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Calculation and Verification on the Linear Instability of Shaped-Charge Jet Under Axial Pulse Current

机译:轴向脉冲电流作用下异形电荷射流线性不稳定性的计算与验证

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摘要

To improve the defense capability of passive electromagnetic armor against shaped-charge jet (SCJ), according to the superposition principle and the linear perturbation theory, the SCJ disturbance control equations are constructed and the 3-D equation is reduced to 1-D equation, consequently, the instability growth rates of the pinch and kink of SCJ and the varying law of instability growth rates with time and yield stress are obtained under the axial pulse current, which indicate that the instabilities must occur as long as the perturbations exit. Meanwhile, the SCJ deformation can be calculated through numerical method. The pinching experiments with a 39.2-mm diameter armor-piercing projectile proceeded when the charging voltage is 5370 V and the peak current is 140 kA. The kinking experiments with a 1.75-mm diameter copper wire proceeded when the charging voltage is 5140 V and the peak current is 43 kA. The experimental results demonstrate that axial pulse current can destroy the SCJ because of necking or kinking perturbation and confirm the validity of the theoretical analysis.
机译:为了提高无源电磁装甲对定型射流(SCJ)的防御能力,根据叠加原理和线性扰动理论,构造了SCJ扰动控制方程,并将3-D方程简化为1-D方程,因此,在轴向脉冲电流的作用下,获得了SCJ夹点和扭结的不稳定性增长速率以及不稳定性增长速率随时间和屈服应力的变化规律,这表明只要扰动消失就必须发生不稳定性。同时,SCJ变形可以通过数值方法来计算。当充电电压为5370 V,峰值电流为140 kA时,进行直径为39.2毫米的穿甲弹的夹紧实验。当充电电压为5140 V,峰值电流为43 kA时,进行了直径1.75毫米铜线的扭结实验。实验结果表明,轴向脉冲电流会由于颈缩或扭折扰动而破坏SCJ,并证实了理论分析的有效性。

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