A three layer quasi 3D finite element model for structural analysis of sandwich plates.

Detalhes bibliográficos
Autor(a) principal: Airton Nabarrete
Data de Publicação: 2002
Tipo de documento: Tese
Idioma: eng
Título da fonte: Biblioteca Digital de Teses e Dissertações do ITA
Texto Completo: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2502
Resumo: A three-layer finite element model for the analysis of sandwich plates with laminated composite face-sheets is evaluated. In the model, the face-sheets are represented as Reissner-Mindlin plates and the core is modeled as a three-dimensional continuum. This representation allows accurate modeling for a wide range of core types. The three-dimensional problem is reduced to two dimensions by analytical through-thickness integration of the energy expressions for the evaluation of elastic and geometric stiffness, and mass matrices. The results from this model are compared to finite element results based on solid elements, laminated Reissner-Mindlin, and laminated classical plate theory. The objective of the work is to analyze the following aspects of sandwich plates using the developed model for a broad range of core stiffness: natural frequencies and corresponding mode shapes, critical buckling loads, stress stiffening effects, and the dynamic analysis including piezoelectric actuation on the face-sheets. When large differences between face-sheet and core stiffness is present it is illustrated that traditional laminate theories yield significant inaccuracy. Moreover, unlike plate models, the present theory is also capable of representing a variety of three dimensional boundary conditions. Furthermore, compared to solid models, the present sandwich model avoids numerical problems due to three dimensional element aspect ratio that facilitates modeling sandwich plates with thin faces and thick core. Therefore, the present model provides a powerful general tool for a wide variety of structural analyses of sandwich plates.
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spelling A three layer quasi 3D finite element model for structural analysis of sandwich plates.Estruturas sanduícheAnálise estruturalMétodo de elementos finitosModelos matemáticosEstruturas tridimensionaisVibração estruturalFlambagemMateriais piezoelétricosAtuadoresPlacas (membros estruturais)Engenharia de materiaisA three-layer finite element model for the analysis of sandwich plates with laminated composite face-sheets is evaluated. In the model, the face-sheets are represented as Reissner-Mindlin plates and the core is modeled as a three-dimensional continuum. This representation allows accurate modeling for a wide range of core types. The three-dimensional problem is reduced to two dimensions by analytical through-thickness integration of the energy expressions for the evaluation of elastic and geometric stiffness, and mass matrices. The results from this model are compared to finite element results based on solid elements, laminated Reissner-Mindlin, and laminated classical plate theory. The objective of the work is to analyze the following aspects of sandwich plates using the developed model for a broad range of core stiffness: natural frequencies and corresponding mode shapes, critical buckling loads, stress stiffening effects, and the dynamic analysis including piezoelectric actuation on the face-sheets. When large differences between face-sheet and core stiffness is present it is illustrated that traditional laminate theories yield significant inaccuracy. Moreover, unlike plate models, the present theory is also capable of representing a variety of three dimensional boundary conditions. Furthermore, compared to solid models, the present sandwich model avoids numerical problems due to three dimensional element aspect ratio that facilitates modeling sandwich plates with thin faces and thick core. Therefore, the present model provides a powerful general tool for a wide variety of structural analyses of sandwich plates. Instituto Tecnológico de AeronáuticaSérgio Frascino Müller de AlmeidaAirton Nabarrete2002-00-00info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/doctoralThesishttp://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2502reponame:Biblioteca Digital de Teses e Dissertações do ITAinstname:Instituto Tecnológico de Aeronáuticainstacron:ITAenginfo:eu-repo/semantics/openAccessapplication/pdf2019-02-02T14:04:48Zoai:agregador.ibict.br.BDTD_ITA:oai:ita.br:2502http://oai.bdtd.ibict.br/requestopendoar:null2020-05-28 19:39:17.878Biblioteca Digital de Teses e Dissertações do ITA - Instituto Tecnológico de Aeronáuticatrue
dc.title.none.fl_str_mv A three layer quasi 3D finite element model for structural analysis of sandwich plates.
title A three layer quasi 3D finite element model for structural analysis of sandwich plates.
spellingShingle A three layer quasi 3D finite element model for structural analysis of sandwich plates.
