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Indentation response of a 3D non-woven carbon-fibre composite
The indentation response of a 3D noninterlaced composite comprising three sets of orthogonal carbon-fibre tows in an epoxy matrix is investigated. The 3D composites have a near isotropic and ductile indentation response. The deformation mode includes the formation of multiple kinks in the tows align...
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Published in: | Journal of materials research 2018-02, Vol.33 (3), p.317-329 |
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creator | Das, Satyajit Kandan, Karthikeyan Kazemahvazi, Sohrab Wadley, Haydn N.G. Deshpande, Vikram S. |
description | The indentation response of a 3D noninterlaced composite comprising three sets of orthogonal carbon-fibre tows in an epoxy matrix is investigated. The 3D composites have a near isotropic and ductile indentation response. The deformation mode includes the formation of multiple kinks in the tows aligned with the indentation direction and shearing of the orthogonally oriented tows. Finite element (FE) calculations are also reported wherein tows in one direction are explicitly modeled with the other two sets of orthogonal tows and the matrix pockets treated as an effective homogenous medium. The calculations capture the indentation response in the direction of the explicitly modeled tows with excellent fidelity but under-predict the indentation strength in the other directions. In contrast to anisotropic and brittle laminated composites, 3D noninterlaced composites have a near isotropic and ductile indentation response making them strong candidates for application as materials to resist impact loading. |
doi_str_mv | 10.1557/jmr.2017.481 |
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The 3D composites have a near isotropic and ductile indentation response. The deformation mode includes the formation of multiple kinks in the tows aligned with the indentation direction and shearing of the orthogonally oriented tows. Finite element (FE) calculations are also reported wherein tows in one direction are explicitly modeled with the other two sets of orthogonal tows and the matrix pockets treated as an effective homogenous medium. The calculations capture the indentation response in the direction of the explicitly modeled tows with excellent fidelity but under-predict the indentation strength in the other directions. In contrast to anisotropic and brittle laminated composites, 3D noninterlaced composites have a near isotropic and ductile indentation response making them strong candidates for application as materials to resist impact loading.</description><identifier>ISSN: 0884-2914</identifier><identifier>EISSN: 2044-5326</identifier><identifier>DOI: 10.1557/jmr.2017.481</identifier><language>eng</language><publisher>New York, USA: Cambridge University Press</publisher><subject>Aircraft ; Applied and Technical Physics ; Biomaterials ; Carbon fiber reinforced plastics ; Carbon fibers ; Carbon-epoxy composites ; Composite materials ; Deformation ; Ductile-brittle transition ; Fiber composites ; Finite element method ; Impact loads ; Impact tests ; Indentation ; Inorganic Chemistry ; Invited Article ; Invited Articles ; Materials Engineering ; Materials research ; Materials Science ; Mathematical models ; Nanotechnology ; Polyethylene ; Polymer matrix composites ; Polymers ; Shearing ; Three dimensional composites ; Tomography ; Velocity ; Yarn</subject><ispartof>Journal of materials research, 2018-02, Vol.33 (3), p.317-329</ispartof><rights>Copyright © Materials Research Society 2018</rights><rights>The Materials Research Society 2018</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c377t-2a6a75ef70842b8426937d74eeb42a1919ecf7e50a42bcc5c8e6f840316e5a183</citedby><cites>FETCH-LOGICAL-c377t-2a6a75ef70842b8426937d74eeb42a1919ecf7e50a42bcc5c8e6f840316e5a183</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.proquest.com/docview/2176179680/fulltextPDF?pq-origsite=primo$$EPDF$$P50$$Gproquest$$H</linktopdf><linktohtml>$$Uhttps://www.proquest.com/docview/2176179680?pq-origsite=primo$$EHTML$$P50$$Gproquest$$H</linktohtml><link.rule.ids>314,778,782,11675,27911,27912,36047,44350,74650</link.rule.ids></links><search><creatorcontrib>Das, Satyajit</creatorcontrib><creatorcontrib>Kandan, Karthikeyan</creatorcontrib><creatorcontrib>Kazemahvazi, Sohrab</creatorcontrib><creatorcontrib>Wadley, Haydn N.G.</creatorcontrib><creatorcontrib>Deshpande, Vikram S.