首页|期刊导航|爆炸与冲击|重复冲击载荷下Al0.3CoCrFeNi高熵合金的动态响应机制与累积损伤效应

重复冲击载荷下Al0.3CoCrFeNi高熵合金的动态响应机制与累积损伤效应OA

Dynamic response mechanism and cumulative damage effect of Al0.3CoCrFeNi high-entropy alloy under repeated impact loading

中文摘要英文摘要

为了揭示高熵合金(high-entropy alloy,HEA)在冲击载荷下的相结构演变、位错分布、能量吸收及冲击累积效应的变化规律,通过分子动力学模拟,系统探讨了Al0.3CoCrFeNi 高熵合金板在受单次及二次冲击载荷下的动态响应行为.结果显示,首次冲击下,Al0.3CoCrFeNi高熵合金板的塑性区域相结构演变和能量吸收方式具有显著的冲击速度依赖性.随着冲击速度的提高,面心立方相结构的比例呈现三阶段下降趋势,而无序化结构则相应增加.在低速(0.5~1.0 km/s)冲击下,能量主要通过位错网络进行吸收;在中速(1.0~2.0 km/s)冲击下,位错与无序化原子共同吸收能量;在高速(2.0~3.0 km/s)冲击下,无序化原子主导吸收能量.位错线长度在刚性球 0.5~0.8 km/s的冲击速度范围内,随冲击速度的提高呈线性增大,而在更高的速度冲击下,因HEA板厚度限制,位错线长度呈下降趋势.应力分析表明,冲击速度提高时,最大应力与塑性区域边界应力随着冲击速度的提高表现出非线性变化的二次函数关系.二次冲击下,几何特征方面,Al0.3CoCrFeNi 高熵合金板在冲击后形成类梯形的破坏区域,其上坑半径随冲击速度的变化呈现二次函数关系,二次冲击的最小影响区域也与冲击速度呈现二次函数关系;抗冲击性能方面,随着刚性球首次冲击速度的提高,其二次冲击后的剩余速度也随之上升,HEA板材料抵抗冲击性能降低.在距冲击中心 10 nm处,HEA板的弹道极限随首次冲击速度的提高而非线性减小,然而,二次冲击速度的提高会使首次冲击的影响减弱.

To investigate the evolution of phase structure,dislocation distribution,energy absorption capacity,and impact accumulation effect of high-entropy alloys (HEA) under shock loading,molecular dynamics simulations were employed to systematically analyze the dynamic response behavior of Al0.3CoCrFeNi HEA plate subjected to single and secondary impact load. The results show that under the first impact,the phase structure evolution and energy absorption mode of the plastic region of Al0.3CoCrFeNi HEA plate exhibits significant velocity dependence. As the velocity increases,the proportion of face-centered cubic structure shows a three-stage downward trend,while the disordered structure increases accordingly. Under low velocity impact (0.5-1.0 km/s),energy is mainly absorbed by dislocation network;at medium velocity impact (1.0-2.0 km/s),both dislocations and disordered atoms contribute;under high velocity impact (2.0-3.0 km/s),disordered atoms dominate energy absorption. Within the velocity range of 0.5-0.8 km/s of the rigid sphere,the dislocation line length increases linearly with the impact velocity. However,at higher impact velocities,the dislocation line length decreases due to the limitation of the plate thickness. The stress analysis shows that when the impact velocity increases,both the maximum stress and the boundary stress of the plastic zone exhibit nonlinear variations characterized by a quadratic relationship. Under the secondary impact,the Al0.3CoCrFeNi HEA plate forms a damage zone resembling a trapezoidal shape after impact. The radius of the pit within this damage zone exhibits a quadratic relationship with the impact velocity. Additionally,the minimum affected area resulting from the secondary impact also demonstrates a quadratic relationship with the impact velocity.Regarding impact resistance,as the initial impact velocity increases,the residual velocity following the secondary impact also rises,indicating a reduction in the resistance capability of HEA. At a distance of 10 nm from the impact center,the ballistic limit velocity decreases nonlinearly with increasing initial impact velocity. However,an increase in the secondary impact velocity mitigates the effects induced by the initial impact.

陈嘉琳;李述涛;安明;周龙云;张生;李镕辛;陈叶青

军事科学院国防工程研究院目标易损性评估国家重点实验室,北京 100036军事科学院国防工程研究院目标易损性评估国家重点实验室,北京 100036东南大学物理学院,江苏 南京 211189军事科学院国防工程研究院目标易损性评估国家重点实验室,北京 100036军事科学院国防工程研究院目标易损性评估国家重点实验室,北京 100036军事科学院国防工程研究院目标易损性评估国家重点实验室,北京 100036军事科学院国防工程研究院目标易损性评估国家重点实验室,北京 100036

数理科学

高熵合金重复冲击分子动力学动态缺陷演化累积损伤

high-entropy alloyrepeated impactmolecular dynamicsdynamic defect evolutioncumulative damage

《爆炸与冲击》 2026 (3)

1-21,21

10.11883/bzycj-2025-0106

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