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聚能线型切割器最佳张开角的理论分析 总被引:3,自引:0,他引:3
本文按不可压缩流体模型,研究滑移爆轰作用下,聚能线型切割器在三维碰撞下形成射流的理论。讨论了射流速度,穿甲流体模型的条件,射流分散对切割效果的影响,并推出了能量取极大值时的最佳金属罩张开角。 相似文献
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聚能射流侵彻厚靶时,对靶材同时进行轴向和径向挤压进而发生轴向侵彻和径向扩孔。本文中基于聚能射流侵彻可压缩模型并结合Szendrei-Held扩孔方程,推导给出考虑弹/靶材料可压缩性的聚能射流扩孔方程。为简化完整可压缩模型繁琐的计算过程,又基于Murnaghan状态方程给出可压缩模型的近似解。与水中聚能射流扩孔的实验研究对比分析,表明该模型预测优于Szendrei-Held扩孔方程。模型分析表明,射流半径、驻点压力、靶材强度、驻点处靶材密度以及聚能射流速度是影响聚能射流扩孔的主要因素。本文模型可以更准确地预测聚能射流侵彻可压缩性较强的靶材的扩孔情况。相关工作可为含液密闭结构干扰聚能射流侵彻提供理论基础。 相似文献
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对2岩石炸药的定常爆轰形成过程进行了实验研究;对起爆端稀疏波效应进行了计算。实验结果表明,距起爆端约10倍装药厚度以内为不定常爆轰区。距离起爆端小于5倍装药厚度时,飞板速度及碰撞角增幅较大,5~10倍装药厚度,两者增幅趋缓,10倍装药厚度以后,爆速、飞板速度及碰撞角逐步进入定常状态。飞板碰撞角的工程计算与实验结果的一致性较好。 相似文献
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在分析纵向磁场能够增强聚能射流稳定性的基础上,根据聚能射流的运动方程以及聚能射流的塑性失稳条件,推导得到了聚能射流在纵向磁场中的极限拉伸系数计算公式,并计算了有、无磁场情况下极限拉伸系数的比值。通过两种炸高下的实验研究对理论模型进行了验证。结果表明:由于磁场的存在而引起的电磁力抑制了聚能射流颈缩的发展,进而延长了射流成型的惯性拉伸阶段,最终使聚能射流在磁场中的极限拉伸系数在一定程度上得到了增加;理论和实验所得结果吻合较好。运用所建立模型可以较准确地反映磁场对聚能射流极限拉伸系数的影响。 相似文献
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对于不可压缩有势流动,有两类典型的不定边界或可动边界问题,即定常型不定边界如常水位闸门出流、过水坝或过水闸、水堰绕流及射流等,非定常型的不定边界如装液容器内的流体晃动问题.它们的共同特点是自由面位置与形状事先是的,需在计算过程中调整网格作自由面拟合.且由于自由面条件呈强烈非线性,给不确定数值计算带来困难.本文综述了两类不定边界问题的有限元和边界元模式,简述了笔者的一些计算经验. 相似文献
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构建了一套高精度的求解成形装药金属射流问题的数值方案,给出了适用于欧拉程序的同时考虑塑性温升和冲击温升的计算方法,通过固体炸药爆炸的经典算例证明了程序是高精度的。对成形装药金属射流进行了模拟,给出了炸药的起爆、金属衬垫的失效以及射流的形成过程。研究了衬垫形状对射流形状、速度和温度的影响,通过数值分析发现,随着衬垫顶角的增大,射流的长度变短,速度减小,衬垫材料的利用率有所增加;在爆炸载荷作用的初期,衬垫的温度随着衬垫顶角的减小而增大,而当射流形成并趋于稳定之后,4种衬垫构型产生的射流温度十分接近。 相似文献
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为研究药型罩对聚能射孔弹侵彻页岩储层的射孔和损伤致裂效果的影响机理,建立了射孔弹-空气-页岩三维模型,设置药型罩的锥角分别为50°、60°、70°和80°,壁厚分别为0.5、1.0和1.5 mm,材料分别为铜、钢、钛和钨。利用ANSYS/LS-DYNA软件进行数值计算,分别从射流速度与形态、页岩射孔效果及页岩孔裂隙形成规律特征等进行系统性分析。研究结果表明:在射孔弹结构中,随着药型罩锥角的减小,射流速度提高、杵体速度降低、侵彻深度增大同时开孔孔径减小。在一定范围内,适当减小药型罩的壁厚,可以提高射流速度、减小杵体质量、增大侵彻深度和开孔倾斜度。药型罩材料对射流速度、杵体结构和页岩射孔效果均有显著影响,其中钨药型罩射孔弹的侵彻深度最大但开孔孔径最小,钛药型罩射孔弹的侵彻深度最小但开孔倾斜度最大,铜比钢药型罩射孔弹的侵彻深度略大但开孔孔径略小。通过研究不同对照组的页岩孔裂隙形成规律特征发现,页岩孔裂隙发育主要发生在杵体对页岩的再扩孔阶段,减小射流初始扩孔孔径、增大杵体直径、提高杵体速度,可以促进页岩孔裂隙发育程度。 相似文献
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Jet formation and penetration mechanism of W typed shaped charge 总被引:1,自引:0,他引:1
Existing classical shaped charges are well known for their longer jets capable of achieving large hole depth to hole diameter ratios in metallic targets. However, in some situations, there arises demand to obtain 1:1 ratio for hole depth to hole diameter which is beyond normal shaped charges capability. A new variant of shape charge, named W typed shape charge (WSC), is proposed in this paper, which can meet the demand of 1:1 ratio, and is based