Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/31727
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dc.contributor.authorCheung, MC-
dc.contributor.authorDjordjevic, N-
dc.contributor.authorWorrall, C-
dc.contributor.authorVignjevic, R-
dc.contributor.authorKazilas, M-
dc.contributor.authorHughes, K-
dc.date.accessioned2025-08-11T17:59:41Z-
dc.date.available2025-08-11T17:59:41Z-
dc.date.issued2025-07-26-
dc.identifierORCiD: Man Chi Cheung https://orcid.org/0009-0000-3428-6965-
dc.identifierORCiD: Nenad Djordjevic https://orcid.org/0000-0002-2729-5721-
dc.identifierORCiD: Chris Worrall https://orcid.org/0000-0002-0284-638X-
dc.identifierORCiD: Rade Vignjević https://orcid.org/0000-0002-4677-068X-
dc.identifierORCiD: Mihalis Kazilas https://orcid.org/0000-0001-6613-9118-
dc.identifierORCiD: Kevin Hughes https://orcid.org/0000-0002-8522-7903-
dc.identifierArticle number: 3512-
dc.identifier.citationCheung, M.C. et al. (2025) 'Conceptual Design of a Hybrid Composite to Metal Joint for Naval Vessels Applications', Materials, 18 (15), 3512, pp. 1 - 26. doi: 10.3390/ma18153512.en_US
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/31727-
dc.descriptionData Availability Statement: The data presented in this study are available on request from the corresponding author due to legal reasons.en_US
dc.description.abstractThis paper describes the development of a new hybrid composite for the metal joints of aluminium and glass fibre composite adherents. The aluminium adherend is manufactured using friction stir-formed studs that are inserted into the composite adherend in the through-thickness direction during the composite manufacturing process, where the dry fibres are displaced to accommodate the studs before the resin infusion process. The materials used were AA6082-T6 aluminium and plain-woven E-glass fabric reinforced epoxy, with primary applications in naval vessels. This joining approach offers a cost-effective solution that does not require complicated onsite welding. The joint design was developed based on a simulation test program with finite element analysis, followed by experimental characterisation and validation. The design solution was analysed in terms of the force displacement response, sequence of load transfer, and characterisation of the joint failure modes.en_US
dc.description.sponsorshipThis publication was made possible by the sponsorship and support of TWI’s Core Research Programme (CRP). This work was enabled through and undertaken at the National Structural Integrity Research Centre (NSIRC), a postgraduate engineering facility for industry-led research into structural integrity established and managed by TWI through a network of both national and international universities.en_US
dc.format.extent1 - 26-
dc.format.mediumElectronic-
dc.languageEnglish-
dc.language.isoen_USen_US
dc.publisherMDPIen_US
dc.rightsCreative Commons Attribution 4.0 International-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.subjectfriction stir spot weldingen_US
dc.subjectglass fibre fabricen_US
dc.subjectsimulation-led designen_US
dc.subjectfinite element methodsen_US
dc.titleConceptual Design of a Hybrid Composite to Metal Joint for Naval Vessels Applicationsen_US
dc.typeArticleen_US
dc.date.dateAccepted2025-07-23-
dc.identifier.doihttps://doi.org/10.3390/ma18153512-
dc.relation.isPartOfMaterials-
pubs.issue15-
pubs.publication-statusPublished online-
pubs.volume18-
dc.identifier.eissn1996-1944-
dc.rights.licensehttps://creativecommons.org/licenses/by/4.0/legalcode.en-
dcterms.dateAccepted2025-07-23-
dc.rights.holderThe authors-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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