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The compressive behavior of CFRP laminates with delamination of different shapes using numerical and experimental approaches
Composite laminates often produce delamination due to a series of factors during the manufacture and service process. In order to research the effect of containing oblique elliptical and circular initial delamination damage on the compressive strength of composite laminates, numerical and experiment...
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Published in: | Journal of mechanical science and technology 2022, 36(9), , pp.4443-4453 |
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creator | Hu, Chunxing Bai, Yujiao Xu, Zhonghai Li, Ruoyu Wang, Rongguo He, Xiaodong |
description | Composite laminates often produce delamination due to a series of factors during the manufacture and service process. In order to research the effect of containing oblique elliptical and circular initial delamination damage on the compressive strength of composite laminates, numerical and experimental methods are used in this paper. Finite element models (FEMs) and the progressive damage subroutine USDFLD are developed to predict the damage initiation and extension behavior of the intralaminar of the laminate. Interlaminar damage is predicted based on cohesive zone models (CZM). At the same time, four compression tests containing different initial delamination damage are performed. The results show that experimental measurements of compression tests concur with the numerical predictions and validate the FEMs. The strength and stiffness of the specimens gradually decrease with the increase of the initial delamination area. It reveals that, for the compression process, the delamination damage extends from the edge of the initial damage to the surroundings. The bearing capacity of the composite laminates is mainly determined by the material properties of the fibers and matrix, rather than the initial delamination. |
doi_str_mv | 10.1007/s12206-022-0809-z |
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In order to research the effect of containing oblique elliptical and circular initial delamination damage on the compressive strength of composite laminates, numerical and experimental methods are used in this paper. Finite element models (FEMs) and the progressive damage subroutine USDFLD are developed to predict the damage initiation and extension behavior of the intralaminar of the laminate. Interlaminar damage is predicted based on cohesive zone models (CZM). At the same time, four compression tests containing different initial delamination damage are performed. The results show that experimental measurements of compression tests concur with the numerical predictions and validate the FEMs. The strength and stiffness of the specimens gradually decrease with the increase of the initial delamination area. It reveals that, for the compression process, the delamination damage extends from the edge of the initial damage to the surroundings. The bearing capacity of the composite laminates is mainly determined by the material properties of the fibers and matrix, rather than the initial delamination.</description><identifier>ISSN: 1738-494X</identifier><identifier>EISSN: 1976-3824</identifier><identifier>DOI: 10.1007/s12206-022-0809-z</identifier><language>eng</language><publisher>Seoul: Korean Society of Mechanical Engineers</publisher><subject>Bearing capacity ; Compression tests ; Compression zone ; Compressive properties ; Compressive strength ; Control ; Crack initiation ; Damage ; Delamination ; Dynamical Systems ; Engineering ; Finite element method ; Fracture mechanics ; Industrial and Production Engineering ; Laminates ; Material properties ; Mathematical analysis ; Mathematical models ; Mechanical Engineering ; Numerical methods ; Numerical prediction ; Original Article ; Stiffness ; Vibration ; 기계공학</subject><ispartof>Journal of Mechanical Science and Technology, 2022, 36(9), , pp.4443-4453</ispartof><rights>The Korean Society of Mechanical Engineers and Springer-Verlag GmbH Germany, part of Springer Nature 2022</rights><rights>The Korean Society of Mechanical Engineers and Springer-Verlag GmbH Germany, part of Springer Nature 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c281t-d0e20ddc59819c839a804223fef7e19a7b68d340396cb3f291c1edeae74c64f93</citedby><cites>FETCH-LOGICAL-c281t-d0e20ddc59819c839a804223fef7e19a7b68d340396cb3f291c1edeae74c64f93</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27923,27924</link.rule.ids><backlink>$$Uhttps://www.kci.go.kr/kciportal/ci/sereArticleSearch/ciSereArtiView.kci?sereArticleSearchBean.artiId=ART002874208$$DAccess content in National Research Foundation of Korea (NRF)$$Hfree_for_read</backlink></links><search><creatorcontrib>Hu, Chunxing</creatorcontrib><creatorcontrib>Bai, Yujiao</creatorcontrib><creatorcontrib>Xu, Zhonghai</creatorcontrib><creatorcontrib>Li, Ruoyu</creatorcontrib><creatorcontrib>Wang, Rongguo</creatorcontrib><creatorcontrib>He, Xiaodong</creatorcontrib><title>The compressive behavior of CFRP laminates with delamination of different shapes using numerical and experimental approaches</title><title>Journal of mechanical science and technology</title><addtitle>J Mech Sci Technol</addtitle><description>Composite laminates often produce delamination due to a series of factors during the manufacture and service process. In order to research the effect of containing oblique elliptical and circular initial delamination damage on the compressive strength of composite laminates, numerical and experimental methods are used in this paper. Finite element models (FEMs) and the progressive damage subroutine USDFLD are developed to predict the damage initiation and extension behavior of the intralaminar of the laminate. Interlaminar damage is predicted based on cohesive zone models (CZM). At the same time, four compression tests containing different initial delamination damage are performed. The results show that experimental measurements of compression tests concur with the numerical predictions and validate the FEMs. The strength and stiffness of the specimens gradually decrease with the increase of the initial delamination area. It reveals that, for the compression process, the delamination damage extends from the edge of the initial damage to the surroundings. The bearing capacity of the composite laminates is mainly determined by the material properties of the fibers and matrix, rather than the initial delamination.