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dc.contributor.authorChen, D
dc.contributor.authorLuo, Q
dc.contributor.authorMENG, MAOZHOU
dc.contributor.authorSun, G
dc.date.accessioned2019-08-01T11:28:58Z
dc.date.available2019-08-01T11:28:58Z
dc.date.issued2019-11-01
dc.identifier.issn0961-9526
dc.identifier.other107191
dc.identifier.urihttp://hdl.handle.net/10026.1/14735
dc.description.abstract

This work investigates the effects of carbon/glass/basalt hybridization and fabric structure on the low velocity impact resistance of fibre reinforced plastic composites. Interply hybrid specimens used in the study were fabricated in a sandwich-like stacking sequence using a vacuum assisted resin infusion molding technique. Low velocity impact tests were carried out to study effects of hybridization and fabric structure on the impact resistance of composite laminates. A continuum damage mechanical model was developed and validated for non-hybrid woven fabric laminates at different impact energy levels. Residual damage characteristics in the cross-sectional view were identified using a 3D surface scanning system and an X-ray computed tomography (CT) method. On the basis of experimental results, numerical simulation was conducted to analyse the damage mechanisms of the hybrid laminates. Experimental results showed that: (a) hybrid laminates with carbon fibre as the core exhibited superior impact resistance for sandwich-like stacking sequence; (b) similar impact behaviors appeared for carbon laminates hybrid with either basalt or glass fibre; (c) for basalt fibre, weave fabric composite laminates exhibited better energy absorption capability and deformation resistance than cross-ply laminates reinforced by unidirectional fabrics.

dc.format.extent107191-107191
dc.languageen
dc.language.isoen
dc.publisherElsevier
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rightsAttribution-NonCommercial-ShareAlike 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
dc.subject7 Affordable and Clean Energy
dc.titleLow velocity impact behavior of interlayer hybrid composite laminates with carbon/glass/basalt fibres
dc.typejournal-article
dc.typeJournal Article
plymouth.volume176
plymouth.publication-statusPublished
plymouth.journalComposites Part B: Engineering
dc.identifier.doi10.1016/j.compositesb.2019.107191
plymouth.organisational-group/Plymouth
plymouth.organisational-group/Plymouth/Faculty of Science and Engineering
plymouth.organisational-group/Plymouth/Faculty of Science and Engineering/School of Engineering, Computing and Mathematics
plymouth.organisational-group/Plymouth/REF 2021 Researchers by UoA
plymouth.organisational-group/Plymouth/REF 2021 Researchers by UoA/UoA12 Engineering
plymouth.organisational-group/Plymouth/Users by role
plymouth.organisational-group/Plymouth/Users by role/Academics
dcterms.dateAccepted2019-07-09
dc.rights.embargodate2020-7-9
dc.rights.embargoperiodNot known
rioxxterms.versionofrecord10.1016/j.compositesb.2019.107191
rioxxterms.licenseref.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/
rioxxterms.licenseref.startdate2019-11-01
rioxxterms.typeJournal Article/Review


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