DC ElementWertSprache
dc.contributor.authorRose, Philip-
dc.contributor.authorLinke, Markus-
dc.contributor.authorBusquets, David-
dc.date.accessioned2024-03-04T10:38:02Z-
dc.date.available2024-03-04T10:38:02Z-
dc.date.issued2024-01-01-
dc.identifier.issn1742-6596en_US
dc.identifier.urihttp://hdl.handle.net/20.500.12738/14980-
dc.description.abstractThe Cracked Lap Shear (CLS) specimen allows a mixed-mode loading condition to be generated without a special test fixture using a simple tensile test. The mixed-mode ratio generated is nearly constant over a wide range of crack growth and is representative of the loading conditions in many structural applications of bonded joints. However, this specimen is not standardised, leading to very dissimilar specimen designs in the literature. In this study, the primary design parameter is the sample width in terms of its application for adhesive characterisation, with a typical layup having a 0° layer in contact with the bond line. The results of quasi-static and fatigue tests using varying specimen widths between 5 mm and 40 mm emphasise the specimen width's influence. Moreover, CLS specimens with the same layup but without an adhesive layer between the adherends are investigated to study the effects of width scaling without a toughened adhesive bond. While the static tests show a linear relationship between specimen width and joint strength, it is different in fatigue tests, where the crack growth rate increases with decreasing specimen width, both for specimens with and without adhesive bond between the joining partners.en
dc.description.sponsorshipBundesministerium für Wirtschaft und Klimaschutzen_US
dc.language.isoenen_US
dc.publisherIOP Publishingen_US
dc.relation.ispartofJournal of physics / Conference Seriesen_US
dc.subject.ddc620: Ingenieurwissenschaftenen_US
dc.titleInvestigation of the influence of design parameters onto the cracked lap shear specimenen
dc.typeinProceedingsen_US
dc.relation.conferenceInternational Conference of Engineering Against Failure 2023en_US
dc.description.versionPeerRevieweden_US
tuhh.container.issue1en_US
tuhh.container.startpage012014en_US
tuhh.container.volume2692en_US
tuhh.oai.showtrueen_US
tuhh.publication.instituteDepartment Fahrzeugtechnik und Flugzeugbauen_US
tuhh.publication.instituteFakultät Technik und Informatiken_US
tuhh.publisher.doi10.1088/1742-6596/2692/1/012014-
tuhh.type.opusInProceedings (Aufsatz / Paper einer Konferenz etc.)-
dc.relation.projectVerbundvorhaben: Joining with predictable Damage Tolerance; Teilvorhaben: CrackJump - Verbesserte Schadenstoleranz von Klebeverbindungen durch Vorhersage des Einflusses von intralaminarem Ermüdungsrisswachstum in CFK-Fügepartnernen_US
dc.rights.cchttps://creativecommons.org/licenses/by/3.0/en_US
dc.type.casraiConference Paper-
dc.type.dinicontributionToPeriodical-
dc.type.drivercontributionToPeriodical-
dc.type.statusinfo:eu-repo/semantics/publishedVersionen_US
dcterms.DCMITypeText-
tuhh.container.articlenumber012014-
local.comment.externalarticle number: 012014en_US
item.openairecristypehttp://purl.org/coar/resource_type/c_5794-
item.fulltextNo Fulltext-
item.grantfulltextnone-
item.openairetypeinProceedings-
item.creatorGNDRose, Philip-
item.creatorGNDLinke, Markus-
item.creatorGNDBusquets, David-
item.languageiso639-1en-
item.creatorOrcidRose, Philip-
item.creatorOrcidLinke, Markus-
item.creatorOrcidBusquets, David-
item.cerifentitytypePublications-
crisitem.project.funderBundesministerium für Wirtschaft und Klimaschutz-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau-
crisitem.author.deptDepartment Fahrzeugtechnik und Flugzeugbau-
crisitem.author.orcid0000-0002-0842-6896-
crisitem.author.parentorgFakultät Technik und Informatik-
crisitem.author.parentorgFakultät Technik und Informatik-
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