期刊文献+

碳纤维编织复合材料层合板抗侵彻性能研究

Study on Penetration Resistance of Carbon Fiber Braided Composite Laminates
原文传递
导出
摘要 通过弹道冲击实验开展了碳纤维编织复合材料层合板的抗侵彻性能研究,进行了动态响应分析和损伤模式分析。建立了基于Hashin失效和Yeh分层失效准则的渐进损伤模型,运用ABAQUS有限元软件模拟了碳纤维编织复合材料层合板的侵彻失效过程,采用Lambert-Jonas公式拟合了柱状弹侵彻层合板弹道极限曲线,对比分析了碳纤维编织复合材料层合板侵彻实验与数值模拟的弹道极限速度及损伤形貌。结果表明,层合板侵彻损伤模式主要为分层、纤维断裂和基体开裂失效,弹道极限速度数值模拟结果与实验结果吻合较好。 The penetration resistance of the carbon fiber braided composite laminates is studied by ballistic impact experiment.The trajectory limit curve of the carbon fiber braided composites is fitted according to the Lambert-Jonas formula.The damage pattern and mechanism of the carbon fiber braided composites are analyzed.The progressive damage model based on failure criterion of Hashin and Yeh is set up.The penetration process of the carbon fiber braided composite is simulated by the finite element software ABAQUS,and the ballistic limit velocity and damage morphology of the carbon fiber braided composites are compared between penetration test and simulation.Experimental and simulation results show that the damage modes mainly include delamination failure,fiber fracture failure and matrix cracking failure.The ballistic limit velocity of the simulation results matches well with that of the experimental results.
作者 罗锡林 魏建辉 李飘 刘志康 刘加一 LUO Xilin;WEI Jianhui;LI Piao;LIU Zhikang;LIU Jiayi(Wuhan Second Ship Design and Research Institute,Wuhan 430064,China;School of Naval Architecture and Ocean Engineering,Huazhong University of Science and Technology,Wuhan 430074,China)
出处 《材料开发与应用》 CAS 2023年第4期61-68,共8页 Development and Application of Materials
关键词 碳纤维编织复合材料 抗侵彻 弹道极限曲线 损伤模式 carbon fiber braided composites penetration resistance trajectory limit curve damage pattern
  • 相关文献

参考文献4

二级参考文献39

  • 1梅志远,朱锡,张立军.FRC层合板抗高速冲击机理研究[J].复合材料学报,2006,23(2):143-149. 被引量:28
  • 2许延敏,程小全,陈浩,胡仁伟.含孔平面编织混杂铺层层合板压缩性能[J].航空材料学报,2007,27(3):87-90. 被引量:5
  • 3牛春匀.实用飞机复合材料结构设计与制造[M].北京:航空工业出版社,2010.
  • 4郑海燕.编织复合材料的低速冲击及冲击后压缩特性研究-试验及数值计算[D].西安:西北工业大学,2002.
  • 5Chang KY, Liu S, Chang FK. Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings. J Comp Materi, 1991, 25:274-301.
  • 6Tan SC. A progressing failure model for composites laminated containing openings. J Comp Materi, 1991, 25: 556-577.
  • 7Kallmeyer AR. Stephens RI. A finite element model for predicting time-dependent deformation and damage acumination in laminated composite bolted joints. J Comp Materi, 1999, 33(9): 794-826.
  • 8Reifsmider K, Case S. The mechanics of composite strength evolution. Comp Sci Techn, 2000, 60:2539-2546.
  • 9Naik NK, Tiwari SI, Kumar RS. An analytical model for compressive strength of plain weave fabric composites. Composites Science and Technology, 2003(63): 609-625.
  • 10Christopher T. Key, Shane C. Schumacher, Andrew C. Hansen progressive failure modeling of woven fabric composite materials using multi continuum theory. Composites: Part B 2007, 38:247-257.

共引文献20

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部