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A hybrid damage assessment for E-and S-glass reinforced laminated composite structures under in-plane shear loading

Yilmaz, C.; Akalin, C.; Gunal, I.; Celik, H.; Buyuk, Murat; Suleman, A.; Yildiz, M.


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{
  "@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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