Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM

[EN] In the present research work, a numerical crack growth analysis using linear elastic fracture mechanics is carried out paying attention to the crack paths that grow in the central part of cruciform specimens under biaxial fatigue loads. The crack propagation in this type of specimens has been s...

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Autores: Infante, Diego, Qian, Guian, Miguélez, María Henar, Giner Maravilla, Eugenio|||0000-0003-1903-6495
Tipo de recurso: artículo
Fecha de publicación:2019
País:España
Institución:Universitat Politècnica de València (UPV)
Repositorio:RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
Idioma:inglés
OAI Identifier:oai:riunet.upv.es:10251/157577
Acceso en línea:https://riunet.upv.es/handle/10251/157577
Access Level:acceso abierto
Palabra clave:XFEM
Cruciform specimen
Biaxial fatigue loading
Crack paths
INGENIERIA MECANICA
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dc.title.none.fl_str_mv Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
title Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
spellingShingle Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
Infante, Diego
XFEM
Cruciform specimen
Biaxial fatigue loading
Crack paths
INGENIERIA MECANICA
title_short Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
title_full Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
title_fullStr Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
title_full_unstemmed Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
title_sort Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM
dc.creator.none.fl_str_mv Infante, Diego
Qian, Guian
Miguélez, María Henar
Giner Maravilla, Eugenio|||0000-0003-1903-6495
author Infante, Diego
author_facet Infante, Diego
Qian, Guian
Miguélez, María Henar
Giner Maravilla, Eugenio|||0000-0003-1903-6495
author_role author
author2 Qian, Guian
Miguélez, María Henar
Giner Maravilla, Eugenio|||0000-0003-1903-6495
author2_role author
author
author
dc.contributor.none.fl_str_mv Escuela Técnica Superior de Ingeniería Aeroespacial y Diseño Industrial
Departamento de Ingeniería Mecánica y de Materiales
Instituto Universitario de Investigación Concertado de Ingeniería Mecánica y Biomecánica
Generalitat Valenciana
European Regional Development Fund
Ministerio de Economía y Competitividad
National Natural Science Foundation of China
Agencia Estatal de Investigación
Repositorio Institucional de la Universitat Politècnica de València Riunet
dc.subject.none.fl_str_mv XFEM
Cruciform specimen
Biaxial fatigue loading
Crack paths
INGENIERIA MECANICA
topic XFEM
Cruciform specimen
Biaxial fatigue loading
Crack paths
INGENIERIA MECANICA
description [EN] In the present research work, a numerical crack growth analysis using linear elastic fracture mechanics is carried out paying attention to the crack paths that grow in the central part of cruciform specimens under biaxial fatigue loads. The crack propagation in this type of specimens has been studied using the extended finite element method (XFEM). The objective is to analyse the effect of different phase angles under biaxial fatigue loads and to assess the different orientation criteria for nonproportional loading, benefiting from the advantages of XFEM. The crack path and the stress intensity factor range of a crack either aligned or inclined to the load directions have been investigated using different crack orientation criteria. Symmetrical branching is predicted for an initial crack inclined at 45 degrees with phase angle of loading equal to 90 degrees and 180 degrees. Numerical results are in good agreement with the experimental observations found in the literature, although the study reveals important differences in the crack path predictions depending on the orientation criteria.
publishDate 2019
dc.date.none.fl_str_mv 2019
2019-06-01
dc.type.none.fl_str_mv journal article
http://purl.org/coar/resource_type/c_6501
VoR
http://purl.org/coar/version/c_970fb48d4fbd8a85
dc.type.openaire.fl_str_mv info:eu-repo/semantics/article
format article
dc.identifier.none.fl_str_mv https://riunet.upv.es/handle/10251/157577
url https://riunet.upv.es/handle/10251/157577
dc.language.none.fl_str_mv Inglés
eng
language_invalid_str_mv Inglés
language eng
dc.relation.none.fl_str_mv Ministerio de Economía y Competitividad http://dx.doi.org/10.13039/501100003329 DPI2014-56137-C2-2-R OPTIMIZACION DE PROCESOS DE ACABADO DE COMPONENTES CRITICOS DE AERO-REACTORES
Ministerio de Economía y Competitividad http://dx.doi.org/10.13039/501100003329 BES-2015-072070 BES-2015-072070
Agencia Estatal de Investigación http://dx.doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016 DPI2017-89197-C2-1-R TALADRADO DE COMPONENTES HIBRIDOS CFRPS%2FTI Y TOLERANCIA AL DAÑO DEBIDO A MECANIZADO DURANTE EL COMPORTAMIENTO EN SERVICIO DE UNIONES ESTRUCTURALES AERONAUTICAS
Agencia Estatal de Investigación http://dx.doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016 DPI2017-89197-C2-2-R TALADRADO DE COMPONENTES HIBRIDOS CFRPS%2FTI Y TOLERANCIA AL DAÑO DEBIDO A MECANIZADO DURANTE EL COMPORTAMIENTO EN SERVICIO DE UNIONES ESTRUCTURALES AERONAUTICAS
