Ciepielewski Radosław, Miedzińska Danuta
Faculty of Mechanical Engineering, Military University of Technology, Kaliskiego 2 Street, 00-908 Warsaw, Poland.
Materials (Basel). 2023 Mar 9;16(6):2211. doi: 10.3390/ma16062211.
Aluminum honeycomb structures are used in the construction of protective materials due to the positive relationship between their mass and their energy-absorbing properties. Applying such materials in the construction of large machinery, such as military vehicles, requires the development of a new method of finite element modeling, one that considers conditions with high strain rates, because a material model is currently lacking in the available simulation software, including LS-DYNA. In the present study, we proposed and verified a method of numerically modeling honeycomb materials using a simplified Y element. Results with a good level of agreement between the full core model and the Y element were achieved. The obtained description of the material properties was used in the subsequent creation of a homogeneous model. In addition, we considered the influence of increases in pressure and the leakage of the air entrapped in the honeycomb cells. As a result, we were able to attain a high level of accuracy regarding the stress values across the entire range of progressive failure, from the loss of stability to full core densification, and across a wide range of strain rates.
由于铝蜂窝结构的质量与其能量吸收特性之间存在正相关关系,因此它们被用于防护材料的构造中。将此类材料应用于大型机械(如军车)的构造中,需要开发一种新的有限元建模方法,该方法要考虑高应变率条件,因为包括LS-DYNA在内的现有模拟软件目前缺乏材料模型。在本研究中,我们提出并验证了一种使用简化Y单元对蜂窝材料进行数值建模的方法。全芯模型与Y单元之间取得了具有良好一致性水平的结果。所获得的材料特性描述被用于随后创建均匀模型。此外,我们考虑了压力增加和困在蜂窝单元中的空气泄漏的影响。结果,我们能够在从稳定性丧失到全芯致密化的整个渐进破坏范围内以及在很宽的应变率范围内,对应力值达到很高的精度。