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               <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>
               <dc:description>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</dc:description>
               <dc:description>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</dc:description>
               <dc:date>2025-02-04T00:07:04Z</dc:date>
               <dc:date>2025-02-04T00:07:04Z</dc:date>
               <dc:date>2019-07</dc:date>
               <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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