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    Direct comparison of low velocity impact performance of nanoclay, boric acid and interlayer hybrid composites
    (Wiley, 2024) Örçen, Gurbet; Ünal, Hasan Yavuz; Pekbey, Yeliz
    In this study, the low velocity impact effect of glass fiber-reinforced laminated composites reinforced with nanoclay and boric acid was investigated. Nanoclay, boric acid, and interlayer hybrid composites were produced at 0 (pure), 0.5, 1, and 1.5 wt% with respect to epoxy resin. Laminated composites were obtained by the hand lay-up method. Impact tests were applied to the specimens by releasing the weight. Tests were carried out with impact energies of 30, 40, 50, and 60 J to evaluate the behavior of composites under loading result in rebounding. Nano reinforcement generally increases the maximum reaction force while decreasing the impact duration, maximum displacement, and absorbed energy. As a result of all the tests performed, the reaction force increased up to 53% compared to the pure specimen, while the absorbed energy, impact duration, and maximum displacement values decreased up to 21%, 36%, and 12%, respectively. The results of the hybrid specimens in the interlayer sequence provided more changes compared to the mono-reinforced specimens (i.e., nanoclay or boric acid). The hybrid specimen with a reinforcement ratio of 1.5 wt% impact face boric acid exhibited the greatest enhancement in impact resistance among all the tested specimens. The reaction force, which is an indicator of resistance, increased by 44%, 35%, 51% and 34% from energy level 30 to 60 J, respectively. Furthermore, the specimen exhibited the lowest values for absorbed energy, maximum displacement and impact duration.
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    Öğe
    Progressive Failure Analysis of Reinforced-Adhesively Single-Lap Joint
    (Taylor & Francis Ltd, 2015) Turan, Kadir; Pekbey, Yeliz
    The failure behavior of reinforced-adhesively single-lap joints was investigated experimentally and numerically. The reinforced adhesive was produced by mixing waste composite particles and an epoxy-based commercial adhesive. The single-lap joint was prepared with an adhesive and unidirectional fiber glass/epoxy composite plates with a (0 degrees/90 degrees)(3) stacking sequence. Three types of adhesive were used: an un-reinforced adhesive (ADH), an adhesive mixed with glass fiber-reinforced epoxy resin composite plate particles (GFRC), and an adhesive mixed with carbon fiber-reinforced epoxy resin composite plate particles (CFRC). The adhesive thickness (ta) and overlap length (lap) were 0.4, 0.8, 1.2, and 1.6 mm and 10, 20, 30, and 40 mm, respectively. Progressive failure analysis was performed with the ANSYS (TM) 11.0 finite element program using ANSYS (TM) parametric design language (APDL) code. In the numerical study, the failure loads of the composite and the adhesive were determined with the Hashin failure criteria and the Tresca failure criteria, respectively. The difference between the experimental and numerical studies ranged from 2% to 10%. The failure load of reinforced-adhesively single-lap joints was 1.3-22.8% higher than that of the un-reinforced adhesive.