2019
DOI: 10.1016/j.engfracmech.2019.106511
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Investigation and identification of damage mechanisms of unidirectional carbon/flax hybrid composites using acoustic emission

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Cited by 56 publications
(25 citation statements)
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“…Finally, the delamination, the fiber pull-out and the fiber breakage occurred near 40% of tensile loading at the failure. Such an investigation 45 under cyclic loadings indicated that matrix cracking had the greatest activity and fiber-matrix debonding had less activity. The delamination appeared from the first stage of fatigue tests and it was less than those of matrix cracking and fiber-matrix debonding.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…Finally, the delamination, the fiber pull-out and the fiber breakage occurred near 40% of tensile loading at the failure. Such an investigation 45 under cyclic loadings indicated that matrix cracking had the greatest activity and fiber-matrix debonding had less activity. The delamination appeared from the first stage of fatigue tests and it was less than those of matrix cracking and fiber-matrix debonding.…”
Section: Resultsmentioning
confidence: 99%
“…Therefore, peaks occurred later with a higher amount. 45 Consequently, the cumulative energy could predict effective fatigue failures in composites, considering typical thresholds.…”
Section: Resultsmentioning
confidence: 99%
“…AE signals contain some features representative of the source in such a manner that direct correlation exists between the damage mechanisms and the AE parameters. Therefore, acoustic emission events can be classified using multivariable statistical analysis techniques and then attributed to a damage mechanism in the material [29][30][31]. In the present study, the AE monitoring was performed by using an acquisition system PCI-2 of Mistras Group Corporation.…”
Section: Acoustic Emissionmentioning
confidence: 99%
“…AE is defined as the generation and propagation of a transient elastic wave caused by a sudden release of strain energy which can be due to damage occurrence in the material [32][33][34]. The literature review revealed that this technique has been mainly used to consider the damage behavior of composite laminates under quasi-static loading [32,[35][36][37] while in just limited studies it has been used for the fatigue loading conditions [21,[38][39][40]. In the present study, Scanning Electron Microscope (SEM) images and AE technique have been used to investigate the effect of mode II fatigue crack growth rate, da/ dN, on the fatigue micro-damage features, i.e.…”
Section: Introductionmentioning
confidence: 99%