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超高速不锈钢球冲击铝板中界面演化的数值模拟研究

NUMERICAL INVESTIGATION ON INTERFACE EVOLUTION DURING THE HYPERVELOCITY IMPACT OF A STAINLESS-STEEL SPHERE ON AN ALUMINUM PLATE

  • 摘要: 超高速碰撞现象广泛存在于航天器空间碎片防护、军事装甲毁伤评估以及天体物理撞击坑形成等领域. 针对有限厚度金属靶板在超高速冲击下的动态响应, 特别是激波在介质中的传播及介质界面演化机理, 仍需深入的定量化研究以指导防护结构设计. 为此, 本文就超高速不锈钢球冲击铝板这一典型问题, 展开了数值模拟研究. 研究基于欧拉框架下的多介质弹塑性流动数值模拟方法, 构建了模拟不锈钢球超高速冲击有限厚度铝板的二维轴对称模型. 模型结合了可描述大变形的超弹性本构关系及考虑应变硬化与热软化的塑性模型, 能够捕捉超高速冲击过程中介质变形及波系传播. 基于此, 本研究通过捕捉冲击过程中早期波系结构(包括初始激波及反射稀疏波)的动力学演化过程, 揭示了波系作用对界面演化的影响规律, 并重点探究了不锈钢球初始速度  U_\textP 和铝板初始厚度 H_\textT0 对冲击过程的影响特性. 具体地, 研究识别并定义了“穿透模态”与“未穿透模态”两种典型的流动模态, 构建了基于  U_\textP 和 H_\textT0 的流动模态相图. 结果表明, 随着  U_\textP 增加, 介质中初始激波强度显著增强; 随着 H_\textT0 减小, 铝板下表面反射形成的稀疏波增强. 初始激波或反射稀疏波的增强会引发更强的后续激波和稀疏波, 使铝板承受更高强度的冲击. 因此, 随着  U_\textP 增大或 H_\textT0 减小, 流动模态从未穿透模态转变为穿透模态.

     

    Abstract: Hypervelocity impact phenomena are commonly observed in various fields, including spacecraft shielding against space debris, military armor damage assessment, and the formation of astrophysical craters. However, the dynamic response of finite-thickness metal plates under hypervelocity impact still necessitates further exploration. In particular, the propagation of shock waves within materials and the resulting interface-evolution mechanisms require in-depth study to quantitatively inform the design of protective structures. To this end, this study investigates the hypervelocity impact of a stainless-steel sphere on an aluminum plate by numerical simulation. A two-dimensional axisymmetric model simulating the hypervelocity impact of a stainless-steel sphere on a finite-thickness aluminum plate is developed based on a numerical method for multi-material elastic-plastic flow under the Eulerian framework. The developed model employs a hyperelastic constitutive relation to describe large deformations and a plasticity model that accounts for strain hardening and thermal softening, enabling accurate capture of material deformation and wave propagation during the impact process. In this way, this study reveals the effects of waves on interface evolution by closely examining both material deformation and wave propagation during impact. Furthermore, particular focus is given to the effects of the initial impact velocity of the stainless-steel sphere  U_\textP and the initial thickness of the aluminum plate H_\textT0 on the impact behavior. Two typical flow modes are identified as “penetrated mode” and the “unpenetrated mode”. A flow-mode phase diagram is then confirmed in the parameter space defined by  U_\textP and H_\textT0 . The results demonstrate that increasing  U_\textP significantly enhances the strength of the initial shock wave, while decreasing H_\textT0 intensifies the rarefaction wave reflected from the rear surface of the aluminum plate. The enhancement of either the initial shock wave or the reflected rarefaction wave induces stronger subsequent shock and rarefaction waves within the materials, causing the aluminum plate to experience higher-intensity impacts. Consequently, as  U_\textP increases or H_\textT0 decreases, the flow mode transitions from the unpenetrated mode to the penetrated mode.

     

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