首页> 外文期刊>Composite Structures >Effect of distance between impact point and hole position on the impact fatigue strength of composite laminates
【24h】

Effect of distance between impact point and hole position on the impact fatigue strength of composite laminates

机译:冲击点与孔位置的距离对复合材料层板冲击疲劳强度的影响

获取原文
获取原文并翻译 | 示例
           

摘要

An impact fatigue study was performed to evaluate the effect of the distance between the impact point and the hole on the fatigue life of glass fibre/epoxy laminates. For this purpose, experimental tests were carried out in square plates and for the distances of 0, 5, 10 and 20 mm, from the impact point. The results were compared with the ones obtained in plates without hole. It was possible to conclude that the fatigue life decreased, comparatively to the control samples, about 10.9%, 40%, 63.6% and 69.1% for the distances of 20 mm, 10 mm, 5 mm and 0 mm, respectively. Higher distances promote higher maximum loads and elastic restitution, but an opposite trend in terms of maximum displacement. For example, it was found for 20 mm a maximum load around 5.54 kN, a displacement of about 4.4 mm and an elastic energy of 59.2%, while for 0 mm these values were about 4.59 kN, 5.7 mm and 40.4%, respectively. In terms of multi-impacts, the damage severity is also very influenced by the distance. For small distances the damage progresses quickly, while three stages can be found for the control samples and for the distance of 20 mm. (C) 2017 Elsevier Ltd. All rights reserved.
机译:进行了冲击疲劳研究,以评估冲击点和孔之间的距离对玻璃纤维/环氧树脂层压板疲劳寿命的影响。为此,在方板中进行实验测试,并且距撞击点的距离为0、5、10和20 mm。将结果与在没有孔的板上获得的结果进行比较。可以得出的结论是,相对于对照样品,距离20 mm,10 mm,5 mm和0 mm的疲劳寿命分别降低了约10.9%,40%,63.6%和69.1%。距离越远,最大载荷和弹性恢复越高,但是在最大位移方面却相反。例如,对于20毫米,发现最大载荷约为5.54 kN,位移约为4.4毫米,弹性能为59.2%,而对于0毫米,这些值分别约为4.59 kN,5.7毫米和40.4%。就多重影响而言,损坏的严重程度也受距离的影响很大。对于较小的距离,损坏会迅速发展,而对于对照样品和20 mm的距离,可以发现三个阶段。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号