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| 3. |
- Bravo, L, et al.
(författare)
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- 2021
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swepub:Mat__t
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| 4. |
- Tabiri, S, et al.
(författare)
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- 2021
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swepub:Mat__t
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| 5. |
- Glasbey, JC, et al.
(författare)
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- 2021
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swepub:Mat__t
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| 8. |
- Hakeem, Ibrahim Y, et al.
(författare)
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Nonlocal theoretical inquiry into pultruded GFRP plate dynamics: Integrating experimental and numerical analyses
- 2024
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Ingår i: Journal of Engineered Fibers and Fabrics. - : Sage. - 1558-9250. ; 19, s. 1-21
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Tidskriftsartikel (refereegranskat)abstract
- Few studies combining experimental and theoretical analyses of pultruded fiber-reinforced polymer (FRP) composites are available in the literature. In this study, experimental methods and a nonlocal theoretical approach were used to investigate the flexural performance of pultruded glass-FRP (GFRP) plates. In the theoretical method used, the Eringen’s nonlocal elasticity theory was adopted so that small-scale material effects on pultruded FRP composite plates were taken into account. Based on the plate theory of high-order shear deformation, the kinematic relationships of the composite plates were established. The stiffness matrix coefficients and tangential stiffness matrix were shown along with the nonlocal force vector. Also, finite element modeling was performed with the help of ABAQUS for the accuracy of experimental and theoretical results. For the analysis, a variety of laminated plate types were taken into consideration. The flexural performance was investigated utilizing flexural tests under point and distributed loads. To comprehend the behavior of the pultruded GFRP plates more fully, macro mechanical damage analyses were carried out. Numerical values were compared with experimental findings, theoretical solution results, and finite element simulation results which were found to be very similar.
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| 9. |
- Madenci, Emrah, et al.
(författare)
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Behavior of functionally graded carbon nanotube reinforced composite sandwich beams with pultruded GFRP core under bending effect
- 2024
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Ingår i: Frontiers in Materials. - : Frontiers. - 2296-8016. ; 10
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Tidskriftsartikel (refereegranskat)abstract
- A novel generation of composite sandwich beams with laminated carbon fiber-reinforced polymer skins and pultruded glass fiber-reinforced polymer core materials was examined for their flexural behavior. The strength and failure mechanisms of the composite sandwich beams in flatwise and edgewise configurations were investigated using three-point static bending tests. These sophisticated composite structures must be designed and used in a variety of sectors, and our research provides vital insights into their performance and failure patterns. In comparison to the reference specimens (FGM-1), the carbon nanotube-reinforced specimens’ bending capacity was affected and ranged from −2.5% to 7.75%. The amount of the carbon nanotube addition had a substantial impact on the beams’ application level and load-carrying capacity. Particularly, the application of 0.5 wt% additive in the outermost fiber region of the beams, such as in FGM-4, led to an increase in the bending capacity. However, the stiffness values at the maximum load were decreased by 0.3%–18.6% compared to FGM-1, with the minimum level of the decrease in FGM-4. The experimental results were compared with the theoretical calculations based on the high-order shear deformation theory, which yielded an approximation between 11.99% and 12.98% by applying the Navier’s solution.
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| 10. |
- Madenci, Emrah, et al.
(författare)
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Experimental investigation and analytical verification of buckling of functionally graded carbon nanotube-reinforced sandwich beams
- 2024
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Ingår i: Heliyon. - : Elsevier. - 2405-8440. ; 10:8
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Tidskriftsartikel (refereegranskat)abstract
- Carbon nanotube (CNT) reinforcement can lead to a new way to enhance the properties of composites by transforming the reinforcement phases into nanoscale fillers. In this study, the buckling response of functionally graded CNT-reinforced composite (FG-CNTRC) sandwich beams was investigated experimentally and analytically. The top and bottom plates of the sandwich beams were composed of carbon fiber laminated composite layers and hard core. The hard core was made of a pultruded glass fiber-reinforced polymer (GFRP) profile. The layers of FG-CNTRC surfaces were reinforced with different proportions of CNT. The reference sample was made of only a pultruded GFRP profile. In the study, the reference sample and four samples with CNT were tested under compression. The largest buckling load difference between the reference sample and the sample with CNT was 37.7%. The difference between the analytical calculation results and experimental results was obtained with an approximation of 0.49%–4.92%. Finally, the buckling, debonding, interlaminar cracks, and fiber breakage were observed in the samples.
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