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Mode II Interlaminar Fracture Toughness of Flax/Glass/Epoxy Hybrid Composite Materials: An Experimental and Numerical Study
The mode II interlaminar fracture toughness characteristics of flax/glass/epoxy hybrid laminates were experimentally and numerically examined. Three types of hybrid composites that are made of flax (F) and glass (G) and with different layup sequences (i.e., Hybrid I [0 G /0 F ] 8S , Hybrid II [0 4...
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Published in: | Journal of natural fibers 2022-11, Vol.19 (11), p.4286-4300 |
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creator | Ekeoseye, Wilfred Stephen Kolasangiani, Kamal Oguamanam, Donatus C.D. Bougherara, Habiba |
description | The mode II interlaminar fracture toughness characteristics of flax/glass/epoxy hybrid laminates were experimentally and numerically examined. Three types of hybrid composites that are made of flax (F) and glass (G) and with different layup sequences (i.e., Hybrid I [0
G
/0
F
]
8S
, Hybrid II [0
4G
/0
4F
]
S
, and Hybrid III [0
4G
/(90/0)
2F
]
S
) were investigated. The experimental results obtained from end notch flexural tests showed that both the mode II fracture toughness and flexural strength of Hybrid I composites were higher than those for Hybrid II & III composites. This was attributed to the presence of bridging in several interfaces of the flax plies and the glass plies in Hybrid I. A second delamination propagation between the flax/epoxy midplane plies was observed in Hybrid II and III and this helped to lower both the mode II fracture toughness and flexural strength. The finite element simulations employed the virtual crack closure technique and the cohesive zone model. The results showed that both methods successfully predicted mode II interlaminar fracture toughness characteristics of the Hybrid I composites, but significantly overpredicted the values for both Hybrid II & III due to the presence of a secondary delamination propagation. |
doi_str_mv | 10.1080/15440478.2020.1856277 |
format | article |
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G
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F
]
8S
, Hybrid II [0
4G
/0
4F
]
S
, and Hybrid III [0
4G
/(90/0)
2F
]
S
) were investigated. The experimental results obtained from end notch flexural tests showed that both the mode II fracture toughness and flexural strength of Hybrid I composites were higher than those for Hybrid II & III composites. This was attributed to the presence of bridging in several interfaces of the flax plies and the glass plies in Hybrid I. A second delamination propagation between the flax/epoxy midplane plies was observed in Hybrid II and III and this helped to lower both the mode II fracture toughness and flexural strength. The finite element simulations employed the virtual crack closure technique and the cohesive zone model. The results showed that both methods successfully predicted mode II interlaminar fracture toughness characteristics of the Hybrid I composites, but significantly overpredicted the values for both Hybrid II & III due to the presence of a secondary delamination propagation.</description><identifier>ISSN: 1544-0478</identifier><identifier>EISSN: 1544-046X</identifier><identifier>DOI: 10.1080/15440478.2020.1856277</identifier><language>eng</language><publisher>Abingdon: Taylor & Francis</publisher><subject>cohesive zone model ; Composite materials ; Crack closure ; Delamination ; ENF test ; Flax ; Flax/glass/epoxy hybrid composite ; Flexural strength ; Fracture toughness ; Heat treating ; Hybrid composites ; II型层间断裂韧性 ; Interfaces ; Laminates ; Layers ; mode II interlaminar fracture toughness ; Propagation ; virtual crack closure technique ; 分层 ; 测试 ; 环氧/亚麻复合玻璃 ; 粘性带模型 ; 虚拟裂缝闭合技术</subject><ispartof>Journal of natural fibers, 2022-11, Vol.19 (11), p.4286-4300</ispartof><rights>2020 Taylor & Francis 2020</rights><rights>2020 Taylor & Francis</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c404t-2b8bc10da12388524ee8303f4265b7d5100237cdf46a24d4d89d07d7e8c5fb693</citedby><cites>FETCH-LOGICAL-c404t-2b8bc10da12388524ee8303f4265b7d5100237cdf46a24d4d89d07d7e8c5fb693</cites><orcidid>0000-0001-6678-570X</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27922,27923</link.rule.ids></links><search><creatorcontrib>Ekeoseye, Wilfred Stephen</creatorcontrib><creatorcontrib>Kolasangiani, Kamal</creatorcontrib><creatorcontrib>Oguamanam, Donatus C.D.</creatorcontrib><creatorcontrib>Bougherara, Habiba</creatorcontrib><title>Mode II Interlaminar Fracture Toughness of Flax/Glass/Epoxy Hybrid Composite Materials: An Experimental and Numerical Study</title><title>Journal of natural fibers</title><description>The mode II interlaminar fracture toughness characteristics of flax/glass/epoxy hybrid laminates were experimentally and numerically examined. Three types of hybrid composites that are made of flax (F) and glass (G) and with different layup sequences (i.e., Hybrid I [0
G
/0
F
]
8S
, Hybrid II [0
4G
/0
4F
]
S
, and Hybrid III [0
4G
/(90/0)
2F
]
S
) were investigated. The experimental results obtained from end notch flexural tests showed that both the mode II fracture toughness and flexural strength of Hybrid I composites were higher than those for Hybrid II & III composites. This was attributed to the presence of bridging in several interfaces of the flax plies and the glass plies in Hybrid I. A second delamination propagation between the flax/epoxy midplane plies was observed in Hybrid II and III and this helped to lower both the mode II fracture toughness and flexural strength. The finite element simulations employed the virtual crack closure technique and the cohesive zone model. The results showed that both methods successfully predicted mode II interlaminar fracture toughness characteristics of the Hybrid I composites, but significantly overpredicted the values for both Hybrid II & III due to the presence of a secondary delamination propagation.</description><subject>cohesive zone model</subject><subject>Composite materials</subject><subject>Crack closure</subject><subject>Delamination</subject><subject>ENF test</subject><subject>Flax</subject><subject>Flax/glass/epoxy hybrid composite</subject><subject>Flexural strength</subject><subject>Fracture toughness</subject><subject>Heat treating</subject><subject>Hybrid composites</subject><subject>II型层间断裂韧性</subject><subject>Interfaces</subject><subject>Laminates</subject><subject>Layers</subject><subject>mode II interlaminar fracture toughness</subject><subject>Propagation</subject><subject>virtual crack closure technique</subject><subject>分层</subject><subject>测试</subject><subject>环氧/亚麻复合玻璃</subject><subject>粘性带模型</subject><subject>虚拟裂缝闭合技术</subject><issn>1544-0478</issn><issn>1544-046X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><sourceid>DOA</sourceid><recordid>eNp9kU1v1DAQhiMEEqXlJyBZ4rxd27FjhxPVareN1NIDReJmTfxRskriYDtiI_58vd3SIyd7Xs088_EWxSeCLwmWeE04Y5gJeUkxzZLkFRXiTXF21FeYVT_fvv6FfF98iHGPMa05oWfF3ztvLGoa1IzJhh6GboSAdgF0moNFD35-_DXaGJF3aNfDYX3dQ4zr7eQPC7pZ2tAZtPHD5GOXLLqDDOmgj1_Q1Yi2hylHgx0T9AhGg77NQxZ0jr6n2SwXxTuXc-3Hl_e8-LHbPmxuVrf3183m6nal81ppRVvZaoINEFpKySmzVpa4dIxWvBWGk7xMKbRxrALKDDOyNlgYYaXmrq3q8rxoTlzjYa-mPBKERXno1LPgw6OCkDrdW1XXJRbSlsSBZpTWrSMcwBrBoTL5epn1-cSagv8925jU3s9hzOMrKkhNOcXs2JGfsnTwMQbrXrsSrI6eqX-eqaNn6sWzXPf1VNeNzocB_vjQG5Vg6X1wAUbdRVX-H_EEmqGdhA</recordid><startdate>20221102</startdate><enddate>20221102</enddate><creator>Ekeoseye, Wilfred Stephen</creator><creator>Kolasangiani, Kamal</creator><creator>Oguamanam, Donatus C.D.</creator><creator>Bougherara, Habiba</creator><general>Taylor & Francis</general><general>Taylor & Francis Ltd</general><general>Taylor & Francis Group</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7QO</scope><scope>7QQ</scope><scope>7SC</scope><scope>7SE</scope><scope>7SP</scope><scope>7SR</scope><scope>7T7</scope><scope>7TA</scope><scope>7TB</scope><scope>7U5</scope><scope>8BQ</scope><scope>8FD</scope><scope>C1K</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>H8G</scope><scope>JG9</scope><scope>JQ2</scope><scope>KR7</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>P64</scope><scope>DOA</scope><orcidid>https://orcid.org/0000-0001-6678-570X</orcidid></search><sort><creationdate>20221102</creationdate><title>Mode II Interlaminar Fracture Toughness of Flax/Glass/Epoxy Hybrid Composite Materials: An Experimental and Numerical Study</title><author>Ekeoseye, Wilfred Stephen ; Kolasangiani, Kamal ; Oguamanam, Donatus C.D. ; Bougherara, Habiba</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c404t-2b8bc10da12388524ee8303f4265b7d5100237cdf46a24d4d89d07d7e8c5fb693</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>cohesive zone model</topic><topic>Composite materials</topic><topic>Crack closure</topic><topic>Delamination</topic><topic>ENF test</topic><topic>Flax</topic><topic>Flax/glass/epoxy hybrid composite</topic><topic>Flexural strength</topic><topic>Fracture toughness</topic><topic>Heat treating</topic><topic>Hybrid composites</topic><topic>II型层间断裂韧性</topic><topic>Interfaces</topic><topic>Laminates</topic><topic>Layers</topic><topic>mode II interlaminar fracture toughness</topic><topic>Propagation</topic><topic>virtual crack closure technique</topic><topic>分层</topic><topic>测试</topic><topic>环氧/亚麻复合玻璃</topic><topic>粘性带模型</topic><topic>虚拟裂缝闭合技术</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ekeoseye, Wilfred Stephen</creatorcontrib><creatorcontrib>Kolasangiani, Kamal</creatorcontrib><creatorcontrib>Oguamanam, Donatus C.D.</creatorcontrib><creatorcontrib>Bougherara, Habiba</creatorcontrib><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Biotechnology Research Abstracts</collection><collection>Ceramic Abstracts</collection><collection>Computer and Information Systems Abstracts</collection><collection>Corrosion Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Industrial and Applied Microbiology Abstracts (Microbiology A)</collection><collection>Materials Business File</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Copper Technical Reference Library</collection><collection>Materials Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>Biotechnology and BioEngineering Abstracts</collection><collection>DOAJ Directory of Open Access Journals</collection><jtitle>Journal of natural fibers</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ekeoseye, Wilfred Stephen</au><au>Kolasangiani, Kamal</au><au>Oguamanam, Donatus C.D.</au><au>Bougherara, Habiba</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Mode II Interlaminar Fracture Toughness of Flax/Glass/Epoxy Hybrid Composite Materials: An Experimental and Numerical Study</atitle><jtitle>Journal of natural fibers</jtitle><date>2022-11-02</date><risdate>2022</risdate><volume>19</volume><issue>11</issue><spage>4286</spage><epage>4300</epage><pages>4286-4300</pages><issn>1544-0478</issn><eissn>1544-046X</eissn><abstract>The mode II interlaminar fracture toughness characteristics of flax/glass/epoxy hybrid laminates were experimentally and numerically examined. Three types of hybrid composites that are made of flax (F) and glass (G) and with different layup sequences (i.e., Hybrid I [0
G
/0
F
]
8S
, Hybrid II [0
4G
/0
4F
]
S
, and Hybrid III [0
4G
/(90/0)
2F
]
S
) were investigated. The experimental results obtained from end notch flexural tests showed that both the mode II fracture toughness and flexural strength of Hybrid I composites were higher than those for Hybrid II & III composites. This was attributed to the presence of bridging in several interfaces of the flax plies and the glass plies in Hybrid I. A second delamination propagation between the flax/epoxy midplane plies was observed in Hybrid II and III and this helped to lower both the mode II fracture toughness and flexural strength. The finite element simulations employed the virtual crack closure technique and the cohesive zone model. The results showed that both methods successfully predicted mode II interlaminar fracture toughness characteristics of the Hybrid I composites, but significantly overpredicted the values for both Hybrid II & III due to the presence of a secondary delamination propagation.</abstract><cop>Abingdon</cop><pub>Taylor & Francis</pub><doi>10.1080/15440478.2020.1856277</doi><tpages>15</tpages><orcidid>https://orcid.org/0000-0001-6678-570X</orcidid><oa>free_for_read</oa></addata></record> |
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source | Taylor and Francis Science and Technology Collection |
subjects | cohesive zone model Composite materials Crack closure Delamination ENF test Flax Flax/glass/epoxy hybrid composite Flexural strength Fracture toughness Heat treating Hybrid composites II型层间断裂韧性 Interfaces Laminates Layers mode II interlaminar fracture toughness Propagation virtual crack closure technique 分层 测试 环氧/亚麻复合玻璃 粘性带模型 虚拟裂缝闭合技术 |
title | Mode II Interlaminar Fracture Toughness of Flax/Glass/Epoxy Hybrid Composite Materials: An Experimental and Numerical Study |
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