Effect of Liner Cone Angle, Liner Thickness and Wave Shaper in Large Caliber Shaped Charge Warheads

M. Kumar, Y. Singh, P. Kumar
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Abstract

Shaped charge warheads are being utilized in defence applications against a wide variety of targets provided by armour, RCC and soil cover. Shaped charge warhead focus the explosive energy by the use of a cavity lined with metal normally called a liner. The concentration of energy along the axis of the warhead acts as force multiplier and hence lighter warheads are possible for deeper penetration. Performance of the shaped charge warhead is function of jet tip velocity, jet length and break up time (BUT). These performance parameters are greatly influenced by liner geometry, liner thickness and liner cone angle and selection of explosive. In this paper, simulations using AUTODYN numerical hydrocode were carried out to study the effect of liner geometry (Tulip vs conical), liner cone angle (50,60,70,80) and liner thickness(4mm,6mm,8mm,10mm and 12mm) on large caliber shaped charge warheads. Numerical simulations were also done to study the effect of wave shaper in shaped charge warhead. A shaped charge warhead of dia.340mm has been designed by using AUTODYN numerical hydrocode. OFE Copper (ASTM B152 C10100) is used as liner material. A wave shaper of dia.210mm and nylon material was used in shaped charge warhead. An Eulerian approach was used for the liner, casing, wave shaper and explosive parts. A single point initiation in the centre of the rear end of warhead was chosen. The numerical simulation results showed that the jettip velocity decreases in between 15-20% of liner position with increasing the cone angle when the other parameters are the same. For the cone angle 60, jet tip-velocity decreases as liner thickness is increased from 4mm (Vj-tip : 8.14 km/s) to 12mm (Vj-tip : 6.7 km/s). It was also realized that in case of wave shaper warhead there is more than 15% increase in jet tip velocity and 10% increase in jet length in comparison to without wave shaper warhead due to increase in collapse velocity of liner elements. The slug velocity is 1.22km/s in case of with wave shaper warhead whereas it was 1.05 km/s in without wave shaper. It means that a decision for the selection of liner geometry and dimensions of a shaped charge penetrator should be done according to target, required desired effect on target, permissible weight and available space for the warhead.
大口径聚能弹头衬板锥角、衬板厚度和波形器的影响
聚能弹头在防御应用中被用于对抗装甲、RCC和土壤覆盖提供的各种各样的目标。聚能弹头利用内衬金属的腔体集中爆炸能量,通常称为衬里。沿着弹头轴线的能量集中起着力量倍增器的作用,因此较轻的弹头可以进行更深的突防。聚能战斗部的性能是射流速度、射流长度和破碎时间的函数。这些性能参数受衬里几何形状、衬里厚度、衬里锥角和炸药选择的影响较大。本文采用AUTODYN数值模拟软件,研究了导管几何形状(Tulip vs锥形)、导管锥角(50、60、70、80)和导管厚度(4mm、6mm、8mm、10mm和12mm)对大口径聚能弹头的影响。通过数值模拟研究了整形器在聚能弹头中的作用。直径的聚能弹头。利用AUTODYN数值代码对340mm进行了设计。OFE铜(ASTM B152 C10100)用作衬里材料。直径的造波器聚能战斗部采用210mm和尼龙材料。对尾管、套管、增波器和爆炸部件采用欧拉方法。选择了弹头后端中心单点起爆。数值模拟结果表明,在其他参数相同的情况下,随着锥角的增大,射流速度在尾管位置的15 ~ 20%之间减小。当锥角为60时,随着衬板厚度从4mm (vj -叶尖:8.14 km/s)增加到12mm (vj -叶尖:6.7 km/s),射流尖端速度减小。同时还认识到,采用增波战斗部时,由于尾管元件塌缩速度的增加,射流尖端速度比不加增波战斗部时增加15%以上,射流长度比不加增波战斗部时增加10%以上。带增波弹头的段塞流速度为1.22km/s,不带增波弹头的段塞流速度为1.05 km/s。这意味着聚能穿甲弹的内衬几何形状和尺寸的选择应根据目标、对目标的期望效果、战斗部的允许重量和可用空间来决定。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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