2015
DOI: 10.1007/s10921-015-0306-8
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Acoustic Emission Characterisation of Failure Modes in Hemp/Epoxy and Glass/Epoxy Composite Laminates

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Cited by 24 publications
(13 citation statements)
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“…22 Peak frequency analysis based on the principle that each failure mode generates an AE signal, which is related to the amount of strain energy released from the materials. Based on the peak frequency ranges, 23,24 the failure modes are classified as matrix cracking, fiber matrix interfacial debonding, delamination and fiber failure are 60-120 kHz, 130-180 kHz, 190-260 kHz and 270-320 kHz, respectively. In addition that the failure modes in the indented laminates are classified according to low energy with high frequency, low energy with medium frequency, medium energy with medium frequency and high energy with low frequency in AE signals are related to fiber failure, delamination, fiber matrix interfacial debonding and matrix cracking, respectively.…”
Section: Analysis Of Ae Activities During Indentationmentioning
confidence: 99%
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“…22 Peak frequency analysis based on the principle that each failure mode generates an AE signal, which is related to the amount of strain energy released from the materials. Based on the peak frequency ranges, 23,24 the failure modes are classified as matrix cracking, fiber matrix interfacial debonding, delamination and fiber failure are 60-120 kHz, 130-180 kHz, 190-260 kHz and 270-320 kHz, respectively. In addition that the failure modes in the indented laminates are classified according to low energy with high frequency, low energy with medium frequency, medium energy with medium frequency and high energy with low frequency in AE signals are related to fiber failure, delamination, fiber matrix interfacial debonding and matrix cracking, respectively.…”
Section: Analysis Of Ae Activities During Indentationmentioning
confidence: 99%
“…In addition that the failure modes in the indented laminates are classified according to low energy with high frequency, low energy with medium frequency, medium energy with medium frequency and high energy with low frequency in AE signals are related to fiber failure, delamination, fiber matrix interfacial debonding and matrix cracking, respectively. 24 However, the frequency ranges of fiber matrix interfacial debonding and delamination are somehow overlapping. 25 The percentage of AE hits related to dominant failure modes during 0 and 20 indentation loading in UD and CP laminates for the displacement of 2 mm and 3 mm are shown in Figure 10.…”
Section: Analysis Of Ae Activities During Indentationmentioning
confidence: 99%
“…At below 40% of load, some of the specimens have no hits occurring in them and at above 70% of load, input parameters are increasing and varying drastically to a very high value. This may be attributed to echo of failure on the specimen at the time of increasing damage in it at higher loads [11,12,32]. So input parameters used for training are considered from 40% to 70% load for least error.…”
Section: Selection Of Range Of Input Parameters For Trainingmentioning
confidence: 99%
“…Time-scale methods or signal-based approach is used to determine new relevant descriptors to be introduced in the classification process to improve the characterization and the discrimination of the failure modes. 13,15 Pashmforoush et al 16 used Davies-Bouldin (DB) index and harmony search k-means algorithms for discrimination of AE signals where the highest frequency contents were represented as fiber breakage, while signals with the lowest frequency contents were related to matrix cracking. The frequency range of debonding was between matrix cracking and fiber breakage.…”
Section: Introductionmentioning
confidence: 99%