复合材料科学与工程 ›› 2021, Vol. 0 ›› Issue (10): 5-12.DOI: 10.19936/j.cnki.2096-8000.20211028.001

• 基础研究 •    下一篇

基于渐进均匀化多尺度方法的CFR平纹机织材料冲击后压缩损伤研究

张晨曦1, 娄源峰2, 铁瑛1*, 丛世凡1, 李要磊1   

  1. 1.郑州大学 机械与动力工程学院,郑州450001;
    2.周口职业技术学院 建筑工程学院,周口466002
  • 收稿日期:2020-12-30 出版日期:2021-10-28 发布日期:2021-11-03
  • 通讯作者: 铁瑛(1978-),女,博士,教授,主要从事先进机械结构的设计与损伤强度分析、机械结构无损检测等方面的研究,tieying@zzu.edu.cn。
  • 作者简介:张晨曦(1993-),男,硕士研究生,主要从事复合材料冲击后压缩损伤方面的研究。
  • 基金资助:
    国家自科基金民航联合基金(U1833116);河南省科技攻关项目(172102210001)

Research on compression damage of CFR plain woven material after impact based on progressive homogenization multi-scale method

ZHANG Chen-xi1, LOU Yuan-feng2, TIE Ying1*, CONG Shi-fan1, LI Yao-lei1   

  1. 1. School of Mechanical and Power Engineering, Zhengzhou University, Zhengzhou 450001, China;
    2. School of Architectural Engineering, Zhoukou Vocational and Technical College, Zhoukou 466002, China
  • Received:2020-12-30 Online:2021-10-28 Published:2021-11-03

摘要: 本文针对CFR平纹机织材料层合板低速冲击及冲击后压缩(CAI)响应和损伤问题,提出了一种渐进均匀化多尺度分析方法。基于渐进均匀化方法分别算出微观纤维束和介观子胞的等效强度和刚度,在这个基础上,采用三维Hashin失效准则以及连续损伤力学模型来模拟CFR平纹机织材料层合板的损伤起始和演化,用内聚力模型来模拟层间损伤。研究结果表明:CFR平纹机织材料低速冲击后压缩的仿真结果和试验结果吻合较好,验证了渐进均匀化多尺度方法的可靠性和准确性;随着冲击能量的递增,层合板的剩余压缩强度呈非线性下降。纤维损伤和基体损伤在低速冲击载荷下,随着冲击能量的增加,冲击损伤面积增大。而CAI行为则相反,压缩损伤面积随着冲击能量的增大而减小。

关键词: CFR平纹机织材料, 渐进均匀化, 多尺度模型, 低速冲击, 冲击后压缩, 复合材料

Abstract: A progressive homogenization multi-scale analysis method is developed to predict the response and damage of CFR plain woven laminates under low velocity impact and compression after impact (CAI) in this paper. First, a microscopic unit cell model of the carbon fiber bundle is established, the equivalent stiffness and strength of the fiber bundles are calculated. Then, a mesoscopic unit cell model is established, and the mechanical properties at 0° and 90° are calculated. Additionally, the mesoscopic model is transformed into an equivalent subcell model usinga progressive homogenization method, which is then expand into a macro-scale integrated three-dimensional finite element model with low-velocity impact and compression. The three-dimensional Hashin failure criterion and the continuous damage mechanics model are used to simulate the damage initiation and evolution of CFR plain woven material laminates, and the cohesive zone model is used to evaluate the interlayer damage. The results show that the numerical analysis results of CFR plain weave material after low-velocity impact and compression are in good agreement with the experimental results, which verifies the reliability and accuracy of the progressive homogenization multi-scale analysis method. With the increase of impact energy, the remaining compressive strength of the laminate decreases nonlinearly. For the fiber damage and matrix damage under low-velocity impact load, as the impact energy increases, the damage also increases. However, the CAI behavior is the opposite. The area of compression damage decreases with the increase of impact energy.

Key words: CFR plain weave material, progressive homogenization, multi-scale model, low-speed impact, compression after impact, composites

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