Bonded Joints Design Aided by Computational Tool

Detalhes bibliográficos
Autor(a) principal: Ribeiro,Marcelo L.
Data de Publicação: 2012
Outros Autores: Tita,Volnei
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Journal of Aerospace Technology and Management (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462012000300275
Resumo: Abstract: In order to aid the design of bonded joints, a computational tool named System of Analysis for Joints (SAJ) was developed. The software can analyze single and double lap bonded joint with composite-composite or metal-composite materials as adherent parts. Thus, SAJ can calculate the stress distribution, loads and displacements. Their results were compared to finite element software (ABAQUS™) and to specific composite analysis software (ESAComp™). After that, a study about the influence of joint design parameters on the mechanical behavior of the bonded joint was carried out. In regards to parametric study, SAJ leads to some conclusions, which can be used as a guide during the product design process. Therefore, aided by the computational tool, it is possible to perform a conceptual and preliminary design of bonded joints with more accuracy and varying many parameters (materials; fiber orientation and stacking sequence of the laminate; thickness; overlap length).
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spelling Bonded Joints Design Aided by Computational ToolBonded jointsDesign parametersComposite jointsComputational toolAdhesivesStress analysisAbstract: In order to aid the design of bonded joints, a computational tool named System of Analysis for Joints (SAJ) was developed. The software can analyze single and double lap bonded joint with composite-composite or metal-composite materials as adherent parts. Thus, SAJ can calculate the stress distribution, loads and displacements. Their results were compared to finite element software (ABAQUS™) and to specific composite analysis software (ESAComp™). After that, a study about the influence of joint design parameters on the mechanical behavior of the bonded joint was carried out. In regards to parametric study, SAJ leads to some conclusions, which can be used as a guide during the product design process. Therefore, aided by the computational tool, it is possible to perform a conceptual and preliminary design of bonded joints with more accuracy and varying many parameters (materials; fiber orientation and stacking sequence of the laminate; thickness; overlap length).Departamento de Ciência e Tecnologia Aeroespacial2012-09-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462012000300275Journal of Aerospace Technology and Management v.4 n.3 2012reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.2012.04032912info:eu-repo/semantics/openAccessRibeiro,Marcelo L.Tita,Volneieng2017-05-24T00:00:00Zoai:scielo:S2175-91462012000300275Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-24T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Bonded Joints Design Aided by Computational Tool
title Bonded Joints Design Aided by Computational Tool
spellingShingle Bonded Joints Design Aided by Computational Tool
Ribeiro,Marcelo L.
Bonded joints
Design parameters
Composite joints
Computational tool
Adhesives
Stress analysis
title_short Bonded Joints Design Aided by Computational Tool
title_full Bonded Joints Design Aided by Computational Tool
title_fullStr Bonded Joints Design Aided by Computational Tool
title_full_unstemmed Bonded Joints Design Aided by Computational Tool
title_sort Bonded Joints Design Aided by Computational Tool
author Ribeiro,Marcelo L.
author_facet Ribeiro,Marcelo L.
Tita,Volnei
author_role author
author2 Tita,Volnei
author2_role author
dc.contributor.author.fl_str_mv Ribeiro,Marcelo L.
Tita,Volnei
dc.subject.por.fl_str_mv Bonded joints
Design parameters
Composite joints
Computational tool
Adhesives
Stress analysis
topic Bonded joints
Design parameters
Composite joints
Computational tool
Adhesives
Stress analysis
description Abstract: In order to aid the design of bonded joints, a computational tool named System of Analysis for Joints (SAJ) was developed. The software can analyze single and double lap bonded joint with composite-composite or metal-composite materials as adherent parts. Thus, SAJ can calculate the stress distribution, loads and displacements. Their results were compared to finite element software (ABAQUS™) and to specific composite analysis software (ESAComp™). After that, a study about the influence of joint design parameters on the mechanical behavior of the bonded joint was carried out. In regards to parametric study, SAJ leads to some conclusions, which can be used as a guide during the product design process. Therefore, aided by the computational tool, it is possible to perform a conceptual and preliminary design of bonded joints with more accuracy and varying many parameters (materials; fiber orientation and stacking sequence of the laminate; thickness; overlap length).
publishDate 2012
dc.date.none.fl_str_mv 2012-09-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
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status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462012000300275
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462012000300275
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.2012.04032912
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
publisher.none.fl_str_mv Departamento de Ciência e Tecnologia Aeroespacial
dc.source.none.fl_str_mv Journal of Aerospace Technology and Management v.4 n.3 2012
reponame:Journal of Aerospace Technology and Management (Online)
instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
instname_str Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron_str DCTA
institution DCTA
reponame_str Journal of Aerospace Technology and Management (Online)
collection Journal of Aerospace Technology and Management (Online)
repository.name.fl_str_mv Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
repository.mail.fl_str_mv ||secretary@jatm.com.br
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