首页> 外文期刊>Journal of Composite Materials >Mechanical analysis of three-dimensional braided composites by using realistic voxel-based model with local mesh refinement
【24h】

Mechanical analysis of three-dimensional braided composites by using realistic voxel-based model with local mesh refinement

机译:基于局部网眼细化的基于现实体素的模型用现实体素的模型进行三维编织复合材料的力学分析

获取原文
获取原文并翻译 | 示例
       

摘要

The elastic and failure analysis of three-dimensional braided composites is conducted by using realistic geometry model with local mesh refinement. The realistic geometry model is reconstructed by using micro computed tomography images. The voxel meshes are utilized to overcome the difficulties of mesh discretization for realistic geometry model of three-dimensional braided composites with complex meso-geometrical configurations. In order to improve the computational efficiency, the local voxel meshes at the braid yarn boundaries are refined to capture the detailed geometries of braid yarn and reduce the number of mesh. The stress averaging technique is applied to alleviate the local artificial stress spurious introduced from voxel meshes at braid yarn boundaries. Three kinds of computation models are used to predict the tensile properties of the braided composites, which are also compared with experimental results. The effects of braid yarn twist angle and mesh sizes on the predicted tensile behavior of the braided composites are studied further. A systematic way is provided to analyze mechanical properties of three-dimensional braided composites by using realistic voxel-based model.
机译:通过使用本地网格精制的现实几何模型进行三维编织复合材料的弹性和故障分析。通过使用微计算机断层扫描图像重建现实的几何模型。体素网格用于克服具有复杂的中间几何配置的三维编织复合材料的现实几何模型网眼离散化的难度。为了提高计算效率,在编织纱线边界处的局部体素网格被改进以捕获编织纱的详细几何形状并减少网格的数量。施加应力平均技术以缓解来自纹身纱线边界的塑料网引入的局部人造胁迫杂散。三种计算模型用于预测编织复合材料的拉伸性质,其也与实验结果进行比较。进一步研究了辫子纱线扭角和网状尺寸对编织复合材料的预测拉伸行为的影响。提供一种系统的方式来分析三维编织复合材料的机械性能通过使用基于实际的体素的模型来分析三维编织复合材料的机械性能。

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