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平面编织复合材料层压板低速冲击后的压缩失效
引用本文:范金娟,赵旭,陶春虎,程小全.平面编织复合材料层压板低速冲击后的压缩失效[J].高分子材料科学与工程,2010(5):108-110.
作者姓名:范金娟  赵旭  陶春虎  程小全
作者单位:北京航空材料研究院中国航空工业失效分析中心;北京航空航天大学航空科学与工程学院
摘    要:采用超声C扫描检测、断口分析、有限元分析等方法研究低速冲击损伤对G803/5224与G827/5224两种平面编织复合材料层压板失效行为的影响。结果表明,低速冲击后压缩载荷作用下,G803/5224层压板最终为剪切分层失效,G827/5224层压板最终为剪切屈曲失效,两种层压板低速冲击后压缩的失效模式与未受损伤层压板基本相同。建立了平面编织复合材料层压板的损伤扩展与失效模型,该模型的计算结果与试验结果吻合较好,可用于平面编织复合材料层压板的失效仿真。

关 键 词:平面编织复合材料层压板  冲击损伤  压缩失效  失效仿真

Compressive Failure of Plain Woven Composite Laminate with Low Velocity Impact Damage
FAN Jin-juan,ZHAO Xu,TAO Chun-hu,CHENG Xiao-quan.Compressive Failure of Plain Woven Composite Laminate with Low Velocity Impact Damage[J].Polymer Materials Science & Engineering,2010(5):108-110.
Authors:FAN Jin-juan  ZHAO Xu  TAO Chun-hu  CHENG Xiao-quan
Affiliation:1. Failure Analysis Center of AVIC,Beijing Institute of Aeronautical Materials,Beijing 100095,China; 2. School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 10083,China)
Abstract:The effects of low impact damage on compressive failure behavior of plain woven composite laminates were investigated by C-scan,fracture side face analysis and finite element analysis. The results show that G803/5224 laminate finally fails by shearing and delamination way,and shearing and buckling failure is the final failure mode of G827/5224 laminate. The failure of each kind of laminates with low velocity impact damage is basically in the same way with the intact counterpart. A damage evolution and failure model of plain wove composite laminate was established. The results from the model were consistent with the test results,so it can be concluded that the model can be employed to stimulate the failure process of plain wove composite laminate.
Keywords:plain woven composite laminate  impact damage  compressive failure  failure simulation
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