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INTERACTION BETWEEN TRANSVERSE CRACKS AND EDGE DELAMINATION CONSIDERING FREE-EDGE EFFECTS IN COMPOSITE LAMINATES

机译:考虑复合层压板中的自由边缘效应的横裂和边缘分层之间的相互作用

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The high-cycle fatigue characteristics, especially the initiation and propagation of edge delamination, were investigated with quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates with a stacking sequence of [45/0/-45/90]S. To investigate the influence that transverse cracks have on the initiation and propagation of edge delamination, two types of specimens are used. One was a specimen where transverse cracks were arbitrarily introduced by static tensile loading before conducting the fatigue tests. The other was an undamaged specimen as new. As a result, it was found that the single transverse crack introduced before the fatigue test did not seriously affect the initiation of edge delamination. Moreover, the difference of the fatigue damage growth behavior depending on the applied stress level was observed. Under the test conditions of low-applied stress level and high-cyclic loadings, it was observed that the edge delamination grew before, or simultaneously with, the transverse crack propagation.
机译:用Quasi-各向同性碳纤维增强塑料(CFRP)层压板研究了[45/0 / -45 / 90] s的堆叠序列,研究了高循环疲劳特性,尤其是边缘分层的起始和传播。为了研究横裂横向裂缝对边缘分层的开始和传播的影响,使用两种样品。一种是通过静态拉伸在进行疲劳试验之前任意引入横裂裂缝的标本。另一个是一个未造成的标本作为新的。结果发现,在疲劳试验之前引入的单横裂缝并未严重影响边缘分层的启动。此外,观察到取决于所施加的应力水平的疲劳损伤生长行为的差异。在低施加的应力水平和高循环载荷的测试条件下,观察到边缘分层以前或同时增长,横裂裂缝繁殖。

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