An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings

Detalhes bibliográficos
Autor(a) principal: Baptista, Ricardo
Data de Publicação: 2019
Outros Autores: Infante, V., Freitas, 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/10400.26/29707
Resumo: Fatigue is still one of the main concerns when dealing with mechanical components failure. While it is fundamental to experimentally determine the fatigue material behavior using standard specimens, testing large and complex component geometries can be complicated. In these cases, the Finite Element Method can be a cost-effective solution but developing fatigue crack growth models is still a complicated task. In order to solve this problem, an algorithm for automatic crack propagation was developed. Using three different modules, the algorithm can generate a complex Finite Element Method model including a fatigue crack; solve this model considering complex loading conditions, by applying the superposition method; and calculate the fatigue crack propagation rate, using it to update the original model. In order to benchmark this solution two different problems were analyzed, a modified compact tension specimen and a cruciform specimen. By modifying the compact tension specimen hole location and simulating an initial crack, it was possible to understand how mixed mode conditions influence the fatigue crack path. Different load ratios and initial crack directions on the cruciform specimen were analyzed. Increasing the load ratio will increase the crack deflecting angle. The obtain solutions were compared with experimental results, showing good agreement. Therefore the developed algorithm can be used to predict the fatigue crack growth behavior on complex geometries and when different types of loads are applied to the component.
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spelling An algorithm for fatigue crack growth applied to mixed and biaxial mode loadingsFatigueCrack propagationMixed modeAutomatic algorithmFatigue is still one of the main concerns when dealing with mechanical components failure. While it is fundamental to experimentally determine the fatigue material behavior using standard specimens, testing large and complex component geometries can be complicated. In these cases, the Finite Element Method can be a cost-effective solution but developing fatigue crack growth models is still a complicated task. In order to solve this problem, an algorithm for automatic crack propagation was developed. Using three different modules, the algorithm can generate a complex Finite Element Method model including a fatigue crack; solve this model considering complex loading conditions, by applying the superposition method; and calculate the fatigue crack propagation rate, using it to update the original model. In order to benchmark this solution two different problems were analyzed, a modified compact tension specimen and a cruciform specimen. By modifying the compact tension specimen hole location and simulating an initial crack, it was possible to understand how mixed mode conditions influence the fatigue crack path. Different load ratios and initial crack directions on the cruciform specimen were analyzed. Increasing the load ratio will increase the crack deflecting angle. The obtain solutions were compared with experimental results, showing good agreement. Therefore the developed algorithm can be used to predict the fatigue crack growth behavior on complex geometries and when different types of loads are applied to the component.Repositório ComumBaptista, RicardoInfante, V.Freitas, M.2019-09-16T13:51:21Z20192019-01-01T00:00:00Zinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttp://hdl.handle.net/10400.26/29707eng2452-321610.1016/j.prostr.2019.08.073info: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:RCAAP2023-11-21T09:55:13Zoai:comum.rcaap.pt:10400.26/29707Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-19T23:10:58.658741Repositório 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 An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
title An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
spellingShingle An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
Baptista, Ricardo
Fatigue
Crack propagation
Mixed mode
Automatic algorithm
title_short An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
title_full An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
title_fullStr An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
title_full_unstemmed An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
title_sort An algorithm for fatigue crack growth applied to mixed and biaxial mode loadings
author Baptista, Ricardo
author_facet Baptista, Ricardo
Infante, V.
Freitas, M.
author_role author
author2 Infante, V.
Freitas, M.
author2_role author
author
dc.contributor.none.fl_str_mv Repositório Comum
dc.contributor.author.fl_str_mv Baptista, Ricardo
Infante, V.
Freitas, M.
dc.subject.por.fl_str_mv Fatigue
Crack propagation
Mixed mode
Automatic algorithm
topic Fatigue
Crack propagation
Mixed mode
Automatic algorithm
description Fatigue is still one of the main concerns when dealing with mechanical components failure. While it is fundamental to experimentally determine the fatigue material behavior using standard specimens, testing large and complex component geometries can be complicated. In these cases, the Finite Element Method can be a cost-effective solution but developing fatigue crack growth models is still a complicated task. In order to solve this problem, an algorithm for automatic crack propagation was developed. Using three different modules, the algorithm can generate a complex Finite Element Method model including a fatigue crack; solve this model considering complex loading conditions, by applying the superposition method; and calculate the fatigue crack propagation rate, using it to update the original model. In order to benchmark this solution two different problems were analyzed, a modified compact tension specimen and a cruciform specimen. By modifying the compact tension specimen hole location and simulating an initial crack, it was possible to understand how mixed mode conditions influence the fatigue crack path. Different load ratios and initial crack directions on the cruciform specimen were analyzed. Increasing the load ratio will increase the crack deflecting angle. The obtain solutions were compared with experimental results, showing good agreement. Therefore the developed algorithm can be used to predict the fatigue crack growth behavior on complex geometries and when different types of loads are applied to the component.
publishDate 2019
dc.date.none.fl_str_mv 2019-09-16T13:51:21Z
2019
2019-01-01T00:00:00Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
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status_str publishedVersion
dc.identifier.uri.fl_str_mv http://hdl.handle.net/10400.26/29707
url http://hdl.handle.net/10400.26/29707
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 2452-3216
10.1016/j.prostr.2019.08.073
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dc.format.none.fl_str_mv application/pdf
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