2020
DOI: 10.1016/j.mtcomm.2020.101106
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Effects of carbon nanotubes on open-hole carbon fiber reinforced polymer composites

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Cited by 21 publications
(12 citation statements)
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“…The carbon fabric reinforced MWCNT/epoxy structural composites were developed by hand lay-up technique. [22] Eight layers of CF/Epoxy-MWCNT composites were prepared by brushing the affixed mass of Epoxy/MWCNT/curative at each fiber layer until the 8th layer. Finally, the whole setup was compression molded in a hydraulic press at room temperature for 48 h. Figure 1 shows the schematic of the flow chart for the preparation of CNT reinforced polymer matrix nanocomposite (PMNC) and laminated composite.…”
Section: Materials Details and Sample Preparationsmentioning
confidence: 99%
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“…The carbon fabric reinforced MWCNT/epoxy structural composites were developed by hand lay-up technique. [22] Eight layers of CF/Epoxy-MWCNT composites were prepared by brushing the affixed mass of Epoxy/MWCNT/curative at each fiber layer until the 8th layer. Finally, the whole setup was compression molded in a hydraulic press at room temperature for 48 h. Figure 1 shows the schematic of the flow chart for the preparation of CNT reinforced polymer matrix nanocomposite (PMNC) and laminated composite.…”
Section: Materials Details and Sample Preparationsmentioning
confidence: 99%
“…[21,22] The addition of MWCNT reinforcement improved the fracture toughness and retarded the damage propagation of composites by increasing their tensile load-carrying capability. [22] The failure of laminates was mainly due to fiber tensile damage (DAMAEFT and HSNFTCRT), matrix tensile damage (HSNMTCRT), and compressive matrix damage (HSNMCCRT). Further, the different damage contours at 17 kN loading (point C) for different wt% MWCNT laminates are also shown in toughness of laminated composites) was more in the case of 0.5% and 1.0% CNT loaded OHT samples compared with that of CF/neat epoxy.…”
Section: Damage Propagation and Failuresmentioning
confidence: 99%
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“…The AE signals of specimen A during flexural tests take place according to four kinds: low-frequency and low-amplitude, medium-frequency and high-amplitude, medium-frequency and lowamplitude and finally high-frequency, corresponding to matrix bucking, interfacial debonding, delamination and fiber breakage respectively. [43] However, the clustering of specimen B is divided into three categories, and there is no debonding phenomenon compared A. The reason may be that the adhesion between KF and the matrix is lower than that of GF, which directly leads to delamination damage.…”
Section: Gray Relational Analysis and K-means Clusteringmentioning
confidence: 99%
“…The results indicate that the properties of open-hole carbon fiber-reinforced composite laminate specimens can be enhanced by adding appropriate CNTs. 33 Due to the enhancement of interfacial resistance and the effective stress transfer between CNTs and matrix, the addition of CNTs to matrix can enhance the failure load. 26,27,30 Each curve can absolutely describe the damage evolution process under tensile load.…”
Section: Characterization Of Mechanical Propertiesmentioning
confidence: 99%