...
首页> 外文期刊>International journal of structural integrity >A numerical approach to determine fiber orientations around geometric discontinuities in designing against failure of GFRP laminates
【24h】

A numerical approach to determine fiber orientations around geometric discontinuities in designing against failure of GFRP laminates

机译:在设计中防止GFRP层压板失效的一种确定几何不连续性周围纤维取向的数值方法

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Purpose - Determining fiber orientations around geometric discontinuities is challenging and simultaneously crucial when designing laminates against failure. The purpose of this paper is to present an approach for selecting the fiber orientations in the vicinity of a geometric discontinuity; more specifically round holes with edge cracks. Maximum stresses in the discontinuity region are calculated using Classical Lamination Theory (CLT) and the stress concentration factor for the aforementioned condition. The minimum moment to cause failure in a lamina is estimated using the Tsai-Hill and Tsai-Wu failure theories for a symmetric general stacking laminate. Fiber orientations around the discontinuity are obtained using the Tsai-Hill failure theory. Design/methodology/approach - The current research focuses on a general stacking sequence laminate under three-point bending conditions. The laminate material is S2 fiber glass/epoxy. The concepts of mode I stress intensity factor and plastic zone radius are applied to decide the radius of the plastic zone, and stress concentration factor that multiplies the CLT stress distribution in the vicinity of the discontinuity. The magnitude of the minimum moment to cause failure in each ply is then estimated using the Tsai-Hill and Tsai-Wu failure theories, under the aforementioned stress concentration. Findings - The findings of the study are as follows: it confirms the conclusions of previous research that the size and shape of the discontinuity have a significant effect on determining such orientations; the dimensions of the laminate and laminae not only affect the CLT results, but also the effect of the discontinuity in these results; and each lamina depending on its position in the laminate will have a different minimum load to cause failure and consequently, a different fiber orientation around the geometric discontinuity. Originality/value - This paper discusses an important topic for the manufacturing and design against failure of Glass Fiber Reinforced Plastic (GFRP) laminated structures. The topic of introducing geometric discontinuities in unidirectional GFRP laminates is still a challenging one. This paper addresses these issues under 3pt bending conditions, a load condition rarely approached in literature. Therefore, it presents a fairly simple approach to strengthen geometric discontinuity regions without discontinuing fibers.
机译:目的-在设计抗破坏性层压板时,确定围绕几何不连续面的纤维取向是一项挑战,同时也至关重要。本文的目的是提出一种在几何不连续点附近选择纤维取向的方法。更具体地说,是带有边缘裂纹的圆形孔。使用经典层压理论(CLT)和上述条件下的应力集中系数计算不连续区域中的最大应力。使用Tsai-Hill和Tsai-Wu破坏理论对对称的一般堆叠层压板,估计导致层板破坏的最小力矩。使用Tsai-Hill破坏理论获得不连续点周围的纤维取向。设计/方法/方法-当前的研究重点是在三点弯曲条件下的一般堆叠顺序层压板。层压材料是S2玻璃纤维/环氧树脂。应用模式I应力强度因子和塑性区半径的概念来确定塑性区的半径,以及将不连续附近的CLT应力分布乘以CLT应力集中的应力集中系数。然后,在上述应力集中下,使用蔡-希尔(Tsai-Hill)和蔡-伍(Tsai-Wu)破坏理论,估计导致每个层板破坏的最小力矩的大小。研究结果-研究结果如下:它证实了先前研究的结论,即不连续性的大小和形状对确定这种取向有重大影响;层压板和薄片的尺寸不仅影响CLT结果,还影响这些结果中的不连续性;取决于其在层压材料中的位置,每个薄片将具有不同的最小载荷,从而导致破坏,因此,围绕几何不连续性产生的纤维取向也将有所不同。原创性/价值-本文讨论了针对玻璃纤维增​​强塑料(GFRP)层压结构的失效进行制造和设计的重要课题。在单向GFRP层压板中引入几何不连续性这一主题仍然是一个挑战。本文讨论了在3pt弯曲条件下的这些问题,这是文献中很少涉及的载荷条件。因此,它提出了一种相当简单的方法来在不中断纤维的情况下增强几何不连续区域。

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