WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH

Detalhes bibliográficos
Autor(a) principal: Sousa, Kleverson C. de
Data de Publicação: 2017
Outros Autores: Fabro, Adriano T.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Revista Interdisciplinar de Pesquisa em Engenharia
Texto Completo: https://periodicos.unb.br/index.php/ripe/article/view/15029
Resumo: Aerospace structures require high strength and low mass, which has led to an increase in the use of composite materials by its industry. These materials result from the combination of two or more base materials in a way that one or more of the composite’s properties are superior to either of the individual ones. A type of material that presents those desired attributes is the honeycomb sandwich panels and, as the industry is relying more and more on them, their accurate characterization for the given application is of extreme importance. In this paper, the wave and finite element (WFE) approach is applied and thewave parameters of a homogenized honeycomb sandwich panel model for aerospace applications are presented and numerical details discussed. The wave approach differs from the more usual modal analysis (MA) by focusing in properties such as the dispersion relations, wave modes, phase and group velocities, and energy transmission. Although MA with the aid of finite element modelling (FEM) is a widely used technique, as the frequencies of interest increase, the computational cost also increases. Moreover, the size of the elements also limits the maximum frequency that can be accurately characterized. On the other hand, the WFE method requires the model of a single period of a periodic structure, which can be obtained from any commercial FE software, benefiting from the available element libraries,reducing the computational cost when applied to a wider frequency range. The numerically obtained parameters are compared to an analytical model and show agreement with the theory. Keywords: Wave and finite element, Wave propagation, Sandwich panel
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spelling WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACHAerospace structures require high strength and low mass, which has led to an increase in the use of composite materials by its industry. These materials result from the combination of two or more base materials in a way that one or more of the composite’s properties are superior to either of the individual ones. A type of material that presents those desired attributes is the honeycomb sandwich panels and, as the industry is relying more and more on them, their accurate characterization for the given application is of extreme importance. In this paper, the wave and finite element (WFE) approach is applied and thewave parameters of a homogenized honeycomb sandwich panel model for aerospace applications are presented and numerical details discussed. The wave approach differs from the more usual modal analysis (MA) by focusing in properties such as the dispersion relations, wave modes, phase and group velocities, and energy transmission. Although MA with the aid of finite element modelling (FEM) is a widely used technique, as the frequencies of interest increase, the computational cost also increases. Moreover, the size of the elements also limits the maximum frequency that can be accurately characterized. On the other hand, the WFE method requires the model of a single period of a periodic structure, which can be obtained from any commercial FE software, benefiting from the available element libraries,reducing the computational cost when applied to a wider frequency range. The numerically obtained parameters are compared to an analytical model and show agreement with the theory. Keywords: Wave and finite element, Wave propagation, Sandwich panelPrograma de Pós-Graduação em Integridade de Materiais da Engenharia2017-02-08info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionapplication/pdfhttps://periodicos.unb.br/index.php/ripe/article/view/1502910.26512/ripe.v2i19.15029Revista Interdisciplinar de Pesquisa em Engenharia; Vol. 2 No. 19 (2016): MODELING SIMULATION AND CONTROL OF AEROSPACE AND NAVAL STRUCTURES DYNAMICS (I); 174-185Revista Interdisciplinar de Pesquisa em Engenharia; v. 2 n. 19 (2016): MODELING SIMULATION AND CONTROL OF AEROSPACE AND NAVAL STRUCTURES DYNAMICS (I); 174-1852447-6102reponame:Revista Interdisciplinar de Pesquisa em Engenhariainstname:Universidade de Brasília (UnB)instacron:UNBenghttps://periodicos.unb.br/index.php/ripe/article/view/15029/13343Copyright (c) 2017 Revista Interdisciplinar de Pesquisa em Engenharia - RIPEinfo:eu-repo/semantics/openAccessSousa, Kleverson C. deFabro, Adriano T.2019-06-16T14:56:46Zoai:ojs.pkp.sfu.ca:article/15029Revistahttps://periodicos.unb.br/index.php/ripePUBhttps://periodicos.unb.br/index.php/ripe/oaianflor@unb.br2447-61022447-6102opendoar:2019-06-16T14:56:46Revista Interdisciplinar de Pesquisa em Engenharia - Universidade de Brasília (UnB)false
dc.title.none.fl_str_mv WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
title WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
spellingShingle WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
Sousa, Kleverson C. de
title_short WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
title_full WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
title_fullStr WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
title_full_unstemmed WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
title_sort WAVE MODELLING OF A LIGHTWEIGHT AEROSPACE PANEL USING A FINITE ELEMENT APPROACH
author Sousa, Kleverson C. de
author_facet Sousa, Kleverson C. de
Fabro, Adriano T.
