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Influence of stiffener on fracture parameter and fatigue crack growth life of a finite aluminium alloy plate
The present paper discusses the methodology for prediction of fracture parameter, fatigue crack growth life (FC) and inspection interval (II) considering the stiffener effect using Afgrow software of NASGRO crack growth model. Based on numerically predicted normalised stress intensity factor ( β ) u...
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Published in: | Journal of the Brazilian Society of Mechanical Sciences and Engineering 2021-05, Vol.43 (5), Article 251 |
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creator | Srivastava, Amit Kumar Arora, P. K. |
description | The present paper discusses the methodology for prediction of fracture parameter, fatigue crack growth life (FC) and inspection interval (II) considering the stiffener effect using Afgrow software of NASGRO crack growth model. Based on numerically predicted normalised stress intensity factor (
β
) using finite element method (FEM), correction factor (C.F.) in
β
of un-stiffened panel/plate is introduced to account for the stiffener effect. The
β
of stiffened plate is further used for prediction of fatigue crack growth life (FC) and II. The fracture parameters of stiffened panel for different crack lengths, stiffener area, and stiffener offset using FEM are predicted, which is further used for estimation of FC and II. The typical numerical prediction of fracture parameter using finite element method and FC with incorporation of C.F. using Afgrow software is compared with published experimental results and analytical prediction which show good conformity. |
doi_str_mv | 10.1007/s40430-021-02968-9 |
format | article |
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β
) using finite element method (FEM), correction factor (C.F.) in
β
of un-stiffened panel/plate is introduced to account for the stiffener effect. The
β
of stiffened plate is further used for prediction of fatigue crack growth life (FC) and II. The fracture parameters of stiffened panel for different crack lengths, stiffener area, and stiffener offset using FEM are predicted, which is further used for estimation of FC and II. The typical numerical prediction of fracture parameter using finite element method and FC with incorporation of C.F. using Afgrow software is compared with published experimental results and analytical prediction which show good conformity.</description><identifier>ISSN: 1678-5878</identifier><identifier>EISSN: 1806-3691</identifier><identifier>DOI: 10.1007/s40430-021-02968-9</identifier><language>eng</language><publisher>Berlin/Heidelberg: Springer Berlin Heidelberg</publisher><subject>Aluminum base alloys ; Crack propagation ; Engineering ; Fatigue failure ; Finite element analysis ; Finite element method ; Fracture mechanics ; Growth models ; Inspection ; Mechanical Engineering ; Metal plates ; Numerical prediction ; Parameters ; Software ; Stress intensity factors ; Technical Paper</subject><ispartof>Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2021-05, Vol.43 (5), Article 251</ispartof><rights>The Brazilian Society of Mechanical Sciences and Engineering 2021</rights><rights>The Brazilian Society of Mechanical Sciences and Engineering 2021.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-aa885248c46f6ce71e2192cfa87bcf2127450a8b6788aa34c8da9a192659d9ec3</citedby><cites>FETCH-LOGICAL-c319t-aa885248c46f6ce71e2192cfa87bcf2127450a8b6788aa34c8da9a192659d9ec3</cites><orcidid>0000-0002-7086-8759</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Srivastava, Amit Kumar</creatorcontrib><creatorcontrib>Arora, P. K.</creatorcontrib><title>Influence of stiffener on fracture parameter and fatigue crack growth life of a finite aluminium alloy plate</title><title>Journal of the Brazilian Society of Mechanical Sciences and Engineering</title><addtitle>J Braz. Soc. Mech. Sci. Eng</addtitle><description>The present paper discusses the methodology for prediction of fracture parameter, fatigue crack growth life (FC) and inspection interval (II) considering the stiffener effect using Afgrow software of NASGRO crack growth model. Based on numerically predicted normalised stress intensity factor (
β
) using finite element method (FEM), correction factor (C.F.) in
β
of un-stiffened panel/plate is introduced to account for the stiffener effect. The
β
