Gao Dianwei, Zhang Jianhua, Zhang Chunwei, You Yun
School of Architecture and Civil Engineering, Shenyang University of Technology, Shenyang 110870, China.
Multidisciplinary Center for Infrastructure Engineering, Shenyang University of Technology, Shenyang 110870, China.
Materials (Basel). 2023 Jul 25;16(15):5219. doi: 10.3390/ma16155219.
Re-entrant auxetics offer the potential to address lightweight challenges while exhibiting superior impact resistance, energy absorption capacity, and a synclastic curvature deformation mechanism for a wide range of engineering applications. This paper presents a systematic numerical study on the compressive and flexural behaviour of re-entrant honeycomb and 3D re-entrant lattice using the finite element method implemented with ABAQUS/Explicit, in comparison with that of regular hexagonal honeycomb. The finite element model was validated with experimental data obtained from the literature, followed by a mesh size sensitivity analysis performed to determine the optimal element size. A series of simulations was then conducted to investigate the failure mechanisms and effects of different factors including strain rate, relative density, unit cell number, and material property on the dynamic response of re-entrant auxetics subjected to axial and flexural loading. The simulation results indicate that 3D re-entrant lattice is superior to hexagonal honeycomb and re-entrant honeycomb in energy dissipation, which is insensitive to unit cell number. Replacing re-entrant honeycomb with 3D re-entrant lattice leads to an 884% increase in plastic energy dissipation and a 694% rise in initial peak stress. Under flexural loading, the re-entrant honeycomb shows a small flexural modulus, but maintains the elastic deformation regime over a large range of strain. In all cases, the compressive and flexural dynamic response of re-entrant auxetics exhibits a strong dependence on strain rate, relative density, and material property. This study provides intuitive insight into the compressive and flexural performance of re-entrant auxetics, which can facilitate the optimal design of auxetic composites.
折返式负泊松比材料有潜力应对轻量化挑战,同时在广泛的工程应用中展现出卓越的抗冲击性、能量吸收能力以及双曲度曲率变形机制。本文采用ABAQUS/Explicit有限元方法,对折返式蜂窝结构和三维折返式晶格结构的压缩和弯曲行为进行了系统的数值研究,并与常规六边形蜂窝结构进行了比较。有限元模型通过文献中的实验数据进行了验证,随后进行了网格尺寸敏感性分析以确定最佳单元尺寸。然后进行了一系列模拟,研究了应变率、相对密度、单胞数量和材料特性等不同因素对折返式负泊松比材料在轴向和弯曲载荷下动态响应的失效机制和影响。模拟结果表明,三维折返式晶格结构在能量耗散方面优于六边形蜂窝结构和折返式蜂窝结构,且对单胞数量不敏感。用三维折返式晶格结构取代折返式蜂窝结构可使塑性能量耗散增加884%,初始峰值应力提高694%。在弯曲载荷下,折返式蜂窝结构的弯曲模量较小,但在较大应变范围内保持弹性变形状态。在所有情况下,折返式负泊松比材料的压缩和弯曲动态响应都强烈依赖于应变率、相对密度和材料特性。本研究为折返式负泊松比材料的压缩和弯曲性能提供了直观的认识,有助于优化设计负泊松比复合材料。