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Fatigue life prediction of cracked attachment lugs using XFEM
•Stress intensity factor estimation in attachment lugs.•Extended finite element method to calculate SIF in attachment lugs.•Fatigue life estimation and crack growth in straight lugs. In the present paper, a three dimensional finite element method (FEM) is used to compute the stress intensity factor...
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Published in: | International journal of fatigue 2015-08, Vol.77, p.186-193 |
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container_title | International journal of fatigue |
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creator | Naderi, M. Iyyer, N. |
description | •Stress intensity factor estimation in attachment lugs.•Extended finite element method to calculate SIF in attachment lugs.•Fatigue life estimation and crack growth in straight lugs.
In the present paper, a three dimensional finite element method (FEM) is used to compute the stress intensity factor (SIF) in straight lugs of Aluminum 7075-T6. Extended finite element method (XFEM) capability available in ABAQUS is used to calculate the stress intensity factor. Crack growth and fatigue life of single through-thickness and single quarter elliptical corner cracks in attachment lug are estimated and then compared with the available experimental data for two different load ratios equal to 0.1 and 0.5. The SIF calculated from XFEM shows that the introduction of different loading boundary conditions significantly affect the estimated fatigue life. |
doi_str_mv | 10.1016/j.ijfatigue.2015.02.021 |
format | article |
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In the present paper, a three dimensional finite element method (FEM) is used to compute the stress intensity factor (SIF) in straight lugs of Aluminum 7075-T6. Extended finite element method (XFEM) capability available in ABAQUS is used to calculate the stress intensity factor. Crack growth and fatigue life of single through-thickness and single quarter elliptical corner cracks in attachment lug are estimated and then compared with the available experimental data for two different load ratios equal to 0.1 and 0.5. The SIF calculated from XFEM shows that the introduction of different loading boundary conditions significantly affect the estimated fatigue life.</description><identifier>ISSN: 0142-1123</identifier><identifier>EISSN: 1879-3452</identifier><identifier>DOI: 10.1016/j.ijfatigue.2015.02.021</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Attachment ; Attachment lugs ; Crack propagation ; Extended finite element method ; Fatigue life ; Finite element method ; Lugs ; Mathematical analysis ; Mathematical models ; Stress intensity factor</subject><ispartof>International journal of fatigue, 2015-08, Vol.77, p.186-193</ispartof><rights>2015 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c418t-6e0c2a8f5f538798928637096207920eaf184125c18c98134498647631b6ac753</citedby><cites>FETCH-LOGICAL-c418t-6e0c2a8f5f538798928637096207920eaf184125c18c98134498647631b6ac753</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27898,27899</link.rule.ids></links><search><creatorcontrib>Naderi, M.</creatorcontrib><creatorcontrib>Iyyer, N.</creatorcontrib><title>Fatigue life prediction of cracked attachment lugs using XFEM</title><title>International journal of fatigue</title><description>•Stress intensity factor estimation in attachment lugs.•Extended finite element method to calculate SIF in attachment lugs.•Fatigue life estimation and crack growth in straight lugs.
In the present paper, a three dimensional finite element method (FEM) is used to compute the stress intensity factor (SIF) in straight lugs of Aluminum 7075-T6. Extended finite element method (XFEM) capability available in ABAQUS is used to calculate the stress intensity factor. Crack growth and fatigue life of single through-thickness and single quarter elliptical corner cracks in attachment lug are estimated and then compared with the available experimental data for two different load ratios equal to 0.1 and 0.5. The SIF calculated from XFEM shows that the introduction of different loading boundary conditions significantly affect the estimated fatigue life.</description><subject>Attachment</subject><subject>Attachment lugs</subject><subject>Crack propagation</subject><subject>Extended finite element method</subject><subject>Fatigue life</subject><subject>Finite element method</subject><subject>Lugs</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Stress intensity factor</subject><issn>0142-1123</issn><issn>1879-3452</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><recordid>eNqFkEFLxDAUhIMouK7-BnP00pqXJk1y8LAsrgorXhS8hZhN1tRuuyap4L-3S8WrMDCXmeG9D6FLICUQqK-bMjTe5LAdXEkJ8JLQUXCEZiCFKirG6TGaEWC0AKDVKTpLqSGEKCL4DN2spipug3d4H90m2Bz6Dvce22jsh9tgk7Ox7zvXZdwO24SHFLotfl3dPp6jE2_a5C5-fY5eVrfPy_ti_XT3sFysC8tA5qJ2xFIjPfe8Gm-Sisq6EkTVlAhFiTMeJAPKLUirJFSMKVkzUVfwVhsreDVHV9PuPvafg0tZ70Kyrm1N5_ohaRAgFeOg1BgVU9TGPqXovN7HsDPxWwPRB2C60X_A9AGYJnQUjM3F1HTjJ1_BRZ1scJ0dkURns9704d-NHwQhdcw</recordid><startdate>20150801</startdate><enddate>20150801</enddate><creator>Naderi, M.</creator><creator>Iyyer, N.</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>20150801</creationdate><title>Fatigue life prediction of cracked attachment lugs using XFEM</title><author>Naderi, M. ; Iyyer, N.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c418t-6e0c2a8f5f538798928637096207920eaf184125c18c98134498647631b6ac753</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Attachment</topic><topic>Attachment lugs</topic><topic>Crack propagation</topic><topic>Extended finite element method</topic><topic>Fatigue life</topic><topic>Finite element method</topic><topic>Lugs</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Stress intensity factor</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Naderi, M.</creatorcontrib><creatorcontrib>Iyyer, N.</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>International journal of fatigue</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Naderi, M.</au><au>Iyyer, N.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fatigue life prediction of cracked attachment lugs using XFEM</atitle><jtitle>International journal of fatigue</jtitle><date>2015-08-01</date><risdate>2015</risdate><volume>77</volume><spage>186</spage><epage>193</epage><pages>186-193</pages><issn>0142-1123</issn><eissn>1879-3452</eissn><abstract>•Stress intensity factor estimation in attachment lugs.•Extended finite element method to calculate SIF in attachment lugs.•Fatigue life estimation and crack growth in straight lugs.
In the present paper, a three dimensional finite element method (FEM) is used to compute the stress intensity factor (SIF) in straight lugs of Aluminum 7075-T6. Extended finite element method (XFEM) capability available in ABAQUS is used to calculate the stress intensity factor. Crack growth and fatigue life of single through-thickness and single quarter elliptical corner cracks in attachment lug are estimated and then compared with the available experimental data for two different load ratios equal to 0.1 and 0.5. The SIF calculated from XFEM shows that the introduction of different loading boundary conditions significantly affect the estimated fatigue life.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.ijfatigue.2015.02.021</doi><tpages>8</tpages></addata></record> |
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source | ScienceDirect Freedom Collection 2022-2024 |
subjects | Attachment Attachment lugs Crack propagation Extended finite element method Fatigue life Finite element method Lugs Mathematical analysis Mathematical models Stress intensity factor |
title | Fatigue life prediction of cracked attachment lugs using XFEM |
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