of stiffened plate is further used for prediction of fatigue crack growth life (FC) and II. The fracture parameters of stiffened panel for different crack lengths, stiffener area, and stiffener offset using FEM are predicted, which is further used for estimation of FC and II. The typical numerical prediction of fracture parameter using finite element method and FC with incorporation of C.F. using Afgrow software is compared with published experimental results and analytical prediction which show good conformity.</description><subject>Aluminum base alloys</subject><subject>Crack propagation</subject><subject>Engineering</subject><subject>Fatigue failure</subject><subject>Finite element analysis</subject><subject>Finite element method</subject><subject>Fracture mechanics</subject><subject>Growth models</subject><subject>Inspection</subject><subject>Mechanical Engineering</subject><subject>Metal plates</subject><subject>Numerical prediction</subject><subject>Parameters</subject><subject>Software</subject><subject>Stress intensity factors</subject><subject>Technical Paper</subject><issn>1678-5878</issn><issn>1806-3691</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9UE1LAzEQDaJgrf4BTwHPq_nYzSZHKX4UCl70HKbppG7dj5pkkf57Y1fw5mGYx8x7b5hHyDVnt5yx-i6WrJSsYILnMkoX5oTMuGaqkMrw04xVrYtK1_qcXMS4Y0yKSlUz0i57347YO6SDpzE13mOPgQ499QFcGgPSPQToMOUp9BvqITXbEanL6w-6DcNXeqdt448GQH3TNwkptGOX0dhl1A4Hum8h4SU589BGvPrtc_L2-PC6eC5WL0_Lxf2qcJKbVABoXYlSu1J55bDmKLgRzoOu184LLuqyYqDX-SUNIEunN2AgU1RlNgadnJObyXcfhs8RY7K7YQx9PmlFxbnQZS11ZomJ5cIQY0Bv96HpIBwsZ_YnVTulanOq9piqNVkkJ1HM5H6L4c_6H9U3kvV7gQ</recordid><startdate>20210501</startdate><enddate>20210501</enddate><creator>Srivastava, Amit Kumar</creator><creator>Arora, P. K.</creator><general>Springer Berlin Heidelberg</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0002-7086-8759</orcidid></search><sort><creationdate>20210501</creationdate><title>Influence of stiffener on fracture parameter and fatigue crack growth life of a finite aluminium alloy plate</title><author>Srivastava, Amit Kumar ; Arora, P. K.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-aa885248c46f6ce71e2192cfa87bcf2127450a8b6788aa34c8da9a192659d9ec3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Aluminum base alloys</topic><topic>Crack propagation</topic><topic>Engineering</topic><topic>Fatigue failure</topic><topic>Finite element analysis</topic><topic>Finite element method</topic><topic>Fracture mechanics</topic><topic>Growth models</topic><topic>Inspection</topic><topic>Mechanical Engineering</topic><topic>Metal plates</topic><topic>Numerical prediction</topic><topic>Parameters</topic><topic>Software</topic><topic>Stress intensity factors</topic><topic>Technical Paper</topic><toplevel>online_resources</toplevel><creatorcontrib>Srivastava, Amit Kumar</creatorcontrib><creatorcontrib>Arora, P. K.</creatorcontrib><collection>CrossRef</collection><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Srivastava, Amit Kumar</au><au>Arora, P. K.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Influence of stiffener on fracture parameter and fatigue crack growth life of a finite aluminium alloy plate</atitle><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle><stitle>J Braz. Soc. Mech. Sci. Eng</stitle><date>2021-05-01</date><risdate>2021</risdate><volume>43</volume><issue>5</issue><artnum>251</artnum><issn>1678-5878</issn><eissn>1806-3691</eissn><abstract>The present paper discusses the methodology for prediction of fracture parameter, fatigue crack growth life (FC) and inspection interval (II) considering the stiffener effect using Afgrow software of NASGRO crack growth model. Based on numerically predicted normalised stress intensity factor (
β
) using finite element method (FEM), correction factor (C.F.) in
β
of un-stiffened panel/plate is introduced to account for the stiffener effect. The
β
of stiffened plate is further used for prediction of fatigue crack growth life (FC) and II. The fracture parameters of stiffened panel for different crack lengths, stiffener area, and stiffener offset using FEM are predicted, which is further used for estimation of FC and II. The typical numerical prediction of fracture parameter using finite element method and FC with incorporation of C.F. using Afgrow software is compared with published experimental results and analytical prediction which show good conformity.</abstract><cop>Berlin/Heidelberg</cop><pub>Springer Berlin Heidelberg</pub><doi>10.1007/s40430-021-02968-9</doi><orcidid>https://orcid.org/0000-0002-7086-8759</orcidid></addata></record> |
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subjects | Aluminum base alloys Crack propagation Engineering Fatigue failure Finite element analysis Finite element method Fracture mechanics Growth models Inspection Mechanical Engineering Metal plates Numerical prediction Parameters Software Stress intensity factors Technical Paper |
title | Influence of stiffener on fracture parameter and fatigue crack growth life of a finite aluminium alloy plate |
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