author_role author
author2 Fabro, Adriano T.
author2_role author
dc.contributor.author.fl_str_mv Sousa, Kleverson C. de
Fabro, Adriano T.
description Aerospace structures require high strength and low mass, which has led to an increase in the use of composite materials by its industry. These materials result from the combination of two or more base materials in a way that one or more of the composite’s properties are superior to either of the individual ones. A type of material that presents those desired attributes is the honeycomb sandwich panels and, as the industry is relying more and more on them, their accurate characterization for the given application is of extreme importance. In this paper, the wave and finite element (WFE) approach is applied and thewave parameters of a homogenized honeycomb sandwich panel model for aerospace applications are presented and numerical details discussed. The wave approach differs from the more usual modal analysis (MA) by focusing in properties such as the dispersion relations, wave modes, phase and group velocities, and energy transmission. Although MA with the aid of finite element modelling (FEM) is a widely used technique, as the frequencies of interest increase, the computational cost also increases. Moreover, the size of the elements also limits the maximum frequency that can be accurately characterized. On the other hand, the WFE method requires the model of a single period of a periodic structure, which can be obtained from any commercial FE software, benefiting from the available element libraries,reducing the computational cost when applied to a wider frequency range. The numerically obtained parameters are compared to an analytical model and show agreement with the theory. Keywords: Wave and finite element, Wave propagation, Sandwich panel
publishDate 2017
dc.date.none.fl_str_mv 2017-02-08
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv https://periodicos.unb.br/index.php/ripe/article/view/15029
10.26512/ripe.v2i19.15029
url https://periodicos.unb.br/index.php/ripe/article/view/15029
identifier_str_mv 10.26512/ripe.v2i19.15029
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv https://periodicos.unb.br/index.php/ripe/article/view/15029/13343
dc.rights.driver.fl_str_mv Copyright (c) 2017 Revista Interdisciplinar de Pesquisa em Engenharia - RIPE
info:eu-repo/semantics/openAccess
rights_invalid_str_mv Copyright (c) 2017 Revista Interdisciplinar de Pesquisa em Engenharia - RIPE
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Programa de Pós-Graduação em Integridade de Materiais da Engenharia
publisher.none.fl_str_mv Programa de Pós-Graduação em Integridade de Materiais da Engenharia
dc.source.none.fl_str_mv Revista Interdisciplinar de Pesquisa em Engenharia; Vol. 2 No. 19 (2016): MODELING SIMULATION AND CONTROL OF AEROSPACE AND NAVAL STRUCTURES DYNAMICS (I); 174-185
Revista Interdisciplinar de Pesquisa em Engenharia; v. 2 n. 19 (2016): MODELING SIMULATION AND CONTROL OF AEROSPACE AND NAVAL STRUCTURES DYNAMICS (I); 174-185
2447-6102
reponame:Revista Interdisciplinar de Pesquisa em Engenharia
instname:Universidade de Brasília (UnB)
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reponame_str Revista Interdisciplinar de Pesquisa em Engenharia
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repository.name.fl_str_mv Revista Interdisciplinar de Pesquisa em Engenharia - Universidade de Brasília (UnB)
repository.mail.fl_str_mv anflor@unb.br
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