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Damage tolerance of double lap joins under transverse impact

dc.contributor.authorPaul, Aakash
dc.contributor.authorXu, Xiaodong
dc.contributor.authorShimizu, Takayuki
dc.contributor.authorWisnom, Michael R.
dc.date.accessioned2025-12-09T11:36:43Z
dc.date.available2025-12-09T11:36:43Z
dc.date.freetoread2025-12-09
dc.date.issued2026-01
dc.date.pubOnline2025-11-13
dc.description.abstractLow velocity impact on adhesive joints represents a worst-case scenario in a bonded structure, so their residual tensile strength is a crucial indicator for damage tolerance of the bonded structures. In this study, narrow double lap joints were tested under two transverse impact energy levels to provide a conservative assessment of damage tolerance. Residual tensile tests were conducted after impact, showing a 49% reduction of pristine joint strength after a 2J impact, and a further reduction (57% of pristine joint strength) post a 3J impact. Residual tensile strength of impacted double lap joints was found to correlate to that of the joints with a similar artificial defect length and location near the inner adherend. The failure mechanisms in the double lap joints were explained via X-ray computed tomography and high-speed photography. 2D FE models were developed using surface interactions based on a virtual crack closure technique in ABAQUS Standard. The FE models capture the residual tensile strength reduction trend, confirming the underlying mixed-mode fracture-controlled failure mode influenced by the asymmetrical damage and loading.
dc.description.journalNameJournal of Composite Materials
dc.description.sponsorshipThe author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was supported by Mitsubishi Heavy Industries LTD
dc.format.extentpp. xx-xx
dc.identifier.citationPaul A, Xu X, Shimizu T, Wisnom MR. (2025) Damage tolerance of double lap joins under transverse impact. Journal of Composite Materials, Available online 13 November 2025, Article number 00219983251397503en_UK
dc.identifier.eissn1530-793X
dc.identifier.elementsID866659
dc.identifier.issn0021-9983
dc.identifier.issueNoahead-of-print
dc.identifier.paperNo00219983251397503
dc.identifier.urihttps://doi.org/10.1177/00219983251397503
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/24709
dc.identifier.volumeNoahead-of-print
dc.languageEnglish
dc.language.isoen
dc.publisherSageen_UK
dc.publisher.urihttps://journals.sagepub.com/doi/10.1177/00219983251397503
dc.rightsAttribution 4.0 Internationalen
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectbondingen_UK
dc.subjectdelaminationen_UK
dc.subjectjointsen_UK
dc.subjectfinite element analysis (FEA)en_UK
dc.subjectlow velocity impacten_UK
dc.subject40 Engineeringen_UK
dc.subject4016 Materials Engineeringen_UK
dc.subject4001 Aerospace Engineeringen_UK
dc.subjectMaterialsen_UK
dc.subject4005 Civil engineeringen_UK
dc.subject4017 Mechanical engineeringen_UK
dc.titleDamage tolerance of double lap joins under transverse impacten_UK
dc.typeArticle
dc.type.subtypeJournal Article
dcterms.dateAccepted2025-10-27

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