</creatorcontrib><title>Indentation response of a 3D non-woven carbon-fibre composite</title><title>Journal of materials research</title><addtitle>Journal of Materials Research</addtitle><addtitle>J. Mater. Res</addtitle><description>The indentation response of a 3D noninterlaced composite comprising three sets of orthogonal carbon-fibre tows in an epoxy matrix is investigated. The 3D composites have a near isotropic and ductile indentation response. The deformation mode includes the formation of multiple kinks in the tows aligned with the indentation direction and shearing of the orthogonally oriented tows. Finite element (FE) calculations are also reported wherein tows in one direction are explicitly modeled with the other two sets of orthogonal tows and the matrix pockets treated as an effective homogenous medium. The calculations capture the indentation response in the direction of the explicitly modeled tows with excellent fidelity but under-predict the indentation strength in the other directions. In contrast to anisotropic and brittle laminated composites, 3D noninterlaced composites have a near isotropic and ductile indentation response making them strong candidates for application as materials to resist impact loading.</description><subject>Aircraft</subject><subject>Applied and Technical Physics</subject><subject>Biomaterials</subject><subject>Carbon fiber reinforced plastics</subject><subject>Carbon fibers</subject><subject>Carbon-epoxy composites</subject><subject>Composite materials</subject><subject>Deformation</subject><subject>Ductile-brittle transition</subject><subject>Fiber composites</subject><subject>Finite element method</subject><subject>Impact loads</subject><subject>Impact tests</subject><subject>Indentation</subject><subject>Inorganic Chemistry</subject><subject>Invited Article</subject><subject>Invited Articles</subject><subject>Materials Engineering</subject><subject>Materials research</subject><subject>Materials Science</subject><subject>Mathematical models</subject><subject>Nanotechnology</subject><subject>Polyethylene</subject><subject>Polymer matrix composites</subject><subject>Polymers</subject><subject>Shearing</subject><subject>Three dimensional composites</subject><subject>Tomography</subject><subject>Velocity</subject><subject>Yarn</subject><issn>0884-2914</issn><issn>2044-5326</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><sourceid>M0C</sourceid><recordid>eNqFkE1LxDAQhoMouK7e_AEBr7YmadKkBw-yfi0seNFzSNPJ0sUmNekq_nuz7IIn8TAMwzzzDjwIXVJSUiHkzWaIJSNUllzRIzRjhPNCVKw-RjOiFC9YQ_kpOktpQwgVRPIZul36Dvxkpj54HCGNwSfAwWGDq3vsgy--wid4bE1s8-D6NgK2YRhD6ic4RyfOvCe4OPQ5ent8eF08F6uXp-XiblXYSsqpYKY2UoCTRHHW5qqbSnaSA7ScGdrQBqyTIIjJa2uFVVA7xUlFaxCGqmqOrva5YwwfW0iT3oRt9PmlZlTWVDa1Ipm63lM2hpQiOD3GfjDxW1Oid4J0FqR3gnQWlPFij6eM-TXE39A_-PIQb4Y29t0a_jn4ATqIdfc</recordid><startdate>20180214</startdate><enddate>20180214</enddate><creator>Das, Satyajit</creator><creator>Kandan, Karthikeyan</creator><creator>Kazemahvazi, Sohrab</creator><creator>Wadley, Haydn N.G.</creator><creator>Deshpande, Vikram S.</creator><general>Cambridge University Press</general><general>Springer International Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>0U~</scope><scope>1-H</scope><scope>3V.</scope><scope>7SR</scope><scope>7WY</scope><scope>7WZ</scope><scope>7XB</scope><scope>87Z</scope><scope>8BQ</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>8FK</scope><scope>8FL</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BEZIV</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>FRNLG</scope><scope>F~G</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>K60</scope><scope>K6~</scope><scope>KB.</scope><scope>L.-</scope><scope>L.0</scope><scope>M0C</scope><scope>PDBOC</scope><scope>PQBIZ</scope><scope>PQBZA</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>Q9U</scope><scope>S0W</scope></search><sort><creationdate>20180214</creationdate><title>Indentation response of a 3D non-woven carbon-fibre composite</title><author>Das, Satyajit ; Kandan, Karthikeyan ; Kazemahvazi, Sohrab ; Wadley, Haydn N.G. ; Deshpande, Vikram S.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c377t-2a6a75ef70842b8426937d74eeb42a1919ecf7e50a42bcc5c8e6f840316e5a183</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Aircraft</topic><topic>Applied and Technical Physics</topic><topic>Biomaterials</topic><topic>Carbon fiber reinforced plastics</topic><topic>Carbon fibers</topic><topic>Carbon-epoxy composites</topic><topic>Composite materials</topic><topic>Deformation</topic><topic>Ductile-brittle transition</topic><topic>Fiber composites</topic><topic>Finite element method</topic><topic>Impact loads</topic><topic>Impact tests</topic><topic>Indentation</topic><topic>Inorganic Chemistry</topic><topic>Invited Article</topic><topic>Invited Articles</topic><topic>Materials Engineering</topic><topic>Materials research</topic><topic>Materials Science</topic><topic>Mathematical models</topic><topic>Nanotechnology</topic><topic>Polyethylene</topic><topic>Polymer matrix composites</topic><topic>Polymers</topic><topic>Shearing</topic><topic>Three dimensional composites</topic><topic>Tomography</topic><topic>Velocity</topic><topic>Yarn</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Das, Satyajit</creatorcontrib><creatorcontrib>Kandan, Karthikeyan</creatorcontrib><creatorcontrib>Kazemahvazi, Sohrab</creatorcontrib><creatorcontrib>Wadley, Haydn N.G.