非金属壳体低附带战斗部实验与破片飞散分析

杨世全; 孙传杰; 钱立新; 卫剑锋

doi:10.11858/gywlxb.20170573

非金属壳体低附带战斗部实验与破片飞散分析

doi: 10.11858/gywlxb.20170573

中国工程物理研究院总体工程研究所, 四川绵阳 621999

详细信息

作者简介:
杨世全(1973-), 男, 硕士, 主要从事常规战斗部研制工作.E-mail:yangsq@caep.cn

中图分类号: O355
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出版历程
- 收稿日期: 2017-04-27
- 修回日期: 2017-05-11

Experimentation and Fragment Flight Analysis of Low-Collateral-Damage Warhead with Nonmetal Shell

Institute of Systems Engineering, CAEP, Mianyang 621999, China

摘要

摘要: 为了研究低附带战斗部的非金属破片飞散特性，结合某低附带杀伤战斗部静爆威力实验，对战斗部爆炸产生的非金属破片初速以及速度衰减情况进行了分析。基于能量守恒得到了包含壳体结构和材料强度因素的破片初速公式；基于破片在空气中飞行运动情况的分析，通过对球形破片阻力公式和等效面积进行修正，得到了非金属自然破片的速度衰减规律。所得结果较好地解释了战斗部静爆实验中的破片终点效应情况，亦可为该类战斗部破片毁伤效应评估提供一种分析方法。
- 低附带毁伤战斗部 /
- 非金属破片 /
- 飞行速度 /
- 衰减规律
Abstract: In this work we examined and characterized the original velocity and flight velocity attenuation of the nonmetal fragments of a certain low-collateral-damage warhead in combination with its explosive power experiment.We obtained the fragments' original velocity including the shell configuration and material strength factors based on the conservation of energy, and derived the flight velocity attenuation regularity from the analysis of its fragment flight movement in the air and the modification of its resistance formula and the equivalent area of the spherical fragment.Our analytical result was confirmed by the experimental result, thus providing an analytical method for evaluating the fragment damage efficiency of this kind of warhead.
- low-collateral-damage warhead /
- nonmetal fragment /
- flight velocity /
- attenuation regularity

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图 1 战斗部结构示意

Figure 1. Scheme of warhead structure

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图 2 实验场地布置情况

Figure 2. Experiment layout

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图 3 典型破片飞散情况

Figure 3. Typical fragment flight

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图 4 实验后的效应靶

Figure 4. Efficiency target after experiment

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图 5 实验回收到的部分破片

Figure 5. Fragments retrieved from experiment

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图 6 破片飞行速度随飞行距离的变化关系

Figure 6. Variation of fragment flightvelocity with flight distance

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图 7 最大破片动能随飞行距离的变化关系

Figure 7. Variation of maximum fragmentkinetic energy with flight distance

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参考文献(16)

