1988
DOI: 10.1016/0010-4361(88)90540-x
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Damage sustained by a carbon/ epoxy composite material subjected to repeated impact

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Cited by 34 publications
(20 citation statements)
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“…4a, which represents the contact force history of the 1st impact, has two peaks. As reported by many studies previously (e.g., Wyrick and Adams [6,25], and Liu and Liaw [24]), the sudden drop in contact force right after the first peak, which was around 7 kN in this curve, indicates the occurrence of damage (in the forms of delamination and/or cracking, which are shown as the circular-and cross-shaped damages in Fig. 3, respectively).…”
Section: Resultsmentioning
confidence: 62%
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“…4a, which represents the contact force history of the 1st impact, has two peaks. As reported by many studies previously (e.g., Wyrick and Adams [6,25], and Liu and Liaw [24]), the sudden drop in contact force right after the first peak, which was around 7 kN in this curve, indicates the occurrence of damage (in the forms of delamination and/or cracking, which are shown as the circular-and cross-shaped damages in Fig. 3, respectively).…”
Section: Resultsmentioning
confidence: 62%
“…4a-c, the peak force sustained by the composite increased initially until the maximum peak force was reached. This phenomenon has been reported by other researchers as well [6,7,17,24] can be exemplified by two reasons. First, Wyrick and Adams [6,25] suggested the initial increase in the peak force resulting from the compaction process of the thin layer of unreinforced resin at the impacted surface.…”
Section: Resultsmentioning
confidence: 68%
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“…However, under repeated impacts the laminates experienced a large deterioration in flexural strength because of fracture of the glass fibres [17]. Wyrick and Adams [18] observed that damage in the carbon/epoxy laminates increased with increasing number of impacts of the same energy. The main damage occurs during the first impact and, after, each impact promotes little incremental damages [18].…”
Section: Introductionmentioning
confidence: 99%
“…Wyrick and Adams [18] observed that damage in the carbon/epoxy laminates increased with increasing number of impacts of the same energy. The main damage occurs during the first impact and, after, each impact promotes little incremental damages [18]. On the other hand, Ho et al [19] shows that the fibre pullout and fibre breakage are the major fracture mechanisms in repeated impacts for polycarbonate composites.…”
Section: Introductionmentioning
confidence: 99%