Influence of Residual Stress on the Fatigue Crack Growth Mechanism in the Al-Alloy/Hybrid MMC Bi-Material
In this research, the effect of residual stress on the fatigue crack growth behavior in an aluminum alloy-hybrid metal matrix composite (Al alloy-Hybrid MMC) bi- material system has been investigated and the fatigue life of the bi-material has been predicted based on the crack closure technique. Con...
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| Veröffentlicht in: | Journal of failure analysis and prevention 2022-08, Vol.22 (4), p.1468-1477 |
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| creator | Iqbal, AKM Asif Arai, Yoshio Araki, Wakako |
| description | In this research, the effect of residual stress on the fatigue crack growth behavior in an aluminum alloy-hybrid metal matrix composite (Al alloy-Hybrid MMC) bi- material system has been investigated and the fatigue life of the bi-material has been predicted based on the crack closure technique. Conventional three-point bending fatigue test was carried out in a rectangular notched specimen and the plastic replica technique was used to observe the fatigue crack growth (FCG). The residual stress was measured by the strain relieving method. The fatigue life was predicted by classifying the expression of FCG rate and the effective stress intensity factor, Δ
K
eff
. The results show that the crack propagates slowly in the MMC layer side and maximum crack retardation occurs in the boundary region of the bi-material system due to the change of the state of residual stresses around the boundary. A curved crack front is observed in the aluminum alloy side near the boundary of the bi-material which forms a corner crack that decelerates the crack growth in the vicinity of the boundary of the bi-material even at higher Δ
K
. |
| doi_str_mv | 10.1007/s11668-022-01432-7 |
| format | Article |
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K
eff
. The results show that the crack propagates slowly in the MMC layer side and maximum crack retardation occurs in the boundary region of the bi-material system due to the change of the state of residual stresses around the boundary. A curved crack front is observed in the aluminum alloy side near the boundary of the bi-material which forms a corner crack that decelerates the crack growth in the vicinity of the boundary of the bi-material even at higher Δ
K
.</description><identifier>ISSN: 1547-7029</identifier><identifier>EISSN: 1728-5674</identifier><identifier>EISSN: 1864-1245</identifier><identifier>DOI: 10.1007/s11668-022-01432-7</identifier><language>eng</language><publisher>New York: Springer US</publisher><subject>Aluminum alloys ; Aluminum base alloys ; Aluminum matrix composites ; Bending fatigue ; Characterization and Evaluation of Materials ; Chemistry and Materials Science ; Classical Mechanics ; Corrosion and Coatings ; Crack closure ; Crack propagation ; Deceleration ; Fatigue failure ; Fatigue life ; Fatigue tests ; Fracture mechanics ; Hybrid systems ; Materials Science ; Metal matrix composites ; Quality Control ; Reliability ; Residual stress ; Safety and Risk ; Solid Mechanics ; Stress intensity factors ; Technical Article---Peer-Reviewed ; Tribology</subject><ispartof>Journal of failure analysis and prevention, 2022-08, Vol.22 (4), p.1468-1477</ispartof><rights>ASM International 2022</rights><rights>ASM International 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c249t-d71ddb29ba90b52a42d2d6d47ad988b08fed57548aeb81527064c21d573843863</citedby><cites>FETCH-LOGICAL-c249t-d71ddb29ba90b52a42d2d6d47ad988b08fed57548aeb81527064c21d573843863</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Iqbal, AKM Asif</creatorcontrib><creatorcontrib>Arai, Yoshio</creatorcontrib><creatorcontrib>Araki, Wakako</creatorcontrib><title>Influence of Residual Stress on the Fatigue Crack Growth Mechanism in the Al-Alloy/Hybrid MMC Bi-Material</title><title>Journal of failure analysis and prevention</title><addtitle>J Fail. Anal. and Preven</addtitle><description>In this research, the effect of residual stress on the fatigue crack growth behavior in an aluminum alloy-hybrid metal matrix composite (Al alloy-Hybrid MMC) bi- material system has been investigated and the fatigue life of the bi-material has been predicted based on the crack closure technique. Conventional three-point bending fatigue test was carried out in a rectangular notched specimen and the plastic replica technique was used to observe the fatigue crack growth (FCG). The residual stress was measured by the strain relieving method. The fatigue life was predicted by classifying the expression of FCG rate and the effective stress intensity factor, Δ
K
eff
. The results show that the crack propagates slowly in the MMC layer side and maximum crack retardation occurs in the boundary region of the bi-material system due to the change of the state of residual stresses around the boundary. A curved crack front is observed in the aluminum alloy side near the boundary of the bi-material which forms a corner crack that decelerates the crack growth in the vicinity of the boundary of the bi-material even at higher Δ
K