</description><subject>Bearing capacity</subject><subject>Compression tests</subject><subject>Compression zone</subject><subject>Compressive properties</subject><subject>Compressive strength</subject><subject>Control</subject><subject>Crack initiation</subject><subject>Damage</subject><subject>Delamination</subject><subject>Dynamical Systems</subject><subject>Engineering</subject><subject>Finite element method</subject><subject>Fracture mechanics</subject><subject>Industrial and Production Engineering</subject><subject>Laminates</subject><subject>Material properties</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Mechanical Engineering</subject><subject>Numerical methods</subject><subject>Numerical prediction</subject><subject>Original Article</subject><subject>Stiffness</subject><subject>Vibration</subject><subject>기계공학</subject><issn>1738-494X</issn><issn>1976-3824</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp1kV1LHDEUhodSoXbtD_Au4F1hbL46SS6XpVpBUJYt9C5kMyc70d1kTGbVLv74ZhzBK6_OB8_7cpK3qk4JPicYix-ZUIqbGlNaY4lVffhUHRMlmppJyj-XXjBZc8X_fqm-5nyHcUM5IcfVy6oDZOOuT5CzfwS0hs48-phQdGhxsbxFW7PzwQyQ0ZMfOtTC28LHMDKtdw4ShAHlzvSF2mcfNijsd5C8NVtkQovguS_TrlDjou9TNLaDfFIdObPN8O2tzqo_F79Wi9_19c3l1WJ-XVsqyVC3GChuW_tTSaKsZMpIzCllDpwAooxYN7JlHDPV2DVzVBFLoAUDgtuGO8Vm1ffJNySn763X0fjXuon6Pun5cnWlyy8yJZsRPpvgcuXDHvKg7-I-hXKfpoIQqbCQvFBkomyKOSdwui8PNOlfMRq9hJ4S0SURPSaiD0VDJ00ubNhAenf-WPQfVk6QjA</recordid><startdate>20220901</startdate><enddate>20220901</enddate><creator>Hu, Chunxing</creator><creator>Bai, Yujiao</creator><creator>Xu, Zhonghai</creator><creator>Li, Ruoyu</creator><creator>Wang, Rongguo</creator><creator>He, Xiaodong</creator><general>Korean Society of Mechanical Engineers</general><general>Springer Nature B.V</general><general>대한기계학회</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>ACYCR</scope></search><sort><creationdate>20220901</creationdate><title>The compressive behavior of CFRP laminates with delamination of different shapes using numerical and experimental approaches</title><author>Hu, Chunxing ; Bai, Yujiao ; Xu, Zhonghai ; Li, Ruoyu ; Wang, Rongguo ; He, Xiaodong</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c281t-d0e20ddc59819c839a804223fef7e19a7b68d340396cb3f291c1edeae74c64f93</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Bearing capacity</topic><topic>Compression tests</topic><topic>Compression zone</topic><topic>Compressive properties</topic><topic>Compressive strength</topic><topic>Control</topic><topic>Crack initiation</topic><topic>Damage</topic><topic>Delamination</topic><topic>Dynamical Systems</topic><topic>Engineering</topic><topic>Finite element method</topic><topic>Fracture mechanics</topic><topic>Industrial and Production Engineering</topic><topic>Laminates</topic><topic>Material properties</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Mechanical Engineering</topic><topic>Numerical methods</topic><topic>Numerical prediction</topic><topic>Original Article</topic><topic>Stiffness</topic><topic>Vibration</topic><topic>기계공학</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hu, Chunxing</creatorcontrib><creatorcontrib>Bai, Yujiao</creatorcontrib><creatorcontrib>Xu, Zhonghai</creatorcontrib><creatorcontrib>Li, Ruoyu</creatorcontrib><creatorcontrib>Wang, Rongguo</creatorcontrib><creatorcontrib>He, Xiaodong</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Korean Citation Index</collection><jtitle>Journal of mechanical science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hu, Chunxing</au><au>Bai, Yujiao</au><au>Xu, Zhonghai</au><au>Li, Ruoyu</au><au>Wang, Rongguo</au><au>He, Xiaodong</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The compressive behavior of CFRP laminates with delamination of different shapes using numerical and experimental approaches</atitle><jtitle>Journal of mechanical science and technology</jtitle><stitle>J Mech Sci Technol</stitle><date>2022-09-01</date><risdate>2022</risdate><volume>36</volume><issue>9</issue><spage>4443</spage><epage>4453</epage><pages>4443-4453</pages><issn>1738-494X</issn><eissn>1976-3824</eissn><abstract>Composite laminates often produce delamination due to a series of factors during the manufacture and service process. In order to research the effect of containing oblique elliptical and circular initial delamination damage on the compressive strength of composite laminates, numerical and experimental methods are used in this paper. Finite element models (FEMs) and the progressive damage subroutine USDFLD are developed to predict the damage initiation and extension behavior of the intralaminar of the laminate. Interlaminar damage is predicted based on cohesive zone models (CZM). At the same time, four compression tests containing different initial delamination damage are performed. The results show that experimental measurements of compression tests concur with the numerical predictions and validate the FEMs. The strength and stiffness of the specimens gradually decrease with the increase of the initial delamination area. It reveals that, for the compression process, the delamination damage extends from the edge of the initial damage to the surroundings. The bearing capacity of the composite laminates is mainly determined by the material properties of the fibers and matrix, rather than the initial delamination.</abstract><cop>Seoul</cop><pub>Korean Society of Mechanical Engineers</pub><doi>10.1007/s12206-022-0809-z</doi><tpages>11</tpages></addata></record> |
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subjects | Bearing capacity Compression tests Compression zone Compressive properties Compressive strength Control Crack initiation Damage Delamination Dynamical Systems Engineering Finite element method Fracture mechanics Industrial and Production Engineering Laminates Material properties Mathematical analysis Mathematical models Mechanical Engineering Numerical methods Numerical prediction Original Article Stiffness Vibration 기계공학 |
title | The compressive behavior of CFRP laminates with delamination of different shapes using numerical and experimental approaches |
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