[1]全嘉林,苗润源,梁争峰.不同类型预制破片速度衰减规律及迎风面积的修正[J].爆破器材,2019,48(06):28-32.[doi:10.3969/j.issn.1001-8352.2019.06.006]
 QUAN Jialin,MIAO Runyuan,LIANG Zhengfeng.Velocity Attenuation Rule of Different Prefabricated Fragments and Correction of Windward Area[J].EXPLOSIVE MATERIALS,2019,48(06):28-32.[doi:10.3969/j.issn.1001-8352.2019.06.006]
点击复制

不同类型预制破片速度衰减规律及迎风面积的修正()
分享到:

《爆破器材》[ISSN:1001-8352/CN:32-1163/TJ]

卷:
48
期数:
2019年06
页码:
28-32
栏目:
基础理论
出版日期:
2019-12-09

文章信息/Info

Title:
Velocity Attenuation Rule of Different Prefabricated Fragments and Correction of Windward Area
文章编号:
5359
作者:
全嘉林苗润源梁争峰
西安近代化学研究所(陕西西安,710065)
Author(s):
QUAN Jialin MIAO Runyuan LIANG Zhengfeng
Xi’an Modern Chemistry Research Institute (Shaanxi Xi’an, 710065)
关键词:
杀伤战斗部预制破片破片速度速度衰减迎风面积
Keywords:
fragmenting warhead prefabricated fragment fragment velocity velocity attenuation windward area
分类号:
TJ410.3+3
DOI:
10.3969/j.issn.1001-8352.2019.06.006
文献标志码:
A
摘要:
为研究不同速度区间典型预制破片在空气中飞行的速度衰减规律,采用基于多普勒效应的雷达测速装置,获得了典型球形和长方体破片在1.5 Ma~4.0 Ma速度区间内的速度衰减规律和衰减系数,并对长方体破片迎风面积的确定方法进行了修正。结果表明:球形破片衰减系数拟合值与经典理论计算值吻合良好,Φ7 mm和Φ8 mm球形破片的速度衰减系数分别为0.007 61 m-1和0.006 65 m-1;而长方体破片衰减系数的试验值与经典理论计算值相比明显偏低,约为理论计算值的0.75~0.95倍;长方体破片迎风面积修正系数kMa近似呈线性关系。
Abstract:
In order to study the velocity attenuation rule of typical prefabricated fragments flying in the air at different velocity intervals, velocity attenuation rule and attenuation coefficient of typical spherical and rectangular fragments in the velocity interval of 1.5 Ma-4.0 Ma were obtained by radar velocity measurement device based on Doppler effect. Moreover, the method for determining the windward area of rectangular fragments was modified. The results show that the fitting values of the attenuation coefficients of spherical fragments are in good agreement with those calculated by classical theory. The velocity attenuation coefficients of spherical fragments of Φ7mm and Φ8mm are 0.007 61 m-1 and 0.006 65 m-1, respectively. While the experimental values of the attenuation coefficients of cuboid fragments are significantly lower than those that was calculated by classical theory, which are about 0.75-0.95 times of the theoretical values. Windward area correction coefficient k of cuboid fragments is approximately linear with Ma.

参考文献/References:

[1]郑雄伟,孙兴昀,周涛.美俄海军防空反导战斗部技术研究综述[J].飞航导弹,2016(4):48-51,62.
[2]易春林,李丽萍,吕永柱,等.Φ8钨球破片速度衰减试验及速度预报方法研究[J].弹箭与制导学报,2014,34(6):61-63,67. YI C L, LI L P,
?Lǔ Y Z, et al.Study on velocity attenuation regularity of Φ8 tungsten spherical fragment and speed forecast[J].Journal of Projectiles,Rockets,Missiles and Guidance,2014,34(6):61-63,67.
[3]杨世全,孙传杰,钱立新,等.非金属壳体低附带战斗部实验与破片飞散分析[J].高压物理学报,2018,32(4):131-135.
YANG S Q, SUN C J, QIAN L X,et al. Experimentation and fragment flight analysis of low-collateral-damage warhead with nonmetal shell[J].Chinese Journal of High Pressure Physics,2018,32(4):131-135.
[4]KPENYIGBA K M, JANKOWIAK T, RUSINEK A, et al. Effect of projectile nose shape on ballistic resistance of interstitial-free steel sheets[J]. International Journal of Impact Engineering,2014,79:83-94.
[5]王儒策, 赵国志.弹丸终点效应[M].北京:北京理工大学出版社,1993.
[6]王鹏, 马晓青, 高润芳. 圆柱形破片形状系数研究[J]. 弹箭与制导学报, 2005, 25(3):161-163,166.
WANG P, MA X Q, GAO R F. Research on figure modulus of cylindrical fragment [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2005, 25 (3): 161-163,166.
[7]白蕊霞,王斌永,童鹏.激光多普勒测速雷达技术研究现状[J].激光与红外,2016,46(3):249-253.
BAI R X, WANG B Y, TONG P. Research status of laser Doppler velocity radar technology[J].Laser and Infrared,2016,46(3):249-253.
[8]中国物理研究院.面杀伤导弹战斗部静爆威力试验方法:第2部分 破片初速测试:GJB 6390.2—2008 [S].北京:总装备部军标出版发行部,2008.
China Academy of Engineering Physics. Static power method for anti-surface missile warhead:part 2 measurement of initial velocity of fragments: GJB 6390.2—2008 [S].Beijng:Military Standard Publishing Department of General Armament Department, 2008.
[9]隋树元,王树山. 终点效应学[M]. 北京: 国防工业出版社,2000.
[10]马玉媛.小型预制破片的速度衰减和侵彻深度的研究[J]. 兵工学报, 1981, 2(1):52-58.
MA Y Y. A study on the velocity dampings and penetrating depth of small preformed fragments [J].Acta Armamentarii, 1981, 2(1): 52-58.
[11]DAVIDSON R O.Ammunition series section 2,design for terminal effects:AD389304[R]. 1976.
[12]韩子鹏.弹箭外弹道学[M].北京:北京理工大学出版社,2008.

相似文献/References:

[1]臧立伟,尹建平,王志军.轴向预制破片战斗部的设计研究[J].爆破器材,2013,42(02):5.[doi:10.3969/j.issn.1001-8352.2013.02.002]
 ZANG liwei,YIN Jianping,WANG Zhijun.Optimizing Design of Axial Prefabricated Fragments[J].EXPLOSIVE MATERIALS,2013,42(06):5.[doi:10.3969/j.issn.1001-8352.2013.02.002]
[2]董晓亮①,李文彬①,沈晓军②.预制破片对复合毁伤元战斗部发散角的影响[J].爆破器材,2018,47(06):15.[doi:10.3969/j.issn.1001-8352.2018.06.003]
 DONG Xiaoliang,LI Wenbin,SHEN Xiaojun.Influence of Pre-fragment on Divergence Angle of Warhead with Combined Damage Elements[J].EXPLOSIVE MATERIALS,2018,47(06):15.[doi:10.3969/j.issn.1001-8352.2018.06.003]

备注/Memo

备注/Memo:
收稿日期:2019-05-15
第一作者:全嘉林(1997-),男,硕士研究生,主要从事爆炸力学与战斗部技术研究。E-mail:quan_jialin@163.com
通信作者:梁争峰(1972-),男,博士,研究员,主要从事爆炸力学与弹药技术研究。E-mail:1697589935@qq.com
更新日期/Last Update: 2019-12-04