Design and development of new spiral head projectiles undergoing ballistics impact

IF 3.5 Q1 ENGINEERING, MULTIDISCIPLINARY
V. Pranay, S. Panigrahi
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引用次数: 0

Abstract

PurposeThe purpose of this study is to design and develop new spiral head projectiles undergoing ballistics impact.Design/methodology/approachThe introduction of the rifled barrel in firearms made projectile spin during its flight path. The central translational velocity (impact velocity) is one parameter to defeat/penetrate the target in the penetration process. Another important parameter considered to be the shape of the projectile. Many types of projectile shapes have been designed to defeat the target. In the recent years, ogival nose shape is one of the well-known projectile shapes in use abundantly. The present research is made to design the nose shape so as to use the spin during the penetration of target effectively. In this study, a new spiral head projectile shape is proposed and designed, which uses the rotation of projectile (spin) for penetrating the Al7075-T6 target. When the ogive and new spiral head projectile is impacted on Al 7075-T6 target of 12.5 mm, 18 mm thicknesses at ordnance velocities, the residual velocity is evaluated numerically using ANSYS/Explicit Dynamics at normal impact condition. Two projectile materials, steel 4340 and tungsten alloy, are used as projectile materials. Along with the translational velocity, rotation velocities (spin rate) 13,000, 26,000 and 52,000 rad/s also provided to projectile. The residual velocities verses spin rate are plotted for different spiral angle projectiles for impact velocities 1,000–1,500 m/s, at normal impact conditions on the Al 7075-T6 target. Compared with the ogive nose projectile, the proposed new spiral head projectile made of tungsten alloy is significantly effective.FindingsSpiral head projectile having tungsten alloy material gives encouraging results at 12.5 mm target thickness. The new spiral head projectile is damaged partially. At 18 mm target thickness impact conditions, it is observed that the projectile head is completely damaged. The effectiveness of spiral head projectile on a target plate thickness of 18 mm is considered to study the impact condition.Research limitations/implicationsAll the above results need to be experimentally verified. However, the basic numerical model used in the present study, i.e. the basic ogive nose numerical model with only translational energy, is well validated with penetration theory available in literatures.Practical implicationsThe designed new spiral head projectile is only effective with tungsten alloy material within considered design parameters. For steel 4340 material, the spiral head projectile is less effective than the ogive nose projectile. In tungsten alloy projectiles, by observing all considered spiral angles, 30-degree spiral angle projectile gives the best performance at most of the considered impact velocity conditions.Originality/valueThe proposed research outputs are original, innovative and, have lot of importance in defence applications particularly in arms and ammunitions.
新型弹道冲击螺旋头弹的设计与研制
目的本研究的目的是设计和开发新型弹道冲击螺旋头弹。设计/方法/方法在火器中引入线膛枪管使炮弹在飞行过程中旋转。中心平移速度(冲击速度)是在穿透过程中击败/穿透目标的一个参数。另一个被认为是抛射物形状的重要参数。已经设计了许多类型的炮弹形状来击败目标。弧鼻形是近年来广泛使用的一种著名的弹形。本研究的目的是设计机头形状,以便有效地利用目标穿透过程中的旋转。在本研究中,提出并设计了一种新的螺旋头弹丸形状,该形状利用弹丸的旋转(旋转)来穿透Al7075-T6目标。当拱形和新型螺旋头炮弹以军械速度撞击厚度为12.5mm、18mm的Al 7075-T6目标时,在正常撞击条件下,使用ANSYS/显式动力学对残余速度进行了数值评估。两种射弹材料,钢4340和钨合金,被用作射弹材料。除了平移速度外,还为抛射体提供了13000、26000和52000 rad/s的旋转速度。在Al 7075-T6靶的正常撞击条件下,绘制了冲击速度为1000–1500 m/s的不同螺旋角射弹的残余速度与旋转速率的关系图。与弧鼻弹相比,所提出的新型钨合金螺旋头弹效果显著。Findings具有钨合金材料的螺旋弹头在目标厚度为12.5毫米时产生了令人鼓舞的结果。新型螺旋头炮弹部分损坏。在18毫米目标厚度的冲击条件下,可以观察到射弹头部完全损坏。为了研究螺旋头弹对18mm厚靶板的冲击条件,考虑了螺旋头弹的有效性。研究局限性/含义所有上述结果都需要通过实验验证。然而,本研究中使用的基本数值模型,即仅具有平移能的基本尖鼻数值模型,与文献中可用的穿透理论得到了很好的验证。实际意义所设计的新型螺旋头弹只有在所考虑的设计参数范围内使用钨合金材料才有效。对于4340钢材料,螺旋头弹的效果不如尖鼻弹。在钨合金弹中,通过观察所有考虑的螺旋角,30度螺旋角弹在大多数考虑的冲击速度条件下都具有最佳性能。独创性/价值拟议的研究成果具有独创性、创新性,在国防应用中具有重要意义,尤其是在武器弹药方面。
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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来源期刊
International Journal of Structural Integrity
International Journal of Structural Integrity ENGINEERING, MULTIDISCIPLINARY-
CiteScore
5.40
自引率
14.80%
发文量
42
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