Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/150730
Full metadata record
DC FieldValueLanguage
dc.contributor.authorLiu, Zheen_US
dc.contributor.authorLi, Peifengen_US
dc.contributor.authorSrikanth, Narasimaluen_US
dc.date.accessioned2021-06-08T03:47:42Z-
dc.date.available2021-06-08T03:47:42Z-
dc.date.issued2019-
dc.identifier.citationLiu, Z., Li, P. & Srikanth, N. (2019). Effect of delamination on the flexural response of [+45/−45/0]2s carbon fibre reinforced polymer laminates. Composite Structures, 209, 93-102. https://dx.doi.org/10.1016/j.compstruct.2018.10.049en_US
dc.identifier.issn0263-8223en_US
dc.identifier.urihttps://hdl.handle.net/10356/150730-
dc.description.abstractThe damage arising in the manufacturing or service operation can result in the degradation in mechanical properties or even structural failure in composite laminates. This work investigated the flexural behaviour of [+45/−45/0]2s carbon fibre reinforced polymer laminates with the artificially embedded delamination (pre-delamination) at different interfaces. After static flexural experiments, the internal 3D damage including various failure modes was characterised and quantified in the X-ray microtomography. It was found that regardless of the pre-delamination, similar in-ply (fibre failure, matrix cracking and fibre/matrix debonding) and interlaminar (delamination) failure modes occur dominantly in the outer ply group of the compression zone in all the laminates. However, the pre-delamination and its location have the influence on both the distribution and size of the 3D damage, and thus on the flexural properties. The flexural strength that is reduced by pre-delamination is the most (least) sensitive to the pre-delamination embedded at the third (ninth) interface.en_US
dc.description.sponsorshipMinistry of Defence (MINDEF)en_US
dc.description.sponsorshipNanyang Technological Universityen_US
dc.language.isoenen_US
dc.relationMINDEF-NTU-JPP/12/01/02en_US
dc.relation.ispartofComposite Structuresen_US
dc.rights© 2018 Elsevier Ltd. All rights reserved.en_US
dc.subjectEngineering::Mechanical engineeringen_US
dc.titleEffect of delamination on the flexural response of [+45/−45/0]2s carbon fibre reinforced polymer laminatesen_US
dc.typeJournal Articleen
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.contributor.researchEnergy Research Institute @ NTU (ERI@N)en_US
dc.identifier.doi10.1016/j.compstruct.2018.10.049-
dc.identifier.scopus2-s2.0-85055751792-
dc.identifier.volume209en_US
dc.identifier.spage93en_US
dc.identifier.epage102en_US
dc.subject.keywordsLaminatesen_US
dc.subject.keywordsMechanical Propertiesen_US
dc.description.acknowledgementThis work was financially supported by the Ministry of Defence Singapore – Nanyang Technological University (NTU) Joint Applied R&D Cooperation (JPP) Programme (Grant No.: MINDEF-NTU-JPP/12/01/02). ZL acknowledges the NTU Interdisciplinary Graduate School Research Student Scholarship.en_US
item.grantfulltextnone-
item.fulltextNo Fulltext-
Appears in Collections:MAE Journal Articles

Page view(s)

78
Updated on Jan 24, 2022

Google ScholarTM

Check

Altmetric


Plumx

Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.