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    <responseDate>2026-10-13T21:50:53Z</responseDate>
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            <header>
                <identifier>oai:data.mendeley.com/p4rc97wd7f.1</identifier>
                <datestamp>2023-12-27T06:58:24Z</datestamp>
            </header>
            <metadata><oai_dc:dc xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd" 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">
    <dc:creator>Wang, Congzhe</dc:creator>
    <dc:title>Two-dimentional Mode-II delamination experiments on glass-fiber composite laminates</dc:title>
    <dc:publisher>Mendeley Data</dc:publisher>
    <dc:description>The dataset shows the results for two-dimensional (2D) Mode-II delamination experiments on glass-fiber/epoxy composite laminates. The full experimental program contains a series of experiments with 9 different set-up/specimen combinations, nembered 1 - 9, exhibiting the whole development process of the experimental designs towards the final matrix (Set-up #9), which has been published in a journal paper [Wang C., Vassilopoulos AP, Keller T. Experimental investigation of two-dimensional Mode-II delamination in composite laminates. Composites Part A: Applied Science and Manufacturing. 2023, 173:107666]. These experiments included circular specimens, with the edge either simply supported by a ring or semi-clamped by two ring frames (allow free sliding of the specimen edge), then loaded transversely above the centrally embedded circular pre-crack to promote symmetric (circular) crack propagation. The description of each set-up can be found in the file &quot;2D_Experiments_description.xlsx&quot;. 
All 2D specimens failed in bending at the bottom center. During crack propagation, the loads in the 2D specimens continued to increase, showing certain pseudo-ductility. The results can be compared with standardized one-dimensional (1D) tests, e.g. End-loaded Split (ELS) tests, to reveal different fracture behavior under 2D conditions. The 2D cohesive relationships can be derived by numerical fitting of the data. </dc:description>
    <dc:subject>Fracture</dc:subject>
    <dc:subject>Composite Laminate</dc:subject>
    <dc:subject>Delamination</dc:subject>
    <dc:contributor>Vassilopoulos, Anastasios</dc:contributor>
    <dc:contributor>Keller, Thomas</dc:contributor>
    <dc:type>Dataset</dc:type>
    <dc:identifier>doi:10.17632/p4rc97wd7f.1</dc:identifier>
    <dc:identifier>oai:data.mendeley.com/p4rc97wd7f.1</dc:identifier>
    <dc:rights>Creative Commons Attribution 4.0 International</dc:rights>
    <dc:rights>http://creativecommons.org/licenses/by/4.0</dc:rights>
    <dc:relation>https://data.mendeley.com/datasets/p4rc97wd7f</dc:relation>
    <dc:date>2023-12-27T06:58:24Z</dc:date>
</oai_dc:dc></metadata>
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