.</description><subject>Aluminum alloys</subject><subject>Aluminum base alloys</subject><subject>Aluminum matrix composites</subject><subject>Bending fatigue</subject><subject>Characterization and Evaluation of Materials</subject><subject>Chemistry and Materials Science</subject><subject>Classical Mechanics</subject><subject>Corrosion and Coatings</subject><subject>Crack closure</subject><subject>Crack propagation</subject><subject>Deceleration</subject><subject>Fatigue failure</subject><subject>Fatigue life</subject><subject>Fatigue tests</subject><subject>Fracture mechanics</subject><subject>Hybrid systems</subject><subject>Materials Science</subject><subject>Metal matrix composites</subject><subject>Quality Control</subject><subject>Reliability</subject><subject>Residual stress</subject><subject>Safety and Risk</subject><subject>Solid Mechanics</subject><subject>Stress intensity factors</subject><subject>Technical Article---Peer-Reviewed</subject><subject>Tribology</subject><issn>1547-7029</issn><issn>1728-5674</issn><issn>1864-1245</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp9kF1LwzAUhoMoOKd_wKuA13FJmjTp5SzuA1YEP65D2qRbZtfOpEX2741W8M6rczg873vgAeCW4HuCsZgFQtJUIkwpwoQlFIkzMCGCSsRTwc7jzplAAtPsElyFsMc44YTRCXDrtm4G21YWdjV8tsGZQTfwpfc2BNi1sN9ZuNC92w4W5l5X73Dpu89-Bwtb7XTrwgG6kZo3aN403Wm2OpXeGVgUOXxwqNC99U431-Ci1k2wN79zCt4Wj6_5Cm2elut8vkEVZVmPjCDGlDQrdYZLTjWjhprUMKFNJmWJZW0NF5xJbUtJOBU4ZRUl8ZZIlsg0mYK7sffou4_Bhl7tu8G38aWigmSMx1QSKTpSle9C8LZWR-8O2p8UwepbqRqVqqhU_ShVIoaSMRQi3G6t_6v-J_UFYDl34w</recordid><startdate>20220801</startdate><enddate>20220801</enddate><creator>Iqbal, AKM Asif</creator><creator>Arai, Yoshio</creator><creator>Araki, Wakako</creator><general>Springer US</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TA</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope></search><sort><creationdate>20220801</creationdate><title>Influence of Residual Stress on the Fatigue Crack Growth Mechanism in the Al-Alloy/Hybrid MMC Bi-Material</title><author>Iqbal, AKM Asif ; Arai, Yoshio ; Araki, Wakako</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c249t-d71ddb29ba90b52a42d2d6d47ad988b08fed57548aeb81527064c21d573843863</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Aluminum alloys</topic><topic>Aluminum base alloys</topic><topic>Aluminum matrix composites</topic><topic>Bending fatigue</topic><topic>Characterization and Evaluation of Materials</topic><topic>Chemistry and Materials Science</topic><topic>Classical Mechanics</topic><topic>Corrosion and Coatings</topic><topic>Crack closure</topic><topic>Crack propagation</topic><topic>Deceleration</topic><topic>Fatigue failure</topic><topic>Fatigue life</topic><topic>Fatigue tests</topic><topic>Fracture mechanics</topic><topic>Hybrid systems</topic><topic>Materials Science</topic><topic>Metal matrix composites</topic><topic>Quality Control</topic><topic>Reliability</topic><topic>Residual stress</topic><topic>Safety and Risk</topic><topic>Solid Mechanics</topic><topic>Stress intensity factors</topic><topic>Technical Article---Peer-Reviewed</topic><topic>Tribology</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Iqbal, AKM Asif</creatorcontrib><creatorcontrib>Arai, Yoshio</creatorcontrib><creatorcontrib>Araki, Wakako</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Materials Business File</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of failure analysis and prevention</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Iqbal, AKM Asif</au><au>Arai, Yoshio</au><au>Araki, Wakako</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Influence of Residual Stress on the Fatigue Crack Growth Mechanism in the Al-Alloy/Hybrid MMC Bi-Material</atitle><jtitle>Journal of failure analysis and prevention</jtitle><stitle>J Fail. Anal. and Preven</stitle><date>2022-08-01</date><risdate>2022</risdate><volume>22</volume><issue>4</issue><spage>1468</spage><epage>1477</epage><pages>1468-1477</pages><issn>1547-7029</issn><eissn>1728-5674</eissn><eissn>1864-1245</eissn><abstract>In this research, the effect of residual stress on the fatigue crack growth behavior in an aluminum alloy-hybrid metal matrix composite (Al alloy-Hybrid MMC) bi- material system has been investigated and the fatigue life of the bi-material has been predicted based on the crack closure technique. Conventional three-point bending fatigue test was carried out in a rectangular notched specimen and the plastic replica technique was used to observe the fatigue crack growth (FCG). The residual stress was measured by the strain relieving method. The fatigue life was predicted by classifying the expression of FCG rate and the effective stress intensity factor, Δ
K
eff
. The results show that the crack propagates slowly in the MMC layer side and maximum crack retardation occurs in the boundary region of the bi-material system due to the change of the state of residual stresses around the boundary. A curved crack front is observed in the aluminum alloy side near the boundary of the bi-material which forms a corner crack that decelerates the crack growth in the vicinity of the boundary of the bi-material even at higher Δ
K
.</abstract><cop>New York</cop><pub>Springer US</pub><doi>10.1007/s11668-022-01432-7</doi><tpages>10</tpages></addata></record> |
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| subjects | Aluminum alloys Aluminum base alloys Aluminum matrix composites Bending fatigue Characterization and Evaluation of Materials Chemistry and Materials Science Classical Mechanics Corrosion and Coatings Crack closure Crack propagation Deceleration Fatigue failure Fatigue life Fatigue tests Fracture mechanics Hybrid systems Materials Science Metal matrix composites Quality Control Reliability Residual stress Safety and Risk Solid Mechanics Stress intensity factors Technical Article---Peer-Reviewed Tribology |
| title | Influence of Residual Stress on the Fatigue Crack Growth Mechanism in the Al-Alloy/Hybrid MMC Bi-Material |
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