Xu Kezhong, Zhai Hua, He Linghui, Ni Yong, Lu Pin, Wang Gangfeng, Liu Xuepeng
Anhui Province Key Lab of Aerospace Structural Parts Forming Technology and Equipment, Institute of Industry and Equipment Technology, Hefei University of Technology, Hefei, Anhui, 230009, People's Republic of China.
CAS Key Laboratory of Mechanical Behavior and Design of Materials, University of Science and Technology of China, Hefei, Anhui 230026, People's Republic of China.
J Phys Condens Matter. 2022 Jul 22;34(38). doi: 10.1088/1361-648X/ac8194.
Molecular dynamics simulations are performed to study the mechanical properties and deformation mechanisms of a heterogeneous face-centered cubic/ body-centered cubic Cu/Ta nanolayered composite under uniaxial tension and compression. The results show that the stress-strain curves exhibit two main yield points in tension while only one yield point during compression, and the deformation primarily experiences three stages. The first stage is linearly elastic at small strains, followed by the nucleation and propagation of dislocations and stacking faults in the Cu layers, and eventually the Ta layers yield to plastic deformation. The yield of the specimen is mainly determined by the dislocation evolution in the hard phase (i.e. Ta layers), which leads to a sharp drop in the stress-strain curve. We show that the heterogeneous nanolayered composite exhibits a good deformation compatibility during compression but an obvious deformation incompatibility between Cu and Ta layers in tension. The temperature effect is also systematically investigated. It is revealed that the yield of the specimen at higher temperature depends only on the dislocation evolution in the thick Ta layers, and the yield strengths in tension and compression both decrease with the increasing temperature. In particular, our computations show that high temperature can significantly suppress the dislocation activities in the Cu layers during deformation, which results in a lower dislocation density of the Cu layers compared with that of the Ta layers and thus causing an incompatible fashion among the constituent layers.
进行分子动力学模拟以研究异质面心立方/体心立方Cu/Ta纳米层状复合材料在单轴拉伸和压缩下的力学性能及变形机制。结果表明,应力-应变曲线在拉伸时呈现两个主要屈服点,而在压缩时只有一个屈服点,且变形主要经历三个阶段。第一阶段是在小应变下的线性弹性阶段,随后是Cu层中位错和堆垛层错的形核与扩展,最终Ta层屈服进入塑性变形阶段。试样的屈服主要由硬相(即Ta层)中的位错演化决定,这导致应力-应变曲线急剧下降。我们表明,异质纳米层状复合材料在压缩过程中表现出良好的变形相容性,但在拉伸时Cu层和Ta层之间存在明显变形不相容性。还系统研究了温度效应。结果表明,较高温度下试样的屈服仅取决于厚Ta层中的位错演化,拉伸和压缩时的屈服强度均随温度升高而降低。特别是,我们的计算表明,高温可显著抑制变形过程中Cu层中的位错活动,这导致Cu层的位错密度低于Ta层,从而导致组成层之间出现不相容的变形方式。