[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]Journal of Projectiles, Rockets, Missiles and Guidance >
Numerical Simulation of Explosive Dispersion of Prefabricated Fragments of Trapezoidal Cross-section Warhead
Received date: 2022-11-28
Online published: 2025-02-07
In order to obtain the flying characteristics of prefabricated fragments of trapezoidal section lethal warhead and provide reference for the design of trapezoidal section lethal warhead, the numerical simulation of prefabricated fragments driven by five kinds of trapezoidal section charge explosion was carried out by ANSYS/LS-DYNA software.The distribution law of fragments,the velocity of fragments on each trapezoid surface and the characteristics of fragments at different initiation points were obtained. The results show that the fragments on the four faces of trapezoid form four fragment bundles. The lower fragment flying angle is the largest, up to 105°.The fragmentation direction on the trapezoidal inclined plane is deflected under the trapezoidal relative to the normal direction of the inclined plane.The maximum deflection angle is 34.5°.When angle θ is smaller than 60°, the average fragment velocity on each surface of trapezoid increases by 8.6%.And the average velocity of fragments on the lower surface of trapezoid is greater than that on the upper surface of trapezoid. A large angle θ will decrease the average velocity of the fragment on the lower surface and the inclined surface of the trapezoid. The maximum velocity fragment is located on the upper part of the trapezoidal inclined plane. The initiation points at different positions on the trapezoidal symmetry axis have little effect on the circumferential scattering angle of fragments on each trapezoidal plane and the deflection angle of fragments on the inclined plane, but can increase the velocity of fragments in the contralateral direction,the fragment on the lower surface increased by 3.6%.The angle θ is 45° and the initiation point is set on the trapezoid, which can make the following fragments obtain the maximum killing power.
JIN Xin , XIAO Qiangqiang , HUANG Zhengxiang , MA Bin , ZU Xudong , JIA Xin . Numerical Simulation of Explosive Dispersion of Prefabricated Fragments of Trapezoidal Cross-section Warhead[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2023 , 43(3) : 26 -32 . DOI: 10.15892/j.cnki.djzdxb.2023.03.004
| [1] |
唐伟, 张勇, 李为吉, 等. 二次曲线截面弹身的气动设计及优化[J]. 宇航学报, 2004, 25(4): 429-433.
|
| [2] |
冉洪. 椭圆截面飞行器单独体(高)超声速气动性能初步研究[C]// 中国空气动力学会. 第一届近代实验空气动力学会议论文集. 北京: 原子能出版社, 2007: 418-424.
|
| [3] |
唐伟, 张勇, 马强, 等. 椭圆截面机动飞行器的气动设计[C]// 中国空气动力学会.全国第十三届高超声速气动力(热)学术交流会议论文集. 北京: 原子能出版社, 2005: 68-71.
|
| [4] |
|
| [5] |
|
| [6] |
杨祥, 武海军, 皮爱国, 等. 椭圆截面杀伤战斗部破片初速沿周向分布规律[J]. 北京理工大学学报, 2018, 38(增刊2): 178-183.
|
| [7] |
王钰婷, 黄正祥, 贾鑫, 等. 等腰梯形截面聚能装药射流成型及侵彻特性[J]. 兵工学报, 2022, 43(4): 748-757.
|
| [8] |
李鑫, 黄正祥, 贾鑫, 等. 等腰梯形截面形状对聚能射流成型的影响研究[J]. 弹箭与制导学报, 2022, 42(2): 23-27.
|
| [9] |
马彬, 岑乐山, 江涛, 等. 梯形截面聚能装药射流成型特性研究[J]. 弹箭与制导学报, 2022, 42(2): 16-21.
|
| [10] |
|
| [11] |
李元, 李燕华, 刘琛, 等. 预制破片战斗部爆轰产物泄露数值模拟[J]. 北京理工大学学报, 2017, 37(8): 778-782.
|
| [12] |
武敬博, 苟瑞君, 熊诗辉, 等. 六棱柱形战斗部预制破片驱动的数值模拟和实验[J]. 火炸药学报, 2016, 39(3): 89-94.
|
| [13] |
李元, 赵倩, 郑俊杰, 等. 一种异面棱柱战斗部威力特性的数值模拟[J]. 含能材料, 2019, 29(2): 97-103.
|
| [14] |
|
| [15] |
北京工业学院八系《爆炸及其作用》编写组. 爆炸及其作用[M]. 北京: 国防工业出版社, 1979: 199-201.
Eighth Department of Beijing Institute of Technology. Explosion and its application[M]. Beijing: National Defense Industry Press, 1979: 199-201.
|
/
| 〈 |
|
〉 |