Fatigue behaviour study on repaired aramid fiber/epoxy composites

Detalhes bibliográficos
Autor(a) principal: Botelho,Edson Cocchieri
Data de Publicação: 2009
Outros Autores: Mazur,Rogério Lago, Costa,Michelle Leali, Cândido,Geraldo Maurício, Rezende,Mirabel Cerqueira
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=S2175-91462009000200217
Resumo: Abstract: Aramid fiber reinforced polymer composites have been used in a wide variety of applications, such as aerospace, marine, sporting equipment and in the defense sector, due to their outstanding properties at low density. The most widely adopted procedure to investigate the repair of composites has been by repairing damages simulated in composite specimens. This work presents the structural repair influence on tensile and fatigue properties of a typical aramid fiber/epoxy composite used in the aerospace industry. According to this work, the aramid/epoxy composites with and without repair present tensile strength values of 618 and 680MPa, respectively, and tensile modulus of 26.5 and 30.1 GPa, respectively. Therefore, the fatigue results show that in loads higher than 170 MPa, both composites present a low life cycle (lower than 200,000 cycles) and the repaired aramid/epoxy composite presented low fatigue resistance in low and high cycle when compared with non-repaired composite. With these results, it is possible to observe a decrease of the measured mechanical properties of the repaired composites.
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spelling Fatigue behaviour study on repaired aramid fiber/epoxy compositesFatigue behaviorAramid/epoxy compositeStructural compositesMechanical behaviorAbstract: Aramid fiber reinforced polymer composites have been used in a wide variety of applications, such as aerospace, marine, sporting equipment and in the defense sector, due to their outstanding properties at low density. The most widely adopted procedure to investigate the repair of composites has been by repairing damages simulated in composite specimens. This work presents the structural repair influence on tensile and fatigue properties of a typical aramid fiber/epoxy composite used in the aerospace industry. According to this work, the aramid/epoxy composites with and without repair present tensile strength values of 618 and 680MPa, respectively, and tensile modulus of 26.5 and 30.1 GPa, respectively. Therefore, the fatigue results show that in loads higher than 170 MPa, both composites present a low life cycle (lower than 200,000 cycles) and the repaired aramid/epoxy composite presented low fatigue resistance in low and high cycle when compared with non-repaired composite. With these results, it is possible to observe a decrease of the measured mechanical properties of the repaired composites.Departamento de Ciência e Tecnologia Aeroespacial2009-12-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462009000200217Journal of Aerospace Technology and Management v.1 n.2 2009reponame:Journal of Aerospace Technology and Management (Online)instname:Departamento de Ciência e Tecnologia Aeroespacial (DCTA)instacron:DCTA10.5028/jatm.2009.0102217221info:eu-repo/semantics/openAccessBotelho,Edson CocchieriMazur,Rogério LagoCosta,Michelle LealiCândido,Geraldo MaurícioRezende,Mirabel Cerqueiraeng2017-05-29T00:00:00Zoai:scielo:S2175-91462009000200217Revistahttp://www.jatm.com.br/ONGhttps://old.scielo.br/oai/scielo-oai.php||secretary@jatm.com.br2175-91461984-9648opendoar:2017-05-29T00:00Journal of Aerospace Technology and Management (Online) - Departamento de Ciência e Tecnologia Aeroespacial (DCTA)false
dc.title.none.fl_str_mv Fatigue behaviour study on repaired aramid fiber/epoxy composites
title Fatigue behaviour study on repaired aramid fiber/epoxy composites
spellingShingle Fatigue behaviour study on repaired aramid fiber/epoxy composites
Botelho,Edson Cocchieri
Fatigue behavior
Aramid/epoxy composite
Structural composites
Mechanical behavior
title_short Fatigue behaviour study on repaired aramid fiber/epoxy composites
title_full Fatigue behaviour study on repaired aramid fiber/epoxy composites
title_fullStr Fatigue behaviour study on repaired aramid fiber/epoxy composites
title_full_unstemmed Fatigue behaviour study on repaired aramid fiber/epoxy composites
title_sort Fatigue behaviour study on repaired aramid fiber/epoxy composites
author Botelho,Edson Cocchieri
author_facet Botelho,Edson Cocchieri
Mazur,Rogério Lago
Costa,Michelle Leali
Cândido,Geraldo Maurício
Rezende,Mirabel Cerqueira
author_role author
author2 Mazur,Rogério Lago
Costa,Michelle Leali
Cândido,Geraldo Maurício
Rezende,Mirabel Cerqueira
author2_role author
author
author
author
dc.contributor.author.fl_str_mv Botelho,Edson Cocchieri
Mazur,Rogério Lago
Costa,Michelle Leali
Cândido,Geraldo Maurício
Rezende,Mirabel Cerqueira
dc.subject.por.fl_str_mv Fatigue behavior
Aramid/epoxy composite
Structural composites
Mechanical behavior
topic Fatigue behavior
Aramid/epoxy composite
Structural composites
Mechanical behavior
description Abstract: Aramid fiber reinforced polymer composites have been used in a wide variety of applications, such as aerospace, marine, sporting equipment and in the defense sector, due to their outstanding properties at low density. The most widely adopted procedure to investigate the repair of composites has been by repairing damages simulated in composite specimens. This work presents the structural repair influence on tensile and fatigue properties of a typical aramid fiber/epoxy composite used in the aerospace industry. According to this work, the aramid/epoxy composites with and without repair present tensile strength values of 618 and 680MPa, respectively, and tensile modulus of 26.5 and 30.1 GPa, respectively. Therefore, the fatigue results show that in loads higher than 170 MPa, both composites present a low life cycle (lower than 200,000 cycles) and the repaired aramid/epoxy composite presented low fatigue resistance in low and high cycle when compared with non-repaired composite. With these results, it is possible to observe a decrease of the measured mechanical properties of the repaired composites.
publishDate 2009
dc.date.none.fl_str_mv 2009-12-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462009000200217
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462009000200217
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.5028/jatm.2009.0102217221
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.1 n.2 2009
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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