Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers

Detalhes bibliográficos
Autor(a) principal: Shiino, Marcos Yutaka [UNESP]
Data de Publicação: 2018
Outros Autores: de Siqueira, Guilherme Silva Moraes [UNESP], Cioffi, Maria Odila Hilário [UNESP], Montoro, Sérgio Roberto, Donadon, Maurício Vicente
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1007/s11665-018-3584-3
http://hdl.handle.net/11449/189828
Resumo: The aeronautic structures normally operate under high levels of hygroscopic moisture from the surrounding environment at different temperature ranges while in service. Under such conditions, the behavior of laminate composite submitted to cyclic or static loadings can change drastically. In order to understand those effects in stitched fabrics, fatigue tests with open-hole specimens were carried out with a stress ratio of R = −1 and R = 0.1. The specimens were fatigue-tested as provided (environmental conditions) and after exposed to hygrothermal weathering conditions. Based on evidences from recent studies available in the open literature, e.g., effect of water diffusion on epoxy matrix, the overall results indicated a significant reduction in stiffness after the specimens are exposed to hygrothermal effects. The reduction in matrix stiffness, in this case, enhanced the fatigue strength in tension–tension load (R = 0.1) when compared to the specimens in normal conditions. The opposite occurs for the specimens loaded with stress ratio of R = −1, in which the delamination mechanisms changed during the loading reversion from tension to compression that promoted early delamination. Therefore, this process reduced the fatigue life of the specimens under hygrothermal condition. Then, by fractographic investigation, it was verified fracture patterns that regard to mode II damage in R = −1, in which mode II fracture toughness is known to decrease in the presence of water molecules.
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spelling Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibersfatiguehygrothermallaminatenon-crimp fabricThe aeronautic structures normally operate under high levels of hygroscopic moisture from the surrounding environment at different temperature ranges while in service. Under such conditions, the behavior of laminate composite submitted to cyclic or static loadings can change drastically. In order to understand those effects in stitched fabrics, fatigue tests with open-hole specimens were carried out with a stress ratio of R = −1 and R = 0.1. The specimens were fatigue-tested as provided (environmental conditions) and after exposed to hygrothermal weathering conditions. Based on evidences from recent studies available in the open literature, e.g., effect of water diffusion on epoxy matrix, the overall results indicated a significant reduction in stiffness after the specimens are exposed to hygrothermal effects. The reduction in matrix stiffness, in this case, enhanced the fatigue strength in tension–tension load (R = 0.1) when compared to the specimens in normal conditions. The opposite occurs for the specimens loaded with stress ratio of R = −1, in which the delamination mechanisms changed during the loading reversion from tension to compression that promoted early delamination. Therefore, this process reduced the fatigue life of the specimens under hygrothermal condition. Then, by fractographic investigation, it was verified fracture patterns that regard to mode II damage in R = −1, in which mode II fracture toughness is known to decrease in the presence of water molecules.Universidade Estadual Paulista (Unesp) - Instituto de Ciência e TecnologiaIEAMar/UNESP - Instituto de Estudos Avançados do MarDepartamento de Materiais e Tecnologia Fatigue and Aeronautic Materials Research Group Faculdade de Engenharia Universidade Estadual Paulista (Unesp)Fatec-Faculdade de Tecnologia de Pindamonhangaba, Caixa Postal 1Divisão de Engenharia Aeronáutica Instituto Tecnológico da Aeronáutica - ITA, Praça Marechal do Ar Eduardo Gomes, Vila das AcáciasUniversidade Estadual Paulista (Unesp) - Instituto de Ciência e TecnologiaIEAMar/UNESP - Instituto de Estudos Avançados do MarDepartamento de Materiais e Tecnologia Fatigue and Aeronautic Materials Research Group Faculdade de Engenharia Universidade Estadual Paulista (Unesp)Universidade Estadual Paulista (Unesp)Fatec-Faculdade de Tecnologia de PindamonhangabaInstituto Tecnológico da Aeronáutica - ITAShiino, Marcos Yutaka [UNESP]de Siqueira, Guilherme Silva Moraes [UNESP]Cioffi, Maria Odila Hilário [UNESP]Montoro, Sérgio RobertoDonadon, Maurício Vicente2019-10-06T16:53:29Z2019-10-06T16:53:29Z2018-11-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/article5964-5972http://dx.doi.org/10.1007/s11665-018-3584-3Journal of Materials Engineering and Performance, v. 27, n. 11, p. 5964-5972, 2018.1544-10241059-9495http://hdl.handle.net/11449/18982810.1007/s11665-018-3584-32-s2.0-85055274258216095752915102521609575291510256119671014416126Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengJournal of Materials Engineering and Performanceinfo:eu-repo/semantics/openAccess2024-07-02T15:03:34Zoai:repositorio.unesp.br:11449/189828Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-07-02T15:03:34Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
title Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
spellingShingle Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
Shiino, Marcos Yutaka [UNESP]
fatigue
hygrothermal
laminate
non-crimp fabric
title_short Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
title_full Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
title_fullStr Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
title_full_unstemmed Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
title_sort Hygrothermal Effect on Composites Under In-Plane Fatigue at Stress Ratios of R = −1 and R = 0.1: An Analysis of Quasi-Isotropic Stitched Carbon Fibers
author Shiino, Marcos Yutaka [UNESP]
author_facet Shiino, Marcos Yutaka [UNESP]
de Siqueira, Guilherme Silva Moraes [UNESP]
Cioffi, Maria Odila Hilário [UNESP]
Montoro, Sérgio Roberto
Donadon, Maurício Vicente
author_role author
author2 de Siqueira, Guilherme Silva Moraes [UNESP]
Cioffi, Maria Odila Hilário [UNESP]
Montoro, Sérgio Roberto
Donadon, Maurício Vicente
author2_role author
author
author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (Unesp)
Fatec-Faculdade de Tecnologia de Pindamonhangaba
Instituto Tecnológico da Aeronáutica - ITA
dc.contributor.author.fl_str_mv Shiino, Marcos Yutaka [UNESP]
de Siqueira, Guilherme Silva Moraes [UNESP]
Cioffi, Maria Odila Hilário [UNESP]
Montoro, Sérgio Roberto
Donadon, Maurício Vicente
dc.subject.por.fl_str_mv fatigue
hygrothermal
laminate
non-crimp fabric
topic fatigue
hygrothermal
laminate
non-crimp fabric
description The aeronautic structures normally operate under high levels of hygroscopic moisture from the surrounding environment at different temperature ranges while in service. Under such conditions, the behavior of laminate composite submitted to cyclic or static loadings can change drastically. In order to understand those effects in stitched fabrics, fatigue tests with open-hole specimens were carried out with a stress ratio of R = −1 and R = 0.1. The specimens were fatigue-tested as provided (environmental conditions) and after exposed to hygrothermal weathering conditions. Based on evidences from recent studies available in the open literature, e.g., effect of water diffusion on epoxy matrix, the overall results indicated a significant reduction in stiffness after the specimens are exposed to hygrothermal effects. The reduction in matrix stiffness, in this case, enhanced the fatigue strength in tension–tension load (R = 0.1) when compared to the specimens in normal conditions. The opposite occurs for the specimens loaded with stress ratio of R = −1, in which the delamination mechanisms changed during the loading reversion from tension to compression that promoted early delamination. Therefore, this process reduced the fatigue life of the specimens under hygrothermal condition. Then, by fractographic investigation, it was verified fracture patterns that regard to mode II damage in R = −1, in which mode II fracture toughness is known to decrease in the presence of water molecules.
publishDate 2018
dc.date.none.fl_str_mv 2018-11-01
2019-10-06T16:53:29Z
2019-10-06T16:53:29Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.1007/s11665-018-3584-3
Journal of Materials Engineering and Performance, v. 27, n. 11, p. 5964-5972, 2018.
1544-1024
1059-9495
http://hdl.handle.net/11449/189828
10.1007/s11665-018-3584-3
2-s2.0-85055274258
2160957529151025
2160957529151025
6119671014416126
url http://dx.doi.org/10.1007/s11665-018-3584-3
http://hdl.handle.net/11449/189828
identifier_str_mv Journal of Materials Engineering and Performance, v. 27, n. 11, p. 5964-5972, 2018.
1544-1024
1059-9495
10.1007/s11665-018-3584-3
2-s2.0-85055274258
2160957529151025
6119671014416126
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Journal of Materials Engineering and Performance
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 5964-5972
dc.source.none.fl_str_mv Scopus
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv
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