2000
DOI: 10.1016/s0734-743x(00)00021-x
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Impact perforation resistance of laminated and assembled composite plates

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Cited by 69 publications
(48 citation statements)
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“…1a,c). The sudden reductions of force after the achievement of the maximum value of force have been also observed by other authors [16,21,22]. They concluding that such variations of the force values rather indicate to more extensive and advanced material damage, finally reducing the rigidity and strength of the material.…”
Section: Fig 1 Force -Time (Ac) and Force -Deflection (Bd) Curvessupporting
confidence: 67%
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“…1a,c). The sudden reductions of force after the achievement of the maximum value of force have been also observed by other authors [16,21,22]. They concluding that such variations of the force values rather indicate to more extensive and advanced material damage, finally reducing the rigidity and strength of the material.…”
Section: Fig 1 Force -Time (Ac) and Force -Deflection (Bd) Curvessupporting
confidence: 67%
“…The first stage of the force value variations is responsible for the system stabilization. The force fluctuations in this stage represent the vibration of the material -impactor system [16]. The force fluctuations observed in the next force increase stage are insignificant and mainly associated with local degradation of composite structure [16].…”
Section: Resultsmentioning
confidence: 97%
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“…The correlation between impact energy and absorbed energy can be found using Energy profile method (EPM) (Liua et al [22]). Energy profile variations are seen in Fig.…”
Section: Energy Profile Methodsmentioning
confidence: 99%
“…Mines et al (1999) studied the high velocity perforation behaviour of polymer composite laminates with impact perforation velocities ranging up to 571 m/s. In 2000, Liu et al (2000) studied the impact perforation resistance of laminated and assembled composite plates made of glass fibers and an epoxy matrix, investigated the joining stiffness and perforation threshold of a composite plate assembled using various joining techniques, identified an efficient way to assemble thin composite laminates to achieve a high perforation threshold, and explored the feasibility of replacing costly thick laminated composite plates with assembled composite plates. Vaidya et al (2000) described an innovative integrated hollow (space) E-glass/epoxy core sandwich composite construction that has several multi-functional benefits and advantages in terms of weight and bending stiffness.…”
Section: Introductionmentioning
confidence: 99%