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基于能量法的三维四向编织复合材料细观建模

巩龙东 申秀丽

巩龙东, 申秀丽. 基于能量法的三维四向编织复合材料细观建模[J]. 航空动力学报, 2015, 30(1): 106-113. doi: 10.13224/j.cnki.jasp.2015.01.015
引用本文: 巩龙东, 申秀丽. 基于能量法的三维四向编织复合材料细观建模[J]. 航空动力学报, 2015, 30(1): 106-113. doi: 10.13224/j.cnki.jasp.2015.01.015
GONG Long-dong, SHEN Xiu-li. Mesoscopic modeling of three-dimensional four-directional braided composites using energy method[J]. Journal of Aerospace Power, 2015, 30(1): 106-113. doi: 10.13224/j.cnki.jasp.2015.01.015
Citation: GONG Long-dong, SHEN Xiu-li. Mesoscopic modeling of three-dimensional four-directional braided composites using energy method[J]. Journal of Aerospace Power, 2015, 30(1): 106-113. doi: 10.13224/j.cnki.jasp.2015.01.015

基于能量法的三维四向编织复合材料细观建模

doi: 10.13224/j.cnki.jasp.2015.01.015
详细信息
    作者简介:

    巩龙东(1987-),男,山东泰安人,博士生,主要从事SiCf/SiC复合材料应用于航空发动机热端部件研究.

  • 中图分类号: V231.9;TB332

Mesoscopic modeling of three-dimensional four-directional braided composites using energy method

  • 摘要: 基于三维四向编织携纱器运动规律和内部纤维束受力分析,提出一种基于能量法的细观建模方法,将建模过程分解为纤维束打紧后控制点的调整、纤维束相互挤压缠绕空间位置的改变和应变能最小时纤维束轨迹的确定.通过单胞模型几何尺寸分析,建立了单胞模型与编织参数之间的对应关系.该建模方法得到的纤维束模型互不干涉且紧密压实,纤维束轨迹为空间曲线与其两条相切直线组成,轨迹接近直线.通过实验对比,纤维束轨迹、模型横截面图与电镜扫描得到的图像一致,计算得到的编织结构尺寸与实验测得数据吻合.花节长度最大计算相对误差在5%左右,特别是编织角在21°左右时,计算相对误差在2%以下.

     

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出版历程
  • 收稿日期:  2013-08-23
  • 刊出日期:  2015-01-28

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