首页> 外文期刊>南京航空航天大学学报(英文版) >DAMAGE MECHANISM ANALYSIS OF 2D 1 × 1 BRAIDED COMPOSITES UNDER UNIDIRECTIONAL TENSION
【24h】

DAMAGE MECHANISM ANALYSIS OF 2D 1 × 1 BRAIDED COMPOSITES UNDER UNIDIRECTIONAL TENSION

机译:单向拉伸作用下二维1×1编织复合材料损伤机理分析

获取原文
获取原文并翻译 | 示例
       

摘要

Coupling with the periodical displacement boundary condition ,a representative volume element (RVE) model is established to simulate the progressive damage behavior of 2D 1 × 1 braided composites under unidirection-al tension by using the nonlinear finite element method .Tsai-Wu failure criterion with various damage modes and Mises criterion are considered for predicting damage initiation and progression of yarns and matrix .The anisotropic damage model for yarns and the isotropic damage model for matrix are used to simulate the microscopic damage propagation of 2D 1 × 1 braided composites .Murakami′s damage tensor is adopted to characterize each damage mode .In the simulation process ,the damage mechanisms are revealed and the tensile strength of 2D 1 × 1 braided composites is predicted from the calculated average stress-average strain curve . Numerical results show good agreement with experimental data ,thus the proposed simulation method is verified for damage mechanism analysis of 2D braided composites .
机译:与周期性位移边界条件的耦合,建立代表体积元件(RVE)模型,以通过使用非线性有限元方法来模拟单向型张力下的2D 1×1编织复合材料的逐行损伤行为.TSAI-WU故障标准考虑各种损伤模式和误判标准用于预测纱线和矩阵的损伤启动和进展。纱线的各向异性损伤模型和基质各向同性损伤模型用于模拟2D 1×1编织复合材料的微观损伤传播.murakami'采用S损坏张量来表征每个损坏模式。在仿真过程中,揭示了损坏机构,并且从计算的平均应力平均应变曲线预测了2D 1×1编织复合材料的拉伸强度。数值结果显示了与实验数据的良好一致性,因此验证了所提出的仿真方法,验证了2D编织复合材料的损伤机制分析。

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