DC FieldValueLanguage
dc.contributor.authorRose, Philip-
dc.contributor.authorLinke, Markus-
dc.contributor.authorBusquets Mataix, David-
dc.date.accessioned2025-12-17T09:55:11Z-
dc.date.available2025-12-17T09:55:11Z-
dc.date.issued2025-12-16-
dc.identifier.issn1873-7315en_US
dc.identifier.urihttps://hdl.handle.net/20.500.12738/18557-
dc.description.abstractThis study investigates the influence of layup configuration on the failure behavior of composite bonded joints. Experimental results from quasi-static tests reveal that specimens with a 0°-oriented ply in contact with the adhesive consistently achieve higher fracture loads and exhibit simpler failure mechanisms compared to 45° configuration, where the crack propagates into the adherends and shows complex damage progression. Numerical simulations using cohesive zone modeling are conducted to predict this behavior. A method is applied to ensure sufficient resolution of the cohesive zone, and the influence of mesh size on predictive accuracy is assessed. The results show that at least nine cohesive elements are required within the cohesive zone for convergence in fracture load and accurate damage progression. The presented modeling approach accurately predicts both crack paths and fracture loads, particularly for complex failure scenarios. However, limitations remain for adhesive-layer-only failure due to sensitivity to surface pre-treatment and associated parameter uncertainty. The findings highlight the need for layup-sensitive modeling strategies and mesh resolution when analyzing bonded composite structures.en
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.relation.ispartofEngineering fracture mechanicsen_US
dc.subjectLayup-effecten_US
dc.subjectCracked-Lap-Shear (CLS)en_US
dc.subjectCarbon-Fiber-Reinforced-Plastics (CFRP)en_US
dc.subjectComposite bonded jointsen_US
dc.subjectcohesive-zone method (CZM)en_US
dc.subjectIM7/8552en_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleExperimental investigation and numerical modeling of the layup-specific damage behavior of composite bonded joints under mixed-mode loadingen
dc.typeArticleen_US
dc.description.versionPeerRevieweden_US
tuhh.container.volume332en_US
tuhh.oai.showtrueen_US
tuhh.publication.instituteFakultät Luftfahrt- und Fahrzeugsystemeen_US
tuhh.publisher.doi10.1016/j.engfracmech.2025.111769-
tuhh.type.opus(wissenschaftlicher) Artikel-
dc.rights.cchttps://creativecommons.org/licenses/by-nc/4.0/en_US
dc.type.casraiJournal Article-
dc.type.diniarticle-
dc.type.driverarticle-
dc.type.statusinfo:eu-repo/semantics/publishedVersionen_US
dcterms.DCMITypeText-
local.comment.externalarticle number: 111769en_US
item.cerifentitytypePublications-
item.languageiso639-1en-
item.creatorOrcidRose, Philip-
item.creatorOrcidLinke, Markus-
item.creatorOrcidBusquets Mataix, David-
item.openairetypeArticle-
item.fulltextNo Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_6501-
item.creatorGNDRose, Philip-
item.creatorGNDLinke, Markus-
item.creatorGNDBusquets Mataix, David-
item.grantfulltextnone-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau (ehemalig, aufgelöst 10.2025)-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau (ehemalig, aufgelöst 10.2025)-
crisitem.author.orcid0000-0002-0842-6896-
crisitem.author.parentorgFakultät Technik und Informatik (ehemalig, aufgelöst 10.2025)-
crisitem.author.parentorgFakultät Technik und Informatik (ehemalig, aufgelöst 10.2025)-
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