2022
DOI: 10.1016/j.mechmat.2021.104113
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Failure sequence determination in sandwich structures using concurrent acoustic emission monitoring and postmortem thermography

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Cited by 10 publications
(15 citation statements)
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“…7 and the energy release of related AE hits using load-energy vs. displacement and load-cumulative energy vs. displacement curves, damage types were classified and presented in Table 2, from a lower frequency to a higher frequency as fiber breakage, matrix cracking, face sheet-core debonding, and core damage. Generally, fiber breakage in face sheets of sandwich composites and laminated composites corresponds to AE data having high-frequency values in the literature [14,15,17,19,23]; whereas, some other studies claim the opposite [24,25]. While several factors might affect the difference between the frequency outputs of the studies, specimen type (such as laminated composites and sandwich composites) and testing (i.e.…”
Section: Resultsmentioning
confidence: 95%
See 1 more Smart Citation
“…7 and the energy release of related AE hits using load-energy vs. displacement and load-cumulative energy vs. displacement curves, damage types were classified and presented in Table 2, from a lower frequency to a higher frequency as fiber breakage, matrix cracking, face sheet-core debonding, and core damage. Generally, fiber breakage in face sheets of sandwich composites and laminated composites corresponds to AE data having high-frequency values in the literature [14,15,17,19,23]; whereas, some other studies claim the opposite [24,25]. While several factors might affect the difference between the frequency outputs of the studies, specimen type (such as laminated composites and sandwich composites) and testing (i.e.…”
Section: Resultsmentioning
confidence: 95%
“…6.c) graphs were plotted for each test specimen. Following that, k-means genetic algorithm was employed to increase the effectiveness and the reliability of the damage classification, creating four clusters analogous to previous studies conducted on sandwich composites [14,17,19,23,24]. Each of these four clusters specifies a damage type which are core damage, core-face sheet debonding, matrix cracking, and fiber breakage.…”
Section: Resultsmentioning
confidence: 99%
“…The delamination failure load is first determined based on the experimental data. Previous studies on different composite specimens under tensile loading [38][39][40] and flexural loading [46][47][48] revealed that acoustic emission data provided important evidences for determining various failure modes including delamination failure. The results of these studies showed that geometry, material, layup sequence, and sensor types affected the values of AE parameters of the failure modes but a significant conclusion was that a largescale delamination between plies caused significant load drops in load-displacement curves and also initiation of new AE clusters or groups or a stop in the recording of AE clusters or groups.…”
Section: Methodsmentioning
confidence: 99%
“…42 Characteristic parameters of peak frequency, amplitude and relative energy are used to characterize failure behavior of composite. [43][44][45] In the case of composite repair, AE technology also has important applications in the estimation of repair quality. 39,46 Shruthi et al 46 investigated damage mechanism and evolution process of laminates repaired by different hybrid patches under indentation load by using AE technology.…”
Section: Introductionmentioning
confidence: 99%
“…Among them, AE technology analyzes the damage mechanism by detecting transient elastic waves generated by internal damage in the material 42 . Characteristic parameters of peak frequency, amplitude and relative energy are used to characterize failure behavior of composite 43–45 . In the case of composite repair, AE technology also has important applications in the estimation of repair quality 39,46 .…”
Section: Introductionmentioning
confidence: 99%