National Natural Science Foundation of China https://doi.org/10.13039/501100001809 11872364
Generalitat Valenciana https://doi.org/10.13039/501100003359 PROMETEO%2F2016%2F007 Modelado numérico avanzado en ingeniería mecánica
dc.rights.none.fl_str_mv open access
http://purl.org/coar/access_right/c_abf2
Reconocimiento - No comercial - Sin obra derivada (by-nc-nd)
http://creativecommons.org/licenses/by-nc-nd/4.0/
dc.rights.openaire.fl_str_mv info:eu-repo/semantics/openAccess
rights_invalid_str_mv open access
http://purl.org/coar/access_right/c_abf2
Reconocimiento - No comercial - Sin obra derivada (by-nc-nd)
http://creativecommons.org/licenses/by-nc-nd/4.0/
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
application/pdf
dc.publisher.none.fl_str_mv Elsevier
publisher.none.fl_str_mv Elsevier
dc.source.none.fl_str_mv reponame:RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
instname:Universitat Politècnica de València (UPV)
instname_str Universitat Politècnica de València (UPV)
reponame_str RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
collection RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
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spelling Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEMInfante, DiegoQian, GuianMiguélez, María HenarGiner Maravilla, Eugenio|||0000-0003-1903-6495XFEMCruciform specimenBiaxial fatigue loadingCrack pathsINGENIERIA MECANICA[EN] In the present research work, a numerical crack growth analysis using linear elastic fracture mechanics is carried out paying attention to the crack paths that grow in the central part of cruciform specimens under biaxial fatigue loads. The crack propagation in this type of specimens has been studied using the extended finite element method (XFEM). The objective is to analyse the effect of different phase angles under biaxial fatigue loads and to assess the different orientation criteria for nonproportional loading, benefiting from the advantages of XFEM. The crack path and the stress intensity factor range of a crack either aligned or inclined to the load directions have been investigated using different crack orientation criteria. Symmetrical branching is predicted for an initial crack inclined at 45 degrees with phase angle of loading equal to 90 degrees and 180 degrees. Numerical results are in good agreement with the experimental observations found in the literature, although the study reveals important differences in the crack path predictions depending on the orientation criteria.The authors gratefully acknowledge the financial support given by the Spanish Ministry of Economy and Competitiveness and the FEDER program through the project DPI2017-89197-C2-1-R, DPI2017-89197-C2-2-R and DPI2014-56137-C2-2-11 and the FPI subprogram associated to the project with the reference BES-2015-072070. The support of the Generalitat Valenciana, Programme PROMETEO 2016/007, is also acknowledged. Guian Qian is grateful for the financial support by the National Natural Science Foundation of China (No.11872364).ElsevierEscuela Técnica Superior de Ingeniería Aeroespacial y Diseño IndustrialDepartamento de Ingeniería Mecánica y de MaterialesInstituto Universitario de Investigación Concertado de Ingeniería Mecánica y BiomecánicaGeneralitat ValencianaEuropean Regional Development FundMinisterio de Economía y CompetitividadNational Natural Science Foundation of ChinaAgencia Estatal de InvestigaciónRepositorio Institucional de la Universitat Politècnica de València Riunet20192019-06-01journal articlehttp://purl.org/coar/resource_type/c_6501VoRhttp://purl.org/coar/version/c_970fb48d4fbd8a85info:eu-repo/semantics/articleapplication/pdfapplication/pdfhttps://riunet.upv.es/handle/10251/157577reponame:RiuNet. Repositorio Institucional de la Universitat Politécnica de Valénciainstname:Universitat Politècnica de València (UPV)InglésengMinisterio de Economía y Competitividad http://dx.doi.org/10.13039/501100003329 DPI2014-56137-C2-2-R OPTIMIZACION DE PROCESOS DE ACABADO DE COMPONENTES CRITICOS DE AERO-REACTORESMinisterio de Economía y Competitividad http://dx.doi.org/10.13039/501100003329 BES-2015-072070 BES-2015-072070Agencia Estatal de Investigación http://dx.doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016 DPI2017-89197-C2-1-R TALADRADO DE COMPONENTES HIBRIDOS CFRPS%2FTI Y TOLERANCIA AL DAÑO DEBIDO A MECANIZADO DURANTE EL COMPORTAMIENTO EN SERVICIO DE UNIONES ESTRUCTURALES AERONAUTICASAgencia Estatal de Investigación http://dx.doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016 DPI2017-89197-C2-2-R TALADRADO DE COMPONENTES HIBRIDOS CFRPS%2FTI Y TOLERANCIA AL DAÑO DEBIDO A MECANIZADO DURANTE EL COMPORTAMIENTO EN SERVICIO DE UNIONES ESTRUCTURALES AERONAUTICASNational Natural Science Foundation of China https://doi.org/10.13039/501100001809 11872364Generalitat Valenciana https://doi.org/10.13039/501100003359 PROMETEO%2F2016%2F007 Modelado numérico avanzado en ingeniería mecánicaopen accesshttp://purl.org/coar/access_right/c_abf2Reconocimiento - No comercial - Sin obra derivada (by-nc-nd) http://creativecommons.org/licenses/by-nc-nd/4.0/info:eu-repo/semantics/openAccessoai:riunet.upv.es:10251/1575772026-06-13T07:49:27Z
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