[1]	BRINKLEY R F.Ballistics of projectile fragments[M].Pennsylvania:Bureau of Mine, 1968:73-78.
[2]	谭多望, 温殿英, 张忠兵, 等.球形破片长距离飞行时速度衰减规律研究[J].高压物理学报, 2002, 16(4):271-275. doi: 10.11858/gywlxb.2002.04.006 TAN D W, WEN D Y, ZHANG Z B, et al.Experimental studies on flight performances of spherical fragment[J].Chinese Journal of High Pressure Physics, 2002, 16(4):271-275. doi: 10.11858/gywlxb.2002.04.006
[3]	马永忠, 赵田安, 汪勇.弹丸破片速度衰减规律研究[J].弹道学报, 2006, 18(4):54-56. http://d.wanfangdata.com.cn/Periodical_ddxb200604015.aspx MA Y Z, ZHAO T A, WANG Y.Velocity attenuation regularity of projectile fragments[J].Journal of Ballistics, 2006, 18(4):54-56. http://d.wanfangdata.com.cn/Periodical_ddxb200604015.aspx
[4]	吴洪波, 王笑寒, 孔丽.舰空导弹战斗部破片飞散运动规律解析[J].舰船电子工程, 2012, 32(5):34-36. http://d.old.wanfangdata.com.cn/Periodical/jcdzgc201205012 WU H B, WANG X H, KONG L.Analysis of dispersion movement rule of warhead fragment for ship-air missile[J].Ship Electronic Engineering, 2012, 32(5):34-36. http://d.old.wanfangdata.com.cn/Periodical/jcdzgc201205012
[5]	姚文进, 王晓鸣, 李文彬, 等.低附带毁伤弹药爆炸威力的理论分析与试验研究[J].火炸药学报, 2009, 32(2):21-24. doi: 10.3969/j.issn.1007-7812.2009.02.006 YAO W J, WANG X M, LI W B, et al.Theory analysis and experiment research on blast effect of low collateral damage ammunition[J].Chinese Journal of Explosive & Propellants, 2009, 32(2):21-24. doi: 10.3969/j.issn.1007-7812.2009.02.006
[6]	黄德雨, 张云逸, 王坚茹, 等.低附带陶瓷球形破片衰减规律研究[J].弹箭与制导学报, 2011, 31(1):100-102. doi: 10.3969/j.issn.1673-9728.2011.01.028 HUANG D Y, ZHANG Y Y, WANG J R, et al.A study on distance decay of spherical ceramic fragments with low collateral damage[J].Journal of Projectiles, Rocket, Missiles and Guidance, 2011, 31(1):100-102. doi: 10.3969/j.issn.1673-9728.2011.01.028
[7]	张明, 王坚茹, 王光志, 等.破片材料对低附带毁伤弹药影响特性研究[J].兵器材料科学与工程, 2013, 36(6):94-97. doi: 10.3969/j.issn.1004-244X.2013.06.034 ZHANG M, WANG J R, WANG G Z, et al.Low collateral damage ammunition impact characteristics of fragment material[J].Ordnance Material Science and Engineering, 2013, 36(6):94-97. doi: 10.3969/j.issn.1004-244X.2013.06.034
[8]	刘俊, 姚文进, 郑宇, 等.低附带弹药的炸药/钨粉质量比对钨粉抛撒特性的影响[J].含能材料, 2015, 23(3):258-264. doi: 10.11943/j.issn.1006-9941.2015.03.011 LIU J, YAO W J, ZHENG Y, et al.Effect of explosive/tungsten powder mass ratio for LCD ammunition on dispersal characteristics of tungsten powder[J].Chinese Journal of Energetic Materials, 2015, 23(3):258-264. doi: 10.11943/j.issn.1006-9941.2015.03.011
[9]	高海鹰, 卢永刚, 王建民, 等. 低附带杀伤弹药威力特性及杀伤效应试验研究[C]//2012年含能材料与钝感弹药技术学术研讨会文集. 三亚, 2012. GAO H Y, LU Y G, WANG J M, et al. Experimental research on low collateral damage munitions explosion in air[C]//The Forum Corpus of Energetic Materials and Insensitive Ammunition in 2012. Sanya, 2012.
[10]	北京工业学院.爆炸及其作用:下册[M].北京:国防工业出版社, 1979. Beijing Institute of Technology.Explosion and its action:Volume Ⅱ[M].Beijing:National Defense Industrial Press, 1979.
[11]	晨阳化工内部资料. 改性尼龙检验报告单[Z]. 2014-12-15.
[12]	刘大有.二相流体动力学[M].北京:高等教育出版社, 1993:26-58. LIU D Y.Fluid dynamics of two-phase systems[M].Beijing:Higher Education Press, 1993:26-58.
[13]	郭烈锦.两相与多相流动力学[M].西安:西安交通大学出版社, 2002:342-351. GUO L J.Fluid dynamics of two-phase and multiphase flow[M].Xi'an:Xi'an Jiaotong University Press, 2002:342-351.
[14]	刘鹤年.流体力学[M].北京:中国建筑工业出版社, 2004:96-98. LIU H N.Fluid mechanics[M].Beijing:Chinese Architecture Industry Press, 2004:96-98.
[15]	YIN C G, ROSENDAHL L, KÆR S K, et al.Modeling the motion of cylindrical particles in a nonuniform flow[J].Chemical Engineering Science, 2003, 58(15):3489-3498. doi: 10.1016/S0009-2509(03)00214-8
[16]	隋树元, 王树山.终点效应学[M].北京:国防工业出版社, 2000:2-3. SUI S Y, WANG S S.Terminal effects[M].Beijing:National Defense Industrial Press, 2000:2-3.