Fatigue behaviour study on repaired aramid fiber/epoxy composites
Autor(a) principal: | |
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Data de Publicação: | 2009 |
Outros Autores: | , , , |
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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Journal of Aerospace Technology and Management (Online) |
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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 |
_version_ |
1754732530372706304 |