2010
DOI: 10.1016/j.compstruct.2009.10.036
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An experimental investigation on the impact behavior of hybrid composite plates

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Cited by 133 publications
(62 citation statements)
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“…Since the impact face is loaded in compression and the other face is loaded in tension, the damage mechanisms can be different. Surprisingly, the conclusions of Jang et al [100] seem to contradict with the conclusions of Sayer et al [98] and Park and Jang [99]. This is most likely caused by differences in the damage mechanisms, which are triggered by differences in the materials and their interfaces.…”
Section: Positioningcontrasting
confidence: 54%
See 1 more Smart Citation
“…Since the impact face is loaded in compression and the other face is loaded in tension, the damage mechanisms can be different. Surprisingly, the conclusions of Jang et al [100] seem to contradict with the conclusions of Sayer et al [98] and Park and Jang [99]. This is most likely caused by differences in the damage mechanisms, which are triggered by differences in the materials and their interfaces.…”
Section: Positioningcontrasting
confidence: 54%
“…Sayer et al [98] made asymmetric interlayer hybrids of carbon and glass fibres. By this asymmetric layup, it becomes possible to test the glass side as well as the carbon side on the same layup.…”
Section: Positioningmentioning
confidence: 99%
“…In literature there are many works related to these composites [11][12][13][14][15][16] but very few regarding hybrid composite reinforced by natural fibers and carbon types. 17 One of the most recent applications of the latter is regarding the realization of an ecologic prototype boat named 'Araldite,' which represents the smallest offshore racing boat (hull length ¼ 6.5 m, hull width ¼ 3 m, weight ¼ 750 kg, sail surface ¼ 120 m 2 ), which can sail the Atlantic sea.…”
mentioning
confidence: 99%
“…Rajkumar et al (2012) studied the effect of repeated low-velocity impacts on glass fiber metal composites, and established that the peak load, impact energy, and failure strain decreased with increasing number of impacts. Sayer et al (2010) investigated the impact response of hybrid composite plates (glass-carbon/epoxy) with different stacking sequence for impact energies ranging from 25 to 75 J, and concluded that fiber fracture was the dominant failure mode as the impact energy increased. Murat and Rahman (2017) tested woven carbon/epoxy prepreg laminates at different impact energy levels in the range of 1-10 J, and observed that thicker samples manifested higher resistance to impact damage and the damage area increased with increasing impact energies.…”
Section: Introductionmentioning
confidence: 99%