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...
| Autores: | , , , |
|---|---|
| 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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España |
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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/ |
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info:eu-repo/semantics/openAccess |
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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/ |
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openAccess |
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application/pdf application/pdf |
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Elsevier |
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Elsevier |
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reponame:RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia instname:Universitat Politècnica de València (UPV) |
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Universitat Politècnica de València (UPV) |
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RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia |
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RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia |
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1869406331402715136 |
| 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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15,301603 |