航空学报 > 1995, Vol. 16 Issue (1): 93-98

陶瓷/复合材料航空装甲撞击响应的数值仿真

龚尧南, 钱纯, 张佐光   

  1. 北京航空航天大学固体力学所, 北京, 100083
  • 收稿日期:1993-11-04 修回日期:1994-09-28 出版日期:1995-02-25 发布日期:1995-02-25

NUMERICAL SIMULATION OF IMPACT RESPONSE OF ADVANCED COMPOSED CERAMIC/COMPOSITE AERO ARMOUR

Gong Yaonan, Qian Chun, Zhang Zuoguang   

  1. Research Institute of Solid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing, 100083
  • Received:1993-11-04 Revised:1994-09-28 Online:1995-02-25 Published:1995-02-25

摘要: 用求解接触撞击问题的方法对陶瓷/复合材料装甲的撞击响应和失效机理进行数值仿真。着重讨论了接触撞击界面的搜索与确定、接触撞击力的计算、以及失效准则及其处理技巧等3个问题。计算结果与试验结果进行了比较,符合良好。

关键词: 接触载荷, 数据仿真, 复合材料

Abstract: The impact response and failure mechanism of the composed ceramic/composite armour are simulated numerically by use of the solution method to contact-impact problems. Emphasis is put on the searching and determination of the contact-impact interface between the projectile and armour, the algorithm for the contact-impact force calculation, the establishment of failure criterion and its implementation strategy. The computational results are compared and agreed well with those data resulted from test.

Key words: contactload, data simulat ion, composites

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