Damage tolerance of double lap joins under transverse impact
| dc.contributor.author | Paul, Aakash | |
| dc.contributor.author | Xu, Xiaodong | |
| dc.contributor.author | Shimizu, Takayuki | |
| dc.contributor.author | Wisnom, Michael R. | |
| dc.date.accessioned | 2025-12-09T11:36:43Z | |
| dc.date.available | 2025-12-09T11:36:43Z | |
| dc.date.freetoread | 2025-12-09 | |
| dc.date.issued | 2026-01 | |
| dc.date.pubOnline | 2025-11-13 | |
| dc.description.abstract | Low 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.journalName | Journal of Composite Materials | |
| dc.description.sponsorship | The 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.extent | pp. xx-xx | |
| dc.identifier.citation | Paul 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 00219983251397503 | en_UK |
| dc.identifier.eissn | 1530-793X | |
| dc.identifier.elementsID | 866659 | |
| dc.identifier.issn | 0021-9983 | |
| dc.identifier.issueNo | ahead-of-print | |
| dc.identifier.paperNo | 00219983251397503 | |
| dc.identifier.uri | https://doi.org/10.1177/00219983251397503 | |
| dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/24709 | |
| dc.identifier.volumeNo | ahead-of-print | |
| dc.language | English | |
| dc.language.iso | en | |
| dc.publisher | Sage | en_UK |
| dc.publisher.uri | https://journals.sagepub.com/doi/10.1177/00219983251397503 | |
| dc.rights | Attribution 4.0 International | en |
| dc.rights.uri | http://creativecommons.org/licenses/by/4.0/ | |
| dc.subject | bonding | en_UK |
| dc.subject | delamination | en_UK |
| dc.subject | joints | en_UK |
| dc.subject | finite element analysis (FEA) | en_UK |
| dc.subject | low velocity impact | en_UK |
| dc.subject | 40 Engineering | en_UK |
| dc.subject | 4016 Materials Engineering | en_UK |
| dc.subject | 4001 Aerospace Engineering | en_UK |
| dc.subject | Materials | en_UK |
| dc.subject | 4005 Civil engineering | en_UK |
| dc.subject | 4017 Mechanical engineering | en_UK |
| dc.title | Damage tolerance of double lap joins under transverse impact | en_UK |
| dc.type | Article | |
| dc.type.subtype | Journal Article | |
| dcterms.dateAccepted | 2025-10-27 |
