Numerical model for the stress field ahead of a crack in elastoplastic regime

Detalhes bibliográficos
Autor(a) principal: Pascon, J. P.
Data de Publicação: 2019
Outros Autores: Torres, M. A.S. [UNESP], Baptista, C. A.R.P.
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://dx.doi.org/10.1016/j.prostr.2019.08.054
http://hdl.handle.net/11449/198098
Resumo: Damage-tolerant designs admit the pre-existence of defects and small cracks, which lead to stress redistribution in structural components. The accurate knowledge of the stress field in parts under these conditions is important for damage accumulation analysis and residual life prediction. In this work, a numerical model via finite elements is proposed to determine the stress field ahead of crack tips in a plate under cyclic loading and elastoplastic regime. The analyzed center-cracked plate simulates a M(T) specimen made of 6005-T6 extruded aluminum alloy. From the triple symmetry condition, one eighth of the plate was discretized with tetrahedral solid finite elements of quadratic order. The refinement of the mesh was concentrated around the crack tip region. The cyclic stress-strain curve of the material was experimentally obtained by strain-controlled fatigue tests. With this curve, elastic and plastic parameters have been determined, considering elastoplastic material with isotropic hardening governed by Swift's law. Such a model differs from most usual stress analyses in cracked components, in which the possibility of hardening is not considered. Cyclic loading with ratios R = 0 and R = -1 has been applied from an initial crack of 11 mm in length. The crack growth was imposed by means of a simplified node release scheme. The results showed no significant variation in terms of the equivalent stress, but considerable differences in the equivalent plastic strain. Therefore, the compressive phase in the specimen under R = -1 contributes to increase the equivalent plastic strain, which means that the level of yielding becomes higher even when the specimen is compressed.
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spelling Numerical model for the stress field ahead of a crack in elastoplastic regimeAluminum alloysFatigue cracksFinite Element MethodNumerical modellingDamage-tolerant designs admit the pre-existence of defects and small cracks, which lead to stress redistribution in structural components. The accurate knowledge of the stress field in parts under these conditions is important for damage accumulation analysis and residual life prediction. In this work, a numerical model via finite elements is proposed to determine the stress field ahead of crack tips in a plate under cyclic loading and elastoplastic regime. The analyzed center-cracked plate simulates a M(T) specimen made of 6005-T6 extruded aluminum alloy. From the triple symmetry condition, one eighth of the plate was discretized with tetrahedral solid finite elements of quadratic order. The refinement of the mesh was concentrated around the crack tip region. The cyclic stress-strain curve of the material was experimentally obtained by strain-controlled fatigue tests. With this curve, elastic and plastic parameters have been determined, considering elastoplastic material with isotropic hardening governed by Swift's law. Such a model differs from most usual stress analyses in cracked components, in which the possibility of hardening is not considered. Cyclic loading with ratios R = 0 and R = -1 has been applied from an initial crack of 11 mm in length. The crack growth was imposed by means of a simplified node release scheme. The results showed no significant variation in terms of the equivalent stress, but considerable differences in the equivalent plastic strain. Therefore, the compressive phase in the specimen under R = -1 contributes to increase the equivalent plastic strain, which means that the level of yielding becomes higher even when the specimen is compressed.Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Escola de Engenharia de Lorena University of São Paulo (EEL/USP)Engineering College São Paulo State University (FEG/UNESP)Engineering College São Paulo State University (FEG/UNESP)Universidade de São Paulo (USP)Universidade Estadual Paulista (Unesp)Pascon, J. P.Torres, M. A.S. [UNESP]Baptista, C. A.R.P.2020-12-12T00:59:05Z2020-12-12T00:59:05Z2019-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject411-418http://dx.doi.org/10.1016/j.prostr.2019.08.054Procedia Structural Integrity, v. 17, p. 411-418.2452-3216http://hdl.handle.net/11449/19809810.1016/j.prostr.2019.08.0542-s2.0-85074652330Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengProcedia Structural Integrityinfo:eu-repo/semantics/openAccess2021-10-23T08:39:01Zoai:repositorio.unesp.br:11449/198098Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462021-10-23T08:39:01Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Numerical model for the stress field ahead of a crack in elastoplastic regime
title Numerical model for the stress field ahead of a crack in elastoplastic regime
spellingShingle Numerical model for the stress field ahead of a crack in elastoplastic regime
Pascon, J. P.
Aluminum alloys
Fatigue cracks
Finite Element Method
Numerical modelling
title_short Numerical model for the stress field ahead of a crack in elastoplastic regime
title_full Numerical model for the stress field ahead of a crack in elastoplastic regime
title_fullStr Numerical model for the stress field ahead of a crack in elastoplastic regime
title_full_unstemmed Numerical model for the stress field ahead of a crack in elastoplastic regime
title_sort Numerical model for the stress field ahead of a crack in elastoplastic regime
author Pascon, J. P.
author_facet Pascon, J. P.
Torres, M. A.S. [UNESP]
Baptista, C. A.R.P.
author_role author
author2 Torres, M. A.S. [UNESP]
Baptista, C. A.R.P.
author2_role author
author
dc.contributor.none.fl_str_mv Universidade de São Paulo (USP)
Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Pascon, J. P.
Torres, M. A.S. [UNESP]
Baptista, C. A.R.P.
dc.subject.por.fl_str_mv Aluminum alloys
Fatigue cracks
Finite Element Method
Numerical modelling
topic Aluminum alloys
Fatigue cracks
Finite Element Method
Numerical modelling
description Damage-tolerant designs admit the pre-existence of defects and small cracks, which lead to stress redistribution in structural components. The accurate knowledge of the stress field in parts under these conditions is important for damage accumulation analysis and residual life prediction. In this work, a numerical model via finite elements is proposed to determine the stress field ahead of crack tips in a plate under cyclic loading and elastoplastic regime. The analyzed center-cracked plate simulates a M(T) specimen made of 6005-T6 extruded aluminum alloy. From the triple symmetry condition, one eighth of the plate was discretized with tetrahedral solid finite elements of quadratic order. The refinement of the mesh was concentrated around the crack tip region. The cyclic stress-strain curve of the material was experimentally obtained by strain-controlled fatigue tests. With this curve, elastic and plastic parameters have been determined, considering elastoplastic material with isotropic hardening governed by Swift's law. Such a model differs from most usual stress analyses in cracked components, in which the possibility of hardening is not considered. Cyclic loading with ratios R = 0 and R = -1 has been applied from an initial crack of 11 mm in length. The crack growth was imposed by means of a simplified node release scheme. The results showed no significant variation in terms of the equivalent stress, but considerable differences in the equivalent plastic strain. Therefore, the compressive phase in the specimen under R = -1 contributes to increase the equivalent plastic strain, which means that the level of yielding becomes higher even when the specimen is compressed.
publishDate 2019
dc.date.none.fl_str_mv 2019-01-01
2020-12-12T00:59:05Z
2020-12-12T00:59:05Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/conferenceObject
format conferenceObject
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.1016/j.prostr.2019.08.054
Procedia Structural Integrity, v. 17, p. 411-418.
2452-3216
http://hdl.handle.net/11449/198098
10.1016/j.prostr.2019.08.054
2-s2.0-85074652330
url http://dx.doi.org/10.1016/j.prostr.2019.08.054
http://hdl.handle.net/11449/198098
identifier_str_mv Procedia Structural Integrity, v. 17, p. 411-418.
2452-3216
10.1016/j.prostr.2019.08.054
2-s2.0-85074652330
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Procedia Structural Integrity
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
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dc.format.none.fl_str_mv 411-418
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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