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复合材料层合板鸟撞损伤及吸能影响因素数值分析
引用本文:于连超,陈伟,关玉璞,温海涛.复合材料层合板鸟撞损伤及吸能影响因素数值分析[J].航空动力学报,2008,23(6):1106-1110.
作者姓名:于连超  陈伟  关玉璞  温海涛
作者单位:南京航空航天大学,能源与动力学院,南京 210016
摘    要:数值分析是进行复合材料构件抗鸟撞损伤设计工作中的重要内容.主要采用瞬态非线性有限元分析方法结合文献试验对层合板鸟撞过程进行数值分析,分析了鸟撞层合板的初始损伤情况以及某一时刻各层的应力、应变情况;对比分析了铺层顺序、层合板参数、鸟体参数的变化对层合板吸收能量的影响.分析结果对航空复合材料层合构件抗鸟撞研究具有一定的参考价值.

关 键 词:航空、航天推进系统  鸟撞  复合材料  层合板  数值分析
文章编号:1000-8055(2008)06-1106-05
收稿时间:2007/5/28 0:00:00
修稿时间:2007年5月28日

Numerical analysis of the damage of bird impaction against composite laminates and the influence factors on absorbing energy
YU Lian-chao,CHEN Wei,GUAN Yu-pu and WEN Hai-tao.Numerical analysis of the damage of bird impaction against composite laminates and the influence factors on absorbing energy[J].Journal of Aerospace Power,2008,23(6):1106-1110.
Authors:YU Lian-chao  CHEN Wei  GUAN Yu-pu and WEN Hai-tao
Institution:Collage of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Collage of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Collage of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;Collage of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The numerical analysis is a very important work in the process of design on how composites resist the damage from bird impact.The paper analyzed and tested numerically the initial damage,stress and strain of every layer of laminates from bird impact using instantaneous non-linear FEM.It also analyzed how the changes of ply stacking sequence,parameter of laminates and birds affect the absorbing energy of laminates.The results of this paper provide a basis for further research on composite structures resisting bird impact.
Keywords:aerospace propulsion system  bird impact  composites  laminate  numerical analysis
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