2020
DOI: 10.1016/j.ijmecsci.2020.105783
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Damage accumulation mechanism of composite laminates subjected to repeated low velocity impacts

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Cited by 68 publications
(29 citation statements)
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“…The increase of F Max in the repeated impact was also found in Ref. 31,29 . It was unexpected since the delamination damage created by the first impact would reduce the stiffness of composites, which should result in a decrease rather than an increase in the peak force during the multiple impacts under the same impact energy level.…”
Section: Impact Force-time Responsesupporting
confidence: 78%
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“…The increase of F Max in the repeated impact was also found in Ref. 31,29 . It was unexpected since the delamination damage created by the first impact would reduce the stiffness of composites, which should result in a decrease rather than an increase in the peak force during the multiple impacts under the same impact energy level.…”
Section: Impact Force-time Responsesupporting
confidence: 78%
“…Based on the test results, they concluded that the cross-ply and non-symmetric laminates had a better endurance against low impact events than unidirectional laminates because of multidirectional reinforcement. Liao et al 29 considered the effect of impactor diameter on the damage accumulation of CFRP laminates under repeated impacts, and proposed a damage index to distinguish the occurrence of penetration. In the paper, 30 the symmetric laminate with dissimilar interfaces was proved to have the great endurance against repeated impact.…”
Section: Introductionmentioning
confidence: 99%
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“…Several works regarding this behaviour are available in the literature. 6,15,29 The studies conducted by Wyrick and Adams 30 on a carbon/epoxy laminate suggest the first explanation of this phenomenon. They attributed the initial increase in peak force to the thin layer of unreinforced matrix on the impacted surface.…”
Section: Resultsmentioning
confidence: 96%
“…Several studies regarding the effects of repeated impacts on the mechanical properties of composite structures can be found in the literature. 3,4,5 Among these studies, Liao et al 6 investigated the mechanical response of carbon fibre reinforced laminates subjected to repeated low-velocity impacts at an energy of 15 J, and varying the diameter of the impactor. Moreover, a new damage index (DI-B), based on the reduction of bending stiffness and expressed by the ratio between the maximum displacement recorded during the repeated impact tests and the maximum displacement as the penetration happens, allowed to evaluate the bending stiffness reduction rate, to characterise the damage accumulation and to distinguish the occurrence of penetration simultaneously.…”
Section: Introductionmentioning
confidence: 99%