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芳纶复合材料抗破片模拟弹丸侵彻的一种工程分析方法 被引量:4

Engineering Analysison Aramid Composite Penetration Performance by Fragment Simulating Projectile
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摘要 为研究芳纶复合材料抗破片模拟弹丸侵彻的性能,进行了4.5 g破片模拟弹丸侵彻15 mm厚芳纶靶板的穿甲实验。实验结果表明破片初速与穿透剩余速度呈线性关系,靶板的面密度吸收能可能存在极大值。进而提出一种破片模拟弹丸侵彻芳纶靶板的工程分析方法,给出了破片侵彻芳纶靶板的弹道极限速度与穿透剩余速度的预测公式,预测结果与实验结果有较好的一致性。并提出了面密度吸收能存在极大值,最后讨论了芳纶抗破片侵彻性能的表征方法。 To study penetration performance on aramid composite by fragment simulating projectile,ballistic impact experiments were performed on 15 mm aramid composite penetrated by 4. 5 g fragment simulating projectile. The results show that linear relationship exists between initial velocity and residual penetrating velocity,and a maximum value of energy absorption per areal density occurs. Then,engineering analysis was given on the aramid armor penetrated by fragment simulating projectile. The calculating formulas of ballistic velocity and residual velocity for aramid composite were given. The result of anylytical method agreed well with the test results. Then maximum value of energy absorption per areal density was put forward,finally,the characterization method of aramid composites penetrated by fragment was discussed.
出处 《弹箭与制导学报》 CSCD 北大核心 2014年第5期98-101,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 芳纶复合材料 面密度吸收能 侵彻力学 工程分析方法 aramid composite specific energy absorption per areal density penetration engineering analysis
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参考文献4

  • 1顾伯洪,孙宝忠.纺织结构复合材料冲击动力学[M].北京:科学出版社,2002.
  • 2C TLim,V B C Tan,C H Cheong.Perforation of highstrength double-ply fabric system by varying shaped projectiles[J].International Journal of Impact Engineering,2002,27(2):577-591.
  • 3H M Wen.Predicting the penetration and perforation of FRP laminates struck normally by projectiles with different nose shape[J].Composite Structures,2000,49(3):321-329.
  • 4徐小刚,贾光辉,黄海.单层板超高速撞击弹道极限方程综合建模[J].弹箭与制导学报,2009,29(5):183-185. 被引量:2

二级参考文献6

  • 1乐莉,闫军,钟秋海.超高速撞击仿真算法分析[J].系统仿真学报,2004,16(9):1941-1943. 被引量:22
  • 2贾光辉,黄海,胡震东.超高速撞击数值仿真结果分析[J].爆炸与冲击,2005,25(1):47-53. 被引量:26
  • 3Hayashida KB, Robinson JH. Single wall penetration equations[R]. NASA TM-103565, 1991.
  • 4Xu Xiaogang, Huang Hal, Safety analysis of spacecraft Jia Guanghui, et al. shielding under hypervelocity impact[C]// Proceedings of the seventh international conference on reliability, maintainability and safety, Beijing, 2007 : 584-588.
  • 5Cour-Palais, BG. Hypervelocity impact investigations and meteoroid shielding experience related to Apollo and Skylab[R]. NASA-S-82-05009, 1984.
  • 6Christiansen, EL. Shield sizing and response equations[R], NASA-SN3-91-42, 1991.

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