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            <header>
                <identifier>oai:data.mendeley.com/svhmy6p9t2.1</identifier>
                <datestamp>2020-09-10T18:23:50Z</datestamp>
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            <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>Goossens, Sidney</dc:creator>
    <dc:title>Processed data for: A global assessment of barely visible impact damage for CFRP sub-components with FBG-based sensors</dc:title>
    <dc:publisher>Mendeley Data</dc:publisher>
    <dc:description>Processed data for &quot;A global assessment of barely visible impact damage for CFRP sub-components with FBG-based sensors&quot;.

Barely visible impact damage (BVID) on carbon fibre reinforced polymer (CFRP) aerospace components can create interlaminar defects that may deteriorate during operation with potential failure as a result. Especially damage-prone regions such as the feet of a stiffener must therefore be inspected for BVIDs frequently, which is an effort that increases downtimes and operational costs. The potential of optical fibre sensors as part of a permanently installed structural health monitoring network is well-known. Individual FBG-based strain sensors have shown their capability to detect BVIDs. In this work we introduce a global damage index (GDI) as a figure of merit for the combined response of 60 FBG sensors mounted on several aerospace-grade CFRP flat stiffened panels. We first obtain a detection threshold for the GDI and then demonstrate its use for BVID detection. The proposed methodology is the first of its kind for the representation of the health of a component in a single parameter.

The data set includes the damage indicators as calculated from the spectra, and global damage indices (GDI) as calculated from the damage indicators for every impact.</dc:description>
    <dc:subject>Non-Destructive Testing</dc:subject>
    <dc:subject>Composite Defect</dc:subject>
    <dc:subject>Fiber Bragg Grating</dc:subject>
    <dc:subject>Aerospace Material</dc:subject>
    <dc:subject>Optical Fiber Sensing</dc:subject>
    <dc:subject>Structural Health Monitoring</dc:subject>
    <dc:contributor>Berghmans, Francis</dc:contributor>
    <dc:contributor>Muñoz, Kirsa</dc:contributor>
    <dc:contributor>Jiménez, Miguel</dc:contributor>
    <dc:contributor>Karachalios, Evangelos</dc:contributor>
    <dc:contributor>Saenz-Castillo, Diego</dc:contributor>
    <dc:contributor>Geernaert, Thomas</dc:contributor>
    <dc:type>Dataset</dc:type>
    <dc:identifier>doi:10.17632/svhmy6p9t2.1</dc:identifier>
    <dc:identifier>oai:data.mendeley.com/svhmy6p9t2.1</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/svhmy6p9t2</dc:relation>
    <dc:date>2020-09-10T18:23:50Z</dc:date>
</oai_dc:dc></metadata>
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