on the geometry that can produce annular jets upon proper initiation scheme. In this paper, we present formation and penetration results of WSC based on three different schemes. We also show that not all WSC designs can form annular jets, only annularly initiated WSC, which also fulfils the "Internal-External Liners Equal-Impulse" criterion, has the capability to form annular jet. The experimental and numerical results show that when the ratio between annular initiation ring diameter and the charge diameter is 0.75, an annular jet is formed, which was also supported by high speed photographs performed in vacuum. 2D numerical simulations are performed with indigenously developed simulation software, where Eulerian approach with multi-material interface tracking algorithm is utilized, to find various mechanisms involved during jet formation process. The calculation results are found in good agreement with the experimental results, indicating that the interface treatment algorithm proposed in this paper can not only deal with large deformation problem, but also depict clearly the variation of materials interface. It is especially suitable for simulation of the process from liner collapse to formation of shaped charge jet. 相似文献
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The prediction of the penetration of three-dimensional (3D) shaped charge into steel plates is a challenging task. In this paper, the smoothed particle hydrodynamics (SPH) method is applied to simulate the jet formation generated by the shaped charge detonation and its damage to steel plates. The Jones–Wilkins–Lee (JWL) equation of state (EOS), Tillotson EOS, and elastic–perfectly plastic constitutive model were incorporated into SPH for the modeling of explosive detonation and dynamic behavior of metal material. The compute unified device architecture (CUDA) parallel programming interface has been employed in SPH to improve the computational efficiency of SPH. Firstly, the constitutive models and EOSs are validated by 3D TNT slab detonation and aluminum–aluminum (Al–Al) high velocity impact. Then the jet formation of the shaped charge detonation and its penetration into the steel plates are investigated using the graphics processing unit (GPU)-accelerated SPH methodology. The numerical results of these test cases are compared against the published experimental data or analytical result, which shows that the GPU-accelerated SPH methodology is capable of tackling the 3D shaped charge detonation and penetration involving millions of particles with high computational efficiency. 相似文献
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本文用脉冲X光摄影技术及电探极-记录仪系统,对射流引爆及侵彻工业炸药的过程进行了观测,探讨了的流引爆及侵彻工业炸药的机制,给出了射流与工业炸药作用过程的物理图象。 相似文献