期刊文献+

长径比对动能杆飞散特性影响的数值模拟 被引量:2

Numerical Simulation of the Relation Between Slenderness Ratio and Flight-characteristics of KE-rod
原文传递
导出
摘要 为研究长径比对定向式动能杆飞散特性的影响规律,以非线性动力分析软件LS-DYNA为工具,分别对11种不同长径比的动能杆进行数值模拟,得出动能杆飞散速度、空间分布与动能杆长径比的关系:当长径比大于5小于11时,动能杆的速度呈递增趋势,当长径比大于11时,动能杆的速度趋于平缓,有所降低;从空间分布看,长径比大于5小于8时,动能杆的空间分布较密集,长径比大于8时,动能杆的空间分布相对散开,分布也均匀,当长径比为11时,动能杆的飞散速度和空间分布最优。和文献中的数据进行对比,仿真与文献中数值计算结果基本吻合,和实验稍有差距,可能是由数值模拟采用的材料模型和试验所用的材料有一定误差所致。仿真结果可为此类战斗部的设计提供参考。 This paper studies the effect of the slenderness ratio on the dispersion characteristics of the aimed KE-rod warhead, with the nonlinear dynamic analysis software ES-DYNA, 11 different slenderness ratios of the KE-rod are considered, and the relationship among the KE-rod speed, the spatial distribution and the slenderness ratio is obtained When the slenderness ratio is greater than 5 and less than 11, the speed of the KE-rod increases with the slenderness, and when the slenderness ratio is greater than 11, the speed decrease slowly; for the spatial distribution, when the slenderness ratio greater than 5 and less than 8, the spatial distribution of the KE-rod is more intensive, when the slenderness ratio is greater than 8, the distribution is relatively dispersed and uniform, when the slenderness ratio is 11, the velocity and spatial distribution of the KE-rod is optimal. The simulation results are basically consistent with those in the literature, and differ slightly with those obtained by experiments. The simulation results can provide a reference for the design of this type of warhead.
出处 《科技导报》 CAS CSCD 北大核心 2013年第9期55-58,共4页 Science & Technology Review
基金 航空科学基金项目(20120196006)
关键词 长径比 动能杆 LS-DYNA 数值模拟 slenderness kinetic energy rod LS-DYNA numerical simulation
  • 相关文献

参考文献9

  • 1余建斌,刘惠玲,张涛,等.撞击杆式战斗部反导毁伤机理[C].中国兵工学会弹道专业委员会弹道学术交流会,北京.1997.
  • 2Lloyd R M. Conventional warhead system and engineering design [M]. Virginia: American Institute of Aeronautics and Astronautics, Inc, 1998.
  • 3Lloyd R M. Physics of direct hit and near miss warhead technology[M]. Virginia: American Institute of Aeronautics and Astronantics, Inc, 2001.
  • 4Gentilello J A, Cole M. Aimed rod warhead design and performance [C]. 45th Annual Bomb and Warhead America Defence Preparedness Association, Los Angeles, USA, May 17-18, 1995.
  • 5蒋建伟,门建兵,卢永刚,蒋道建.动能杆定向抛撒规律的数值模拟[J].爆炸与冲击,2004,24(1):85-89. 被引量:7
  • 6李金河,谭多望,方青.定向式动能杆战斗部飞散实验研究[J].高能量密度物理,2008(4):161-165. 被引量:5
  • 7LSTC. LS-DYNA keyword user's manual [M]. California: Livermore Software Technology Corporation, 2007.
  • 8万军.动能杆类战斗部杀伤元素爆炸驱动的数值模拟研究[D].长沙:国防科学技术大学,2002.
  • 9Schwalbe L computation International 23-28, 1996 A, Wingate C A, Stofleth J H, et al. Experiment and studies of rod-deployment mechanisms [C]. 16th Symposium on Ballistcs, San Francisco, USA, September.

二级参考文献5

  • 1[1]Lioyd R M. Conventional Warhead System Physics and Engineering Design[M]. American Institute of Aeronautis and Astronautics, 1999:179.
  • 2[2]Gentilello J A, Cole M. Aimed rod warhead design and performance[A]. 45th Annual Bomb and Warhead America Defence Preparedness Association[C]. Alabama, USA, 1995:7-10.
  • 3[3]Schwalbe. Experiment and computational studies of rod-deployment mechanisms[A]. 16th International Symposium on Ballistics[C]. San Francisco, CA, 1998:246-252.
  • 4[5]AUTODYNTM User Manual Revision 3.0[C]. Century Dynamics Inc,1997.
  • 5[6]Dobratz B M, Crawford P C. LLNL Explosives Handbook[Z]. 1985.

共引文献9

同被引文献10

引证文献2

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