2018
DOI: 10.1016/j.compositesa.2018.04.015
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Thickness effects on fibre-bridged fatigue delamination growth in composites

Abstract: This paper provides an investigation on thickness effects on fibre-bridged fatigue delamination growth (FDG) in composite laminates. A modified Paris relation was employed to interpret experimental fatigue data. The results clearly demonstrated that both thickness and fibre bridging had negligible effects on FDG behaviors. Both energy principles and fractography analysis were subsequently performed to explore the physical reasons of this independence. It was found that the amount of energy release of a given c… Show more

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Cited by 18 publications
(16 citation statements)
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“…(2), has been proposed in a recent study [26]. There is evidence that the application of this new power law relation can result in appropriately interpreting fibre-bridged fatigue delamination behaviors in composite laminates and significantly benefiting one's in-depth understanding on this phenomenon [26,29].…”
Section: Fatigue Delamination Modelsmentioning
confidence: 99%
See 2 more Smart Citations
“…(2), has been proposed in a recent study [26]. There is evidence that the application of this new power law relation can result in appropriately interpreting fibre-bridged fatigue delamination behaviors in composite laminates and significantly benefiting one's in-depth understanding on this phenomenon [26,29].…”
Section: Fatigue Delamination Modelsmentioning
confidence: 99%
“…According to our previous experimental experience in this field [25,26,29], a special test procedure was programed to determine fatigue delamination with different amounts of fibre bridging. DCB specimens were repeatedly tested for several times with different pre-crack lengths, but keeping R-ratio the same.…”
Section: (B)mentioning
confidence: 99%
See 1 more Smart Citation
“…Here one should note that recently Yao et al [23] demonstrated specimen thickness has no significant effect on the zero-bridging curve. This may seem counter intuitive considering the thickness effects reported for quasi-static loading [12] [31].…”
Section: Limiting Conditions To the Proposed Proceduresmentioning
confidence: 99%
“…Upon manufacturing the laminates for the specimens one has to determine the appropriate thickness, because the thickness has been observed to influence the experimental results [23]. An approximately 12-13 µm thin Teflon or FEP foil should be applied to create the starter crack.…”
Section: Pre-crackingmentioning
confidence: 99%