Mixed-mode fatigue crack growth behaviour in aluminium alloy

Detalhes bibliográficos
Autor(a) principal: Borrego, L. P.
Data de Publicação: 2006
Outros Autores: Antunes, F. V., Costa, J. M., Ferreira, J. 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/10316/4228
https://doi.org/10.1016/j.ijfatigue.2005.07.047
Resumo: Fatigue crack propagation tests in compact mixed-mode specimens were carried out for several stress intensity ratios of mode I and mode II, KI/KII, in AlMgSi1-T6 aluminium alloy with 3 mm thickness. The tests were performed in a standard servo-hydraulic machine. A linkage system was developed in order to permit the variation of the KI/KII ratio by changing the loading angle. Crack closure loads were obtained through the compliance technique. A finite element analysis was also done in order to obtain the KI and KII values for the different loading angles. Crack closure increases under mixed-mode loading conditions in comparison to mode-I loading due the friction between the crack tip surfaces. Moreover, the crack closure level increases with the KI/KII ratio decrease. Correlations of the equivalent values of the effective stress intensity factor with the crack growth rates are also performed. Finally, an elastic-plastic finite element analysis was performed to obtain the plastic zones sizes and shapes and model the effect of mixed-mode loading on crack closure.
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spelling Mixed-mode fatigue crack growth behaviour in aluminium alloyAluminium alloyMixed-mode loadingFatigue crack propagationCrack closureFatigue crack propagation tests in compact mixed-mode specimens were carried out for several stress intensity ratios of mode I and mode II, KI/KII, in AlMgSi1-T6 aluminium alloy with 3 mm thickness. The tests were performed in a standard servo-hydraulic machine. A linkage system was developed in order to permit the variation of the KI/KII ratio by changing the loading angle. Crack closure loads were obtained through the compliance technique. A finite element analysis was also done in order to obtain the KI and KII values for the different loading angles. Crack closure increases under mixed-mode loading conditions in comparison to mode-I loading due the friction between the crack tip surfaces. Moreover, the crack closure level increases with the KI/KII ratio decrease. Correlations of the equivalent values of the effective stress intensity factor with the crack growth rates are also performed. Finally, an elastic-plastic finite element analysis was performed to obtain the plastic zones sizes and shapes and model the effect of mixed-mode loading on crack closure.http://www.sciencedirect.com/science/article/B6V35-4HTCTR7-4/1/5c13c025a6dddc4a05eba614cf4759dc2006info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleaplication/PDFhttp://hdl.handle.net/10316/4228http://hdl.handle.net/10316/4228https://doi.org/10.1016/j.ijfatigue.2005.07.047engInternational Journal of Fatigue. 28:5-6 (2006) 618-626Borrego, L. P.Antunes, F. V.Costa, J. M.Ferreira, J. 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:RCAAP2020-11-06T16:49:07Zoai:estudogeral.uc.pt:10316/4228Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-19T20:58:26.793240Repositório 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 Mixed-mode fatigue crack growth behaviour in aluminium alloy
title Mixed-mode fatigue crack growth behaviour in aluminium alloy
spellingShingle Mixed-mode fatigue crack growth behaviour in aluminium alloy
Borrego, L. P.
Aluminium alloy
Mixed-mode loading
Fatigue crack propagation
Crack closure
title_short Mixed-mode fatigue crack growth behaviour in aluminium alloy
title_full Mixed-mode fatigue crack growth behaviour in aluminium alloy
title_fullStr Mixed-mode fatigue crack growth behaviour in aluminium alloy
title_full_unstemmed Mixed-mode fatigue crack growth behaviour in aluminium alloy
title_sort Mixed-mode fatigue crack growth behaviour in aluminium alloy
author Borrego, L. P.
author_facet Borrego, L. P.
Antunes, F. V.
Costa, J. M.
Ferreira, J. M.
author_role author
author2 Antunes, F. V.
Costa, J. M.
Ferreira, J. M.
author2_role author
author
author
dc.contributor.author.fl_str_mv Borrego, L. P.
Antunes, F. V.
Costa, J. M.
Ferreira, J. M.
dc.subject.por.fl_str_mv Aluminium alloy
Mixed-mode loading
Fatigue crack propagation
Crack closure
topic Aluminium alloy
Mixed-mode loading
Fatigue crack propagation
Crack closure
description Fatigue crack propagation tests in compact mixed-mode specimens were carried out for several stress intensity ratios of mode I and mode II, KI/KII, in AlMgSi1-T6 aluminium alloy with 3 mm thickness. The tests were performed in a standard servo-hydraulic machine. A linkage system was developed in order to permit the variation of the KI/KII ratio by changing the loading angle. Crack closure loads were obtained through the compliance technique. A finite element analysis was also done in order to obtain the KI and KII values for the different loading angles. Crack closure increases under mixed-mode loading conditions in comparison to mode-I loading due the friction between the crack tip surfaces. Moreover, the crack closure level increases with the KI/KII ratio decrease. Correlations of the equivalent values of the effective stress intensity factor with the crack growth rates are also performed. Finally, an elastic-plastic finite element analysis was performed to obtain the plastic zones sizes and shapes and model the effect of mixed-mode loading on crack closure.
publishDate 2006
dc.date.none.fl_str_mv 2006
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dc.identifier.uri.fl_str_mv http://hdl.handle.net/10316/4228
http://hdl.handle.net/10316/4228
https://doi.org/10.1016/j.ijfatigue.2005.07.047
url http://hdl.handle.net/10316/4228
https://doi.org/10.1016/j.ijfatigue.2005.07.047
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv International Journal of Fatigue. 28:5-6 (2006) 618-626
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