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Finite element analysis of the impact of liner thickness and hydrodynamic limit on the penetration depth of a shaped charge warhead

机译:衬里厚度和流体动力学限制对成形电荷弹头渗透深度的有限元分析

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In this work, an identification method for the hydrodynamic limit of shaped charge jets (SCJs) is proposed using numerical analysis. To identify the hydrodynamic limit, we consider situations where two targets of the same density but different strengths are penetrated by the same SCJ. As a result, the SCJ corresponding with the hydrodynamic theory is a jet region with a velocity larger than 4 km/s. In addition, an investigation based on the hydrodynamic limit and liner thickness indicates that the penetration capability before and after the hydrodynamic limit improves as apex thickness decreases and base thickness increases, respectively. The simple and clear identification of the hydrodynamic limit is expected to be possible using the proposed method. Accordingly, a selective and organized liner thickness design can be developed.
机译:在这项工作中,提出了一种使用数值分析来提出成形电荷喷射器(SCJS)的流体动力极限的识别方法。 为了识别流体动力学极限,我们考虑两个目标相同密度但不同强度的两个目标被相同的SCJ渗透。 结果,与流体动力学理论相对应的SCJ是速度大于4km / s的喷射区域。 另外,基于流体动力学极限和衬垫厚度的研究表明,随着顶点厚度降低,基础厚度增加,水动力限制在水动力极限之前和之后的渗透能力分别增加。 使用所提出的方法,预计可以实现流体动力极限的简单明确的识别。 因此,可以开发选择性和有组织的衬里厚度设计。

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