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TRANSITION OF PLUGGING FAILURE MODES FOR DUCTILE METAL PLATES UNDER IMPACT BY FLAT-NOSED PROJECTILES

机译:扁形弹丸撞击下韧性金属板的插入失效模式的转变

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摘要

This article deals with the perforation of ductile metal plates subjected to impact by flat-nosed projectiles at normal incidence. Generally speaking, ductile metal plates under impact by flat-ended missiles can fail either by global deformation combined with local shear rupture or by localized adiabatic shear plugging depending upon the geometrical and thermo-mechanical properties of both the targets and the projectiles. Modification is first made to the Bai-Johnson model for adiabatic shear plugging by taking account of strain rate effects using a thermo-viscoplastic constitutive equation instead of thermoplastic material model and equations for the energy dissipated in the perforation process (perforation energy), the ballistic limit and the residual velocity are then obtained. Furthermore, a critical condition is obtained for differentiating localized adiabatic shear plugging from simple shear plugging failure with global deformations by comparing the modified Bai-Johnson model and the Wen-Jones model. It transpires that the present theoretical predictions are in good agreement with available experimental data in terms of the ballistic limits and the critical transition condition for the modes of plugging failure of ductile metal plates subjected to impact by flat-nosed missiles. It also transpires that the present model predicts well the residual velocities and the energies dissipated in the perforation process.
机译:本文涉及在垂直入射时易受扁鼻弹丸撞击的韧性金属板的穿孔。一般而言,取决于目标和弹丸的几何和热机械特性,受平端导弹撞击的易延展金属板可能会由于整体变形与局部剪切破裂或局部绝热剪切堵塞而失效。首先使用热粘塑性本构方程而不是热塑性材料模型和射孔过程中的射孔能量(射孔能量)方程,通过考虑应变率效应,对绝热剪切堵塞的Bai-Johnson模型进行了修改。然后获得极限速度和残余速度。此外,通过比较改进的Bai-Johnson模型和W​​en-Jones模型,获得了区分局部绝热剪切塞与简单剪切塞失败与整体变形的临界条件。可以看出,就弹道导弹的限制而言,目前的理论预测与可塑性试验的弹道极限和临界转变条件的弹道极限和临界过渡条件与现有的实验数据非常吻合。还可以证明,本模型很好地预测了射孔过程中的残余速度和能量消耗。

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