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| Ertürk, Emre |
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| Azevedo, Nuno Monteiro |
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Rizal, Muhammad Asyraf Muhammad
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Publications (9/9 displayed)
- 2024Experimental investigation and analytical verification of buckling of functionally graded carbon nanotube-reinforced sandwich beams
- 2023Experimental and Analytical Investigation of Flexural Behavior of Carbon Nanotube Reinforced Textile Based Compositescitations
- 2023The Characteristics of Polymer Concrete Reinforced with Polypropylene Fibres Under Axial and Lateral Compression Loadscitations
- 2022Natural Fiber-Reinforced Polycaprolactone Green and Hybrid Biocomposites for Various Advanced Applicationscitations
- 2022Natural-Fiber-Reinforced Chitosan, Chitosan Blends and Their Nanocomposites for Various Advanced Applicationscitations
- 2021Micro- and Nanocellulose in Polymer Composite Materials: A Review.citations
- 2020Potential Application of Green Composites for Cross Arm Component in Transmission Tower: A Brief Reviewcitations
- 2019Sugar palm (Arenga pinnata [Wurmb.] Merr) starch films containing sugar palm nanofibrillated cellulose as reinforcement: Water barrier propertiescitations
- 2019Fundamentals of creep, testing methods and development of test rig for the full-scale crossarm: A reviewcitations
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document
Experimental investigation and analytical verification of buckling of functionally graded carbon nanotube-reinforced sandwich beams
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.