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含能材料  2013 

梳状靶法研究爆轰驱动全预制破片的飞行规律

DOI: 10.3969/j.issn.1006-9941.2013.05.019

Keywords: 爆炸力学,预制破片,飞行规律,梳状靶

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Abstract:

为了测量全预制破片在爆轰驱动下的长距离飞行速度,采用梳状靶测量实验方法测量了全预制钨合金破片的飞行速度。介绍了梳状靶测量实验方法原理,给出了典型的梳状靶信号。梳状靶测量实验方法测量的全预制钨合金破片的飞行速度与光幕靶实验方法和理论分析的破片飞行规律进行比较,结果表明,梳状靶实验方法可行,并与高精度的光幕靶测量结果一致。

References

[1]  Held M.Fragmentation Warheads[M]∥Carleone J.Tactical Missile Warheads.Washington DC: the American Institute of Aeronautics and Astronautics, Inc.1993: 462-464.
[2]  杨彦通, 龙洪明.导弹战斗部破片杀伤试验误差分析[J].国防技术基础, 2003(3): 28-29.YANG Yan-tong, LONG Hong-ming.Error analysis of fragments of missile warhead[J].Defensive Technique, 2003(3): 28-29.
[3]  DAVIDSON R O.Ammunition Series Section 2, Design for Terminal Effects[R]: AD389304,1976.
[4]  谭多望, 王广军.球形钨合金破片空气阻力系数实验研究[J].高压物理学报, 2007,21(3): 231-236.TAN Duo-wang, WANG Guang-jun.Air drag coefficients measurements of spherical Tu fragments[J].Chinese High Pressure Physics, 2007,21(3): 231-236.
[5]  Richard M L.Physics of directed hit and near miss warhead technology[M].Washington DC: the American Institute of Aeronautics and Astronautics, Inc.2001: 199-276.
[6]  谭多望, 曹仁义, 王广军.爆轰驱动对钨珠终点弹道性能的影[J].爆炸与冲击, 2008,28(6): 481-487.TAN Duo-wang, CAO Ren-yi, WANG Guang-jun.Flying property of Tu fragments nder detonation driven[J].Explosive and Shock Wave, 2008,28(6): 481-487.
[7]  Charron Y J.Estimation of velocity distribution of fragment warheads using a modified Gurney method[R].AD A074759,1979.
[8]  Victor A C.Warhead performance calculations for threat hazard assessment[C]∥1996 DDESB Explosives Safety Seminar.Las Vegas, Nevada, 1996: 1-20.
[9]  Г И鲍克洛夫斯基.爆炸及其作用[M].张国伟, 译.北京: 国防工业出版社, 1979: 48.Г И Pokrovsky.Explosion and its effects[M].ZHANG Guo-wei.Beijing: Publisher of Defensive Industry, 1979: 48.

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