<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/style.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-04-19T19:19:11Z</responseDate><request verb="GetRecord" identifier="oai:www.recercat.cat:10256/26055" metadataPrefix="qdc">https://recercat.cat/oai/request</request><GetRecord><record><header><identifier>oai:recercat.cat:10256/26055</identifier><datestamp>2025-02-04T00:07:04Z</datestamp><setSpec>com_2072_452955</setSpec><setSpec>com_2072_2054</setSpec><setSpec>col_2072_453061</setSpec></header><metadata><qdc:qualifieddc xmlns:qdc="http://dspace.org/qualifieddc/" xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:dcterms="http://purl.org/dc/terms/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:doc="http://www.lyncode.com/xoai" xsi:schemaLocation="http://purl.org/dc/elements/1.1/ http://dublincore.org/schemas/xmls/qdc/2006/01/06/dc.xsd http://purl.org/dc/terms/ http://dublincore.org/schemas/xmls/qdc/2006/01/06/dcterms.xsd http://dspace.org/qualifieddc/ http://www.ukoln.ac.uk/metadata/dcmi/xmlschema/qualifieddc.xsd">
   <dc:title>Mitigating the weak impact response of thin-ply based thin laminates through an unsymmetrical laminate design incorporating intermediate grade plies</dc:title>
   <dc:creator>Sasikumar, Aravind</dc:creator>
   <dc:creator>Trias Mansilla, Daniel</dc:creator>
   <dc:creator>Costa i Balanzat, Josep</dc:creator>
   <dc:creator>Singery, Vicky</dc:creator>
   <dc:creator>Linde, Peter</dc:creator>
   <dc:subject>Assaigs de materials</dc:subject>
   <dc:subject>Materials laminats</dc:subject>
   <dc:subject>Mecànica de fractura</dc:subject>
   <dc:subject>Materials compostos</dc:subject>
   <dc:subject>Materials -- Testing</dc:subject>
   <dc:subject>Laminated materials</dc:subject>
   <dc:subject>Fracture mechanics</dc:subject>
   <dc:subject>Composite materials</dc:subject>
   <dcterms:abstract>With aeronautic industries focussing on thinner structures and reducing manufacturing costs, recent research has been dedicated to the impact and post impact response of thin laminates (&lt;2 mm) made of textile fabric composites. A recent study revealed that thin laminates based on thin plies exhibit extensive fibre failure and a reduced compression after impact strength. To mitigate this weakness, we propose a novel laminate concept based on combining plies of different thicknesses in an unsymmetrical configuration (intermediate grade plies are located only at the bottom of the laminate, i.e., the non-impacted face). C-scan inspection on impacted and quasi-statically indented specimens, allowed the damage sequence of the proposed unsymmetrical hybrid laminate to be compared with that of the thin-ply baseline. The hybrid laminate with intermediate plies at the bottom, delayed and reduced the fibre damage, decreased the projected delamination area and led to a 30% increase in the compression after impact strength in contrast to the thin-ply baseline laminate</dcterms:abstract>
   <dcterms:abstract>The first author would like to thank the Generalitat de Catalunya for the FI-DGR pre-doctoral grant (2018 FI-B2 00118). his work has been supported by the Spanish Ministerio de Economía y Competitividad through the grant coded MAT2015-69491-C3-1-R, supported by FEDER/E</dcterms:abstract>
   <dcterms:dateAccepted>2025-02-04T00:07:04Z</dcterms:dateAccepted>
   <dcterms:available>2025-02-04T00:07:04Z</dcterms:available>
   <dcterms:created>2025-02-04T00:07:04Z</dcterms:created>
   <dcterms:issued>2019-07</dcterms:issued>
   <dc:type>info:eu-repo/semantics/article</dc:type>
   <dc:type>info:eu-repo/semantics/acceptedVersion</dc:type>
   <dc:type>peer-reviewed</dc:type>
   <dc:identifier>http://hdl.handle.net/10256/26055</dc:identifier>
   <dc:relation>info:eu-repo/semantics/altIdentifier/doi/10.1016/j.compstruct.2019.03.069</dc:relation>
   <dc:relation>info:eu-repo/semantics/altIdentifier/issn/0263-8223</dc:relation>
   <dc:relation>info:eu-repo/semantics/altIdentifier/eissn/1879-1085</dc:relation>
   <dc:relation>MAT2015-69491-C3-1-R</dc:relation>
   <dc:relation>info:eu-repo/grantAgreement/MINECO//MAT2015-69491-C3-1-R/ES/HIBRIDACION LOCAL DE MATERIALES COMPUESTOS LAMINADOS PARA MEJORAR SU TOLERANCIA AL DAÑO/</dc:relation>
   <dc:rights>Reconeixement-NoComercial-SenseObraDerivada 4.0 Internacional</dc:rights>
   <dc:rights>info:eu-repo/semantics/openAccess</dc:rights>
   <dc:publisher>Elsevier</dc:publisher>
   <dc:source>© Composite Structures, 2019, vol. 220, p. 93-104</dc:source>
   <dc:source>Articles publicats (D-EMCI)</dc:source>
   <dc:source>Sasikumar, Aravind Trias Mansilla, Daniel Costa i Balanzat, Josep Singery, Vicky Linde, Peter 2019 Mitigating the weak impact response of thin-ply based thin laminates through an unsymmetrical laminate design incorporating intermediate grade plies Composite Structures 220  93 104</dc:source>
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