Airton Nabarrete
Estruturas sanduíche
Análise estrutural
Método de elementos finitos
Modelos matemáticos
Estruturas tridimensionais
Vibração estrutural
Flambagem
Materiais piezoelétricos
Atuadores
Placas (membros estruturais)
Engenharia de materiais
title_short A three layer quasi 3D finite element model for structural analysis of sandwich plates.
title_full A three layer quasi 3D finite element model for structural analysis of sandwich plates.
title_fullStr A three layer quasi 3D finite element model for structural analysis of sandwich plates.
title_full_unstemmed A three layer quasi 3D finite element model for structural analysis of sandwich plates.
title_sort A three layer quasi 3D finite element model for structural analysis of sandwich plates.
author Airton Nabarrete
author_facet Airton Nabarrete
author_role author
dc.contributor.none.fl_str_mv Sérgio Frascino Müller de Almeida
dc.contributor.author.fl_str_mv Airton Nabarrete
dc.subject.por.fl_str_mv Estruturas sanduíche
Análise estrutural
Método de elementos finitos
Modelos matemáticos
Estruturas tridimensionais
Vibração estrutural
Flambagem
Materiais piezoelétricos
Atuadores
Placas (membros estruturais)
Engenharia de materiais
topic Estruturas sanduíche
Análise estrutural
Método de elementos finitos
Modelos matemáticos
Estruturas tridimensionais
Vibração estrutural
Flambagem
Materiais piezoelétricos
Atuadores
Placas (membros estruturais)
Engenharia de materiais
dc.description.none.fl_txt_mv A three-layer finite element model for the analysis of sandwich plates with laminated composite face-sheets is evaluated. In the model, the face-sheets are represented as Reissner-Mindlin plates and the core is modeled as a three-dimensional continuum. This representation allows accurate modeling for a wide range of core types. The three-dimensional problem is reduced to two dimensions by analytical through-thickness integration of the energy expressions for the evaluation of elastic and geometric stiffness, and mass matrices. The results from this model are compared to finite element results based on solid elements, laminated Reissner-Mindlin, and laminated classical plate theory. The objective of the work is to analyze the following aspects of sandwich plates using the developed model for a broad range of core stiffness: natural frequencies and corresponding mode shapes, critical buckling loads, stress stiffening effects, and the dynamic analysis including piezoelectric actuation on the face-sheets. When large differences between face-sheet and core stiffness is present it is illustrated that traditional laminate theories yield significant inaccuracy. Moreover, unlike plate models, the present theory is also capable of representing a variety of three dimensional boundary conditions. Furthermore, compared to solid models, the present sandwich model avoids numerical problems due to three dimensional element aspect ratio that facilitates modeling sandwich plates with thin faces and thick core. Therefore, the present model provides a powerful general tool for a wide variety of structural analyses of sandwich plates.
description A three-layer finite element model for the analysis of sandwich plates with laminated composite face-sheets is evaluated. In the model, the face-sheets are represented as Reissner-Mindlin plates and the core is modeled as a three-dimensional continuum. This representation allows accurate modeling for a wide range of core types. The three-dimensional problem is reduced to two dimensions by analytical through-thickness integration of the energy expressions for the evaluation of elastic and geometric stiffness, and mass matrices. The results from this model are compared to finite element results based on solid elements, laminated Reissner-Mindlin, and laminated classical plate theory. The objective of the work is to analyze the following aspects of sandwich plates using the developed model for a broad range of core stiffness: natural frequencies and corresponding mode shapes, critical buckling loads, stress stiffening effects, and the dynamic analysis including piezoelectric actuation on the face-sheets. When large differences between face-sheet and core stiffness is present it is illustrated that traditional laminate theories yield significant inaccuracy. Moreover, unlike plate models, the present theory is also capable of representing a variety of three dimensional boundary conditions. Furthermore, compared to solid models, the present sandwich model avoids numerical problems due to three dimensional element aspect ratio that facilitates modeling sandwich plates with thin faces and thick core. Therefore, the present model provides a powerful general tool for a wide variety of structural analyses of sandwich plates.
publishDate 2002
dc.date.none.fl_str_mv 2002-00-00
dc.type.driver.fl_str_mv info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/doctoralThesis
status_str publishedVersion
format doctoralThesis
dc.identifier.uri.fl_str_mv http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2502
url http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2502
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 Estruturas sanduíche
Análise estrutural
Método de elementos finitos
Modelos matemáticos
Estruturas tridimensionais
Vibração estrutural
Flambagem
Materiais piezoelétricos
Atuadores
Placas (membros estruturais)
Engenharia de materiais
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