The Dynamic response of shallow sandwich arch with auxetic metallic honeycomb core under localized impulsive loading

被引:59
|
作者
Li Ying [1 ,2 ]
Chen Zihao [2 ]
Xiao Dengbao [1 ,2 ]
Wu Wenwang [1 ,3 ]
Fang Daining [1 ,2 ]
机构
[1] Inst Adv Struct Technol, Beijing Inst Technol, Beijing Key Lab Lightweight Multifunct Composite, Beijing 100081, Peoples R China
[2] Beijing Inst Technol, State Key Lab Explos Sci & Technol, Beijing 100081, Peoples R China
[3] MIT, Dept Mech Engn, Cambridge, MA 02139 USA
基金
中国国家自然科学基金;
关键词
Auxetic reentrant honeycomb; Shallow sandwich arch; Dynamic response; Impulsive loading; Negative Poisson's ratio; INDENTATION RESPONSE; BLAST RESISTANCE; PANELS; BEHAVIOR; IMPACT; DEFORMATION; STRENGTH; PLATE;
D O I
10.1016/j.ijimpeng.2019.103442
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In recent years, auxetic metallic cellular material such as auxetic reentrant honeycomb is one of the research hotspot in metallic cellular materials due to its attractively negative Poisson's ratio. In this manuscript, the dynamic response of the end-clamped shallow sandwich arch with aluminum face sheets and auxetic reentrant hexagonal aluminum honeycomb core subjected to foam projectile with high-velocity impact was experimentally and numerically investigated. The reentrant honeycomb cores with different cell-