A recursive methodology to determine the mechanical Response of thin laminated plates in bending

Detalhes bibliográficos
Autor(a) principal: Lisbôa, Tales de Vargas
Data de Publicação: 2017
Outros Autores: Geiger, Filipe Paixão, Marczak, Rogerio Jose
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UFRGS
Texto Completo: http://hdl.handle.net/10183/179254
Resumo: The paper’s objective is to present the development of a recursive methodology which is based on Adomian Decompostion Method in order to evaluate the mechanical response of thin laminated plates in linear bending. By the equivalent layer concept, the linear relation between the equivalent stresses and the strains, namely ABD matrix, is established. When viewed by the Adomian Decompostion Method perspective, it generates an interesting idea: each layer influence on the plate’s response can be recursively inserted into a base solution by a rearrangement of the plate’s properties. This base solution is previously obtained and it is, in this paper, an isotropic plate response for the same loading and boundary conditions. This approach can significantly increase optimization and delamination studies, given the simplicity on the layers modification, both in fiber orientation and constitutive properties, as these are considered on the recursive procedure. The pb-2 Rayleigh-Ritz Method is used to approximate the solution space and to generate analytic response surfaces. The methodology is applied to symmetrical and unsymmetrical stacking cases for different boundary conditions sets and loading types and the obtained responses are compared to those found on the literature. A study of case complements the methodology analysis: a simplified landing gear door is modeled considering a set of loading conditions as well as different stacking configurations. Good correspondence was found in all studied cases.
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spelling Lisbôa, Tales de VargasGeiger, Filipe PaixãoMarczak, Rogerio Jose2018-06-09T03:34:19Z20172175-9146http://hdl.handle.net/10183/179254001068241The paper’s objective is to present the development of a recursive methodology which is based on Adomian Decompostion Method in order to evaluate the mechanical response of thin laminated plates in linear bending. By the equivalent layer concept, the linear relation between the equivalent stresses and the strains, namely ABD matrix, is established. When viewed by the Adomian Decompostion Method perspective, it generates an interesting idea: each layer influence on the plate’s response can be recursively inserted into a base solution by a rearrangement of the plate’s properties. This base solution is previously obtained and it is, in this paper, an isotropic plate response for the same loading and boundary conditions. This approach can significantly increase optimization and delamination studies, given the simplicity on the layers modification, both in fiber orientation and constitutive properties, as these are considered on the recursive procedure. The pb-2 Rayleigh-Ritz Method is used to approximate the solution space and to generate analytic response surfaces. The methodology is applied to symmetrical and unsymmetrical stacking cases for different boundary conditions sets and loading types and the obtained responses are compared to those found on the literature. A study of case complements the methodology analysis: a simplified landing gear door is modeled considering a set of loading conditions as well as different stacking configurations. Good correspondence was found in all studied cases.application/pdfengJournal of aerospace technology and management [recurso eletrônico]. São José dos Campos. Vol. 9, no. 4 (Oct./Dec. 2017), p. 409-422Placa finaMétodos matemáticosRecursive methodologyAdomian decomposition methodSandwich plates and laminated platesThin plates in bendingA recursive methodology to determine the mechanical Response of thin laminated plates in bendinginfo:eu-repo/semantics/articleinfo:eu-repo/semantics/otherinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/openAccessreponame:Repositório Institucional da UFRGSinstname:Universidade Federal do Rio Grande do Sul (UFRGS)instacron:UFRGSORIGINAL001068241.pdf001068241.pdfTexto completo (inglês)application/pdf2688712http://www.lume.ufrgs.br/bitstream/10183/179254/1/001068241.pdfd084f7091a3bdcad37a2c2ed92d33635MD51TEXT001068241.pdf.txt001068241.pdf.txtExtracted Texttext/plain43165http://www.lume.ufrgs.br/bitstream/10183/179254/2/001068241.pdf.txta8f0c9b58fbf33fd025d8c57f9336719MD5210183/1792542018-06-10 02:35:31.185666oai:www.lume.ufrgs.br:10183/179254Repositório de PublicaçõesPUBhttps://lume.ufrgs.br/oai/requestopendoar:2018-06-10T05:35:31Repositório Institucional da UFRGS - Universidade Federal do Rio Grande do Sul (UFRGS)false
dc.title.pt_BR.fl_str_mv A recursive methodology to determine the mechanical Response of thin laminated plates in bending
title A recursive methodology to determine the mechanical Response of thin laminated plates in bending
spellingShingle A recursive methodology to determine the mechanical Response of thin laminated plates in bending
Lisbôa, Tales de Vargas
Placa fina
Métodos matemáticos
Recursive methodology
Adomian decomposition method
Sandwich plates and laminated plates
Thin plates in bending
title_short A recursive methodology to determine the mechanical Response of thin laminated plates in bending
title_full A recursive methodology to determine the mechanical Response of thin laminated plates in bending
title_fullStr A recursive methodology to determine the mechanical Response of thin laminated plates in bending
title_full_unstemmed A recursive methodology to determine the mechanical Response of thin laminated plates in bending
title_sort A recursive methodology to determine the mechanical Response of thin laminated plates in bending
author Lisbôa, Tales de Vargas
author_facet Lisbôa, Tales de Vargas
Geiger, Filipe Paixão
Marczak, Rogerio Jose
author_role author
author2 Geiger, Filipe Paixão
Marczak, Rogerio Jose
author2_role author
author
dc.contributor.author.fl_str_mv Lisbôa, Tales de Vargas
Geiger, Filipe Paixão
Marczak, Rogerio Jose
dc.subject.por.fl_str_mv Placa fina
Métodos matemáticos
topic Placa fina
Métodos matemáticos
Recursive methodology
Adomian decomposition method
Sandwich plates and laminated plates
Thin plates in bending
dc.subject.eng.fl_str_mv Recursive methodology
Adomian decomposition method
Sandwich plates and laminated plates
Thin plates in bending
description The paper’s objective is to present the development of a recursive methodology which is based on Adomian Decompostion Method in order to evaluate the mechanical response of thin laminated plates in linear bending. By the equivalent layer concept, the linear relation between the equivalent stresses and the strains, namely ABD matrix, is established. When viewed by the Adomian Decompostion Method perspective, it generates an interesting idea: each layer influence on the plate’s response can be recursively inserted into a base solution by a rearrangement of the plate’s properties. This base solution is previously obtained and it is, in this paper, an isotropic plate response for the same loading and boundary conditions. This approach can significantly increase optimization and delamination studies, given the simplicity on the layers modification, both in fiber orientation and constitutive properties, as these are considered on the recursive procedure. The pb-2 Rayleigh-Ritz Method is used to approximate the solution space and to generate analytic response surfaces. The methodology is applied to symmetrical and unsymmetrical stacking cases for different boundary conditions sets and loading types and the obtained responses are compared to those found on the literature. A study of case complements the methodology analysis: a simplified landing gear door is modeled considering a set of loading conditions as well as different stacking configurations. Good correspondence was found in all studied cases.
publishDate 2017
dc.date.issued.fl_str_mv 2017
dc.date.accessioned.fl_str_mv 2018-06-09T03:34:19Z
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dc.identifier.uri.fl_str_mv http://hdl.handle.net/10183/179254
dc.identifier.issn.pt_BR.fl_str_mv 2175-9146
dc.identifier.nrb.pt_BR.fl_str_mv 001068241
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dc.relation.ispartof.pt_BR.fl_str_mv Journal of aerospace technology and management [recurso eletrônico]. São José dos Campos. Vol. 9, no. 4 (Oct./Dec. 2017), p. 409-422
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