<?xml version="1.0" encoding="UTF-8"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-10-18T23:47:35Z</responseDate><request verb="GetRecord" identifier="oai:ebyu-rdlopen.rawdatalibrary.net:ebyu/14892" metadataPrefix="oai_dc">https://ebyu-rdlopen.rawdatalibrary.net/oai/request</request><GetRecord><record><header><identifier>oai:ebyu-rdlopen.rawdatalibrary.net:ebyu/14892</identifier><datestamp>2026-10-18T20:39:21Z</datestamp><setSpec>openaire</setSpec><setSpec>driver</setSpec><setSpec>com_ebyu_10000</setSpec><setSpec>col_ebyu_10001</setSpec></header><metadata><oai_dc:dc xmlns:oai_dc="http://www.openarchives.org/OAI/2.0/oai_dc/" xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd"><dc:title>Effects of unbalance on the adhesively bonded composites-aluminium joints</dc:title><dc:creator>Gültekin, KürŞat</dc:creator><dc:creator>Akpinar, Salih</dc:creator><dc:creator>Özel, Adnan</dc:creator><dc:creator>Öner, GülŞah Alar</dc:creator><dc:subject>Adhesion</dc:subject><dc:subject>carbon fibre</dc:subject><dc:subject>finite element analysis (FEA)</dc:subject><dc:subject>layered structures</dc:subject><dc:subject>mechanical testing</dc:subject><dc:subject>Aluminum</dc:subject><dc:subject>Aluminum alloys</dc:subject><dc:subject>Carbon fibers</dc:subject><dc:subject>Numerical methods</dc:subject><dc:subject>Aluminium adherend</dc:subject><dc:subject>Carbon/epoxy composites</dc:subject><dc:subject>Constant thickness</dc:subject><dc:subject>Four-point bending test</dc:subject><dc:subject>Nonlinear finite element method</dc:subject><dc:subject>Numerical results</dc:subject><dc:subject>Structural adhesive</dc:subject><dc:subject>Finite element method</dc:subject><dc:description>This article presents the experimental and numerical results of adhesively bonded hybrid single-lap joint (SLJ) geometry with different configurations of lower and upper adherends subject to a four-point bending test. AA2024-T3 aluminium alloy and carbon/epoxy composites with different lamina numbers and four different stacking angles as adherend and two-part liquid, structural adhesive DP 125 as paste adhesive were used. In the experimental studies, three different types of SLJs were produced using lower material that had a constant thickness of AA2024-T3 aluminium alloy and upper material of composite material that had different numbers of layers and four different stacking sequences ([0], [0/90], [45/−45], [0/45/−45/90]). In the numerical analysis, stress analyses of the SLJs were performed with a three-dimensional non-linear finite element method and the composite adherends were assumed to behave as linearly elastic materials, while the adhesive and aluminium adherend were assumed to be non-linear. Consequently, the change of stacking sequence and thickness of the composite in adhesively bonded SLJs altered the location of the neutral axis in the joint. This situation substantially influences the load-carrying capacity of the joint. © 2017 Taylor &amp; Francis.</dc:description><dc:publisher>Taylor and Francis Inc.</dc:publisher><dc:date>2017</dc:date><dc:type>Article</dc:type><dc:identifier>https://rdlopen.rawdatalibrary.net/r/ebyu/14892</dc:identifier><dc:identifier>https://doi.org/10.1080/00218464.2015.1136998</dc:identifier><dc:identifier>0021-8464</dc:identifier><dc:language>en</dc:language><dc:relation>Journal of Adhesion</dc:relation><dc:rights>info:eu-repo/semantics/openAccess</dc:rights><dc:type>info:eu-repo/semantics/article</dc:type><dc:identifier>https://ebyu-rdlopen.rawdatalibrary.net/tr/items/ebyu/14892</dc:identifier></oai_dc:dc></metadata></record></GetRecord></OAI-PMH>