Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters

Detalhes bibliográficos
Autor(a) principal: Borges, M. F.
Data de Publicação: 2021
Outros Autores: Lopez-Crespo, P., Antunes, F. V., Moreno, B., Prates, P., Camas, D., Neto, D. M.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
Texto Completo: http://hdl.handle.net/10773/32376
Resumo: In this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plastic CTOD range, Δδp. Experimental tests were performed on 12 mm thick CT specimens in order to obtain FCG rate and in cylindrical specimens to obtain stress–strain loops. A numerical analysis replicated the experimental work in terms of material, geometry and loading conditions, but assuming pure plane strain state, in order to obtain Δδp. The material parameters were fitted using the experimental stress–strain loops. The experimental work showed an increase of FCG rate with the increase of stress ratio from R = 0.1 to R = 0.7 mm, which indicated the existence of the crack closure phenomenon. However, the analysis of the position of the first node behind the crack tip showed that there is no crack closure under plane strain state, while a maximum value of 36% was found for plane stress state. Therefore, the surfaces influence FCG rate even in 12 mm thick specimens. A nearly linear relation was found between da/dN and Δδp. The comparison with other aluminium alloys showed that there is a significant influence of material on da/dN-Δδp relation. The change from plane strain to plane stress state decreased FCG rate due to crack closure. Under plane strain state there is a minor influence of stress ratio in the range R = 0.1–0.7, also because there is no crack closure. Finally, a comparison was made between plastic CTOD and cumulative plastic strain at the crack tip. Well defined relations were found, showing that both parameters can be used to quantify crack tip deformation.
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spelling Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parametersFatigue crack growth (FCG)Crack tip opening displacement (CTOD)Cyclic plastic behaviourAluminium alloyIn this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plastic CTOD range, Δδp. Experimental tests were performed on 12 mm thick CT specimens in order to obtain FCG rate and in cylindrical specimens to obtain stress–strain loops. A numerical analysis replicated the experimental work in terms of material, geometry and loading conditions, but assuming pure plane strain state, in order to obtain Δδp. The material parameters were fitted using the experimental stress–strain loops. The experimental work showed an increase of FCG rate with the increase of stress ratio from R = 0.1 to R = 0.7 mm, which indicated the existence of the crack closure phenomenon. However, the analysis of the position of the first node behind the crack tip showed that there is no crack closure under plane strain state, while a maximum value of 36% was found for plane stress state. Therefore, the surfaces influence FCG rate even in 12 mm thick specimens. A nearly linear relation was found between da/dN and Δδp. The comparison with other aluminium alloys showed that there is a significant influence of material on da/dN-Δδp relation. The change from plane strain to plane stress state decreased FCG rate due to crack closure. Under plane strain state there is a minor influence of stress ratio in the range R = 0.1–0.7, also because there is no crack closure. Finally, a comparison was made between plastic CTOD and cumulative plastic strain at the crack tip. Well defined relations were found, showing that both parameters can be used to quantify crack tip deformation.Elsevier2021-10-14T14:29:21Z2021-12-01T00:00:00Z2021-12info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttp://hdl.handle.net/10773/32376eng0142-112310.1016/j.ijfatigue.2021.106478Borges, M. F.Lopez-Crespo, P.Antunes, F. V.Moreno, B.Prates, P.Camas, D.Neto, D. M.info:eu-repo/semantics/openAccessreponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãoinstacron:RCAAP2024-02-22T12:02:24Zoai:ria.ua.pt:10773/32376Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-20T03:04:03.295801Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãofalse
dc.title.none.fl_str_mv Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
title Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
spellingShingle Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
Borges, M. F.
Fatigue crack growth (FCG)
Crack tip opening displacement (CTOD)
Cyclic plastic behaviour
Aluminium alloy
title_short Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
title_full Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
title_fullStr Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
title_full_unstemmed Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
title_sort Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters
author Borges, M. F.
author_facet Borges, M. F.
Lopez-Crespo, P.
Antunes, F. V.
Moreno, B.
Prates, P.
Camas, D.
Neto, D. M.
author_role author
author2 Lopez-Crespo, P.
Antunes, F. V.
Moreno, B.
Prates, P.
Camas, D.
Neto, D. M.
author2_role author
author
author
author
author
author
dc.contributor.author.fl_str_mv Borges, M. F.
Lopez-Crespo, P.
Antunes, F. V.
Moreno, B.
Prates, P.
Camas, D.
Neto, D. M.
dc.subject.por.fl_str_mv Fatigue crack growth (FCG)
Crack tip opening displacement (CTOD)
Cyclic plastic behaviour
Aluminium alloy
topic Fatigue crack growth (FCG)
Crack tip opening displacement (CTOD)
Cyclic plastic behaviour
Aluminium alloy
description In this work, fatigue crack growth (FCG) in the 2024-T351 aluminium alloy is studied using the plastic CTOD range, Δδp. Experimental tests were performed on 12 mm thick CT specimens in order to obtain FCG rate and in cylindrical specimens to obtain stress–strain loops. A numerical analysis replicated the experimental work in terms of material, geometry and loading conditions, but assuming pure plane strain state, in order to obtain Δδp. The material parameters were fitted using the experimental stress–strain loops. The experimental work showed an increase of FCG rate with the increase of stress ratio from R = 0.1 to R = 0.7 mm, which indicated the existence of the crack closure phenomenon. However, the analysis of the position of the first node behind the crack tip showed that there is no crack closure under plane strain state, while a maximum value of 36% was found for plane stress state. Therefore, the surfaces influence FCG rate even in 12 mm thick specimens. A nearly linear relation was found between da/dN and Δδp. The comparison with other aluminium alloys showed that there is a significant influence of material on da/dN-Δδp relation. The change from plane strain to plane stress state decreased FCG rate due to crack closure. Under plane strain state there is a minor influence of stress ratio in the range R = 0.1–0.7, also because there is no crack closure. Finally, a comparison was made between plastic CTOD and cumulative plastic strain at the crack tip. Well defined relations were found, showing that both parameters can be used to quantify crack tip deformation.
publishDate 2021
dc.date.none.fl_str_mv 2021-10-14T14:29:21Z
2021-12-01T00:00:00Z
2021-12
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
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status_str publishedVersion
dc.identifier.uri.fl_str_mv http://hdl.handle.net/10773/32376
url http://hdl.handle.net/10773/32376
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 0142-1123
10.1016/j.ijfatigue.2021.106478
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
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dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv Elsevier
publisher.none.fl_str_mv Elsevier
dc.source.none.fl_str_mv reponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
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