...
首页> 外文期刊>Composite Structures >In-situ effect in cross-ply laminates under various loading conditions analyzed with hybrid macro/micro-scale computational models
【24h】

In-situ effect in cross-ply laminates under various loading conditions analyzed with hybrid macro/micro-scale computational models

机译:用混合宏/微级计算模型分析的各种装载条件下的交叉层层压板的原位效应

获取原文
获取原文并翻译 | 示例

摘要

In this work, mull-scale finite element analyses based on three-dimensional (3D) hybrid macro/micro-scale computational models subjected to various loading conditions are carried out to examine the in-situ effect imposed by the neighboring plies on the failure initiation and propagation of cross-ply laminates. A detailed comparative study on crack suppression mechanisms due to the effect of embedded laminar thickness and adjacent ply orientation is presented. Furthermore, we compare the results of in-situ transverse failure strain and strength between the computational models and analytical predictions. Good agreements are generally observed, indicating the constructed computational models are highly accurate to quantify the in-situ effect. Subsequently, empirical formulas for calculating the in-situ strengths as a function of embedded ply thickness and different ply angle between embedded and adjacent plies are developed, during which several material parameters are obtained using a reverse fitting method. Finally, a new set of failure criteria for sigma(22)-tau(12), sigma(22)-tau(23), and sigma(11)-tau(12) accounting for the in-situ strengths are proposed to predict laminated composites failure under multi-axial stress states. This study demonstrates an effective and efficient computational technique towards the accurate prediction of the failure behaviors and strengths of cross-ply laminates by including the in-situ effects.
机译:在这项工作中,基于经过各种负载条件的三维(3D)混合宏/微刻计算模型的Mull级有限元分析,以检查邻近PLIES对故障启动时施加的原位效应交叉层层压板的繁殖。介绍了由于嵌入层厚度和相邻帘布层取向引起的裂纹抑制机制的详细研究。此外,我们比较原位横向故障应变的结果和计算模型与分析预测之间的强度。通常观察到良好的协议,指示构造的计算模型高度准确以量化原位效应。随后,开发了用于计算原位强度作为嵌入和相邻层之间的嵌入帘布层厚度和不同帘布层的原位强度的经验公式,在此期间使用反向配合方法获得多种材料参数。最后,提出了一组新的失败标准(22)-Tau(12),Sigma(22)-Tau(23)和Sigma(11)-Tau(12)核对原位优势的核算多轴应力状态下的层压复合材料故障。本研究通过包括原位效应来朝着精确预测交叉层层压板的故障行为和强度的精确预测有效高效的计算技术。

著录项

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