_txtF_mv Placas (membros estruturais)
Laminados
Piezoeletricidade
Estruturas
Método de elementos finitos
Materiais compósitos
Engenharia estrutural
Engenharia mecânica
_version_ 1706804999393116160

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