Dergi makalesi Açık Erişim
Yilmaz, C.; Akalin, C.; Gunal, I.; Celik, H.; Buyuk, Murat; Suleman, A.; Yildiz, M.
{ "@context": "https://schema.org/", "@id": 110510, "@type": "ScholarlyArticle", "creator": [ { "@type": "Person", "name": "Yilmaz, C." }, { "@type": "Person", "name": "Akalin, C." }, { "@type": "Person", "affiliation": "KNRTU KAI, Struct Strength Dept, Kazan, Russia", "name": "Gunal, I." }, { "@type": "Person", "affiliation": "Yonca Onuk JV Shipyard, Istanbul, Turkey", "name": "Celik, H." }, { "@type": "Person", "name": "Buyuk, Murat" }, { "@type": "Person", "affiliation": "Univ Victoria, Dept Mech Engn, Ctr Aerosp Res, Victoria, BC V8W 3P6, Canada", "name": "Suleman, A." }, { "@type": "Person", "name": "Yildiz, M." } ], "datePublished": "2018-01-01", "description": "Micro-damage initiation and accumulation in two different Glass Fiber Reinforced -E-glass and S-glass-Laminated Composite Structures (LCS) subjected to in-plane shear stressing are monitored with Acoustic Emission (AE) and thermography methods. AE signals caused by micro-damage formation are graphed as a scatter plot of Weighted Peak Frequency (WPF) versus Partial Power 2 (PP2) features and clustered using the K-means algorithm with Bray Curtis dissimilarity function thus resulting in three different well-separated clusters. Each of these clusters corresponds to different micro damages, i.e., transverse cracks, delaminations, or fiber ruptures. It is observed that the E-glass reinforced LCS has higher numbers of AE hits. Thus, the total amount of micro-damage incurred as well as the average temperature change measured by thermography is higher for the E-glass reinforced LCS. It is shown that due to the curing induced residual tensile stress in E-glass reinforced LCS, the initial formation of delamination in E-glass reinforced LCS starts at higher load level. Under the applied shear load, a significant reduction in in-plane shear modulus is observed both for the E-glass and S-glass-reinforced LCS where the E-glass reinforced LCS shows greater reduction. The decrease in in-plane shear modulus is attributed to micro-damage accumulated in the LCS.", "headline": "A hybrid damage assessment for E-and S-glass reinforced laminated composite structures under in-plane shear loading", "identifier": 110510, "image": "https://aperta.ulakbim.gov.tr/static/img/logo/aperta_logo_with_icon.svg", "license": "http://www.opendefinition.org/licenses/cc-by", "name": "A hybrid damage assessment for E-and S-glass reinforced laminated composite structures under in-plane shear loading", "url": "https://aperta.ulakbim.gov.tr/record/110510" }
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