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Two-scale damage failure analysis of 3D braided composites considering pore defects

机译:考虑孔隙缺陷的3D编织复合材料的两尺度损伤故障分析

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摘要

Pore defects tend to form in the manufacturing process, and significantly influence the mechanical properties of 3D braided composites. To predict the failure modes and strength properties considering pore defects, a two scale progressive damage method coupled with representative volume cell (RVC) has been developed due to the periodic feature across different scales of 3D braided composites. Different void generating methods across two scales are established, including the element-model by elements chosen and the void-model by voids explicitly constructed. The user-defined material subroutine (UMAT) is coupled in the nonlinear finite element analysis software ABAQUS to implement the damage model for micro and meso numerical models. Also, the Chamis model considering pore defects are employed and verified. It shows that results by void-model agree well with the Chamis model and the experimental data. And, the void-model is superior to the element-model when predicting the mechanical properties of braided composites. The pore defects weaken the matrix properties, and therefore largely determine the strength and damage mechanism of 3D braided composites with large braiding angle. This two-scale damage failure analysis method by void-model is effective to predict strength and damage failure mechanism of 3D braided composites considering pore defects.
机译:孔隙缺陷倾向于在制造过程中形成,并且显着影响3D编织复合材料的机械性能。为了预测考虑孔隙缺陷的故障模式和强度性质,由于3D编织复合材料的不同尺度的周期性特征,已经开发了一种与代表体积小区(RVC)耦合的两种逐步逐渐损伤方法。建立了两种尺度的不同void生成方法,包括所选择的元素的元素模型和通过明确构造的空白的void-model。用户定义的材料子程序(UMAT)耦合在非线性有限元分析软件ABAQU中,以实现微观和中学数值模型的损坏模型。此外,考虑孔隙缺陷的Chamis模型被采用和验证。它表明,空隙模型的结果与Chamis模型和实验数据很好。并且,在预测编织复合材料的机械性能时,空隙模型优于元素模型。孔隙缺陷削弱了基质特性,因此大大确定了具有大编织角度的3D编织复合材料的强度和损伤机理。通过空隙模型的这种两种尺度损伤故障分析方法对于考虑孔隙缺陷的3D编织复合材料的强度和损坏机制是有效的。

著录项

  • 来源
    《Composite Structures》 |2021年第3期|113556.1-113556.13|共13页
  • 作者单位

    Beijing Inst Technol Inst Adv Struct Technol Beijing 100081 Peoples R China;

    Beijing Inst Technol Inst Adv Struct Technol Beijing 100081 Peoples R China|Xi An Jiao Tong Univ State Key Lab Strength & Vibrat Mech Struct Xian Peoples R China|Beijing Inst Technol Beijing Key Lab Lightweight Multifunct Composite Beijing 10081 Peoples R China|Beijing Inst Technol State Key Lab Explos Sci & Technol Beijing 100081 Peoples R China;

    Aerosp Syst Engn Shanghai Yuanjiang Rd 3888 Shanghai 201109 Peoples R China|Shanghai Key Lab Spacecraft Mech Jindou Rd 3805 Shanghai 201108 Peoples R China;

    Guizhou Inst Technol Sch Mat & Met Engn Guiyang 550003 Peoples R China;

    Beijing Inst Technol Inst Adv Struct Technol Beijing 100081 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    3D braided composites; Two-scale analysis; Pore defects; Damage failure; Strength;

    机译:3D编织复合材料;双重分析;孔隙缺损;损坏失败;力量;
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