</creatorcontrib><creatorcontrib>Deshpande, Vikram S.</creatorcontrib><collection>CrossRef</collection><collection>Global News & ABI/Inform Professional</collection><collection>Trade PRO</collection><collection>ProQuest Central (Corporate)</collection><collection>Engineered Materials Abstracts</collection><collection>ABI/INFORM Collection (ProQuest)</collection><collection>ABI/INFORM Global (PDF only)</collection><collection>ProQuest Central (purchase pre-March 2016)</collection><collection>ABI/INFORM Collection</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni) (purchase pre-March 2016)</collection><collection>ABI/INFORM Collection (Alumni Edition)</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central</collection><collection>Business Premium Collection</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>Business Premium Collection (Alumni)</collection><collection>ABI/INFORM Global (Corporate)</collection><collection>SciTech Premium Collection</collection><collection>Materials Research Database</collection><collection>ProQuest Business Collection (Alumni Edition)</collection><collection>ProQuest Business Collection</collection><collection>Materials Science Database</collection><collection>ABI/INFORM Professional Advanced</collection><collection>ABI/INFORM Professional Standard</collection><collection>ABI/INFORM Global</collection><collection>Materials science collection</collection><collection>One Business</collection><collection>ProQuest One Business (Alumni)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central Basic</collection><collection>DELNET Engineering & Technology Collection</collection><jtitle>Journal of materials research</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Das, Satyajit</au><au>Kandan, Karthikeyan</au><au>Kazemahvazi, Sohrab</au><au>Wadley, Haydn N.G.</au><au>Deshpande, Vikram S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Indentation response of a 3D non-woven carbon-fibre composite</atitle><jtitle>Journal of materials research</jtitle><stitle>Journal of Materials Research</stitle><addtitle>J. Mater. Res</addtitle><date>2018-02-14</date><risdate>2018</risdate><volume>33</volume><issue>3</issue><spage>317</spage><epage>329</epage><pages>317-329</pages><issn>0884-2914</issn><eissn>2044-5326</eissn><abstract>The indentation response of a 3D noninterlaced composite comprising three sets of orthogonal carbon-fibre tows in an epoxy matrix is investigated. The 3D composites have a near isotropic and ductile indentation response. The deformation mode includes the formation of multiple kinks in the tows aligned with the indentation direction and shearing of the orthogonally oriented tows. Finite element (FE) calculations are also reported wherein tows in one direction are explicitly modeled with the other two sets of orthogonal tows and the matrix pockets treated as an effective homogenous medium. The calculations capture the indentation response in the direction of the explicitly modeled tows with excellent fidelity but under-predict the indentation strength in the other directions. In contrast to anisotropic and brittle laminated composites, 3D noninterlaced composites have a near isotropic and ductile indentation response making them strong candidates for application as materials to resist impact loading.</abstract><cop>New York, USA</cop><pub>Cambridge University Press</pub><doi>10.1557/jmr.2017.481</doi><tpages>13</tpages></addata></record> |
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subjects | Aircraft Applied and Technical Physics Biomaterials Carbon fiber reinforced plastics Carbon fibers Carbon-epoxy composites Composite materials Deformation Ductile-brittle transition Fiber composites Finite element method Impact loads Impact tests Indentation Inorganic Chemistry Invited Article Invited Articles Materials Engineering Materials research Materials Science Mathematical models Nanotechnology Polyethylene Polymer matrix composites Polymers Shearing Three dimensional composites Tomography Velocity Yarn |
title | Indentation response of a 3D non-woven carbon-fibre composite |
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