Delamination migration in CFRP laminates under mode I loading

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dc.contributor.author Ramji, Amit
dc.contributor.author Xu, Yigeng
dc.contributor.author Yasaee, Mehdi
dc.contributor.author Grasso, Marzio
dc.contributor.author Webb, Philip
dc.date.accessioned 2020-02-12T14:59:44Z
dc.date.available 2020-02-12T14:59:44Z
dc.date.issued 2020-02-10
dc.identifier.citation Ramji A, Xu Y, Yasaee M, et al., (2020) Delamination migration in CFRP laminates under mode I loadin. Composites Science and Technology, Available online 10 February 2020, Article number 108067 en_UK
dc.identifier.issn 0266-3538
dc.identifier.uri https://doi.org/10.1016/j.compscitech.2020.108067
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/15124
dc.description.abstract This paper focuses on the effect of interfacial fibre orientation and interleaved veil on the delamination migration of carbon fibre reinforced polymer laminates under Mode I loading. Double cantilever beam specimens with midplane interfacial fibre orientations of 0/0, 90/90, 0/90, 0/45 and 90/45 were tested under two conditions: one with interleaved thermoplastic polyphenylene sulfide veil at the midplane and one without. Results show that, except for the 0/0 configuration, all other orientations exhibit varying levels of migration associated with the interfacial fibre orientation and veil interleaving. The apparent fracture toughness determined with the modified compliance calibration method is closely related to the delamination migration and hence a structural energy dissipation measure dependent on interfacial fibre orientation and the interleaved veil. Distributions of the fibre and matrix materials around the delamination front are found to be closely related to the delamination migration behaviour along its path. The experimental observation and rationalisation presented in this paper provide further knowledge regarding delamination migration and its correlation to the apparent fracture toughness, which is of direct relevance to the damage tolerance design of laminated composite components en_UK
dc.language.iso en en_UK
dc.publisher Elsevier en_UK
dc.rights Attribution-NonCommercial-NoDerivatives 4.0 International *
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/4.0/ *
dc.subject Delamination en_UK
dc.subject Fracture toughness en_UK
dc.subject Damage tolerance en_UK
dc.subject Fibre bridging en_UK
dc.subject Fractography en_UK
dc.title Delamination migration in CFRP laminates under mode I loading en_UK
dc.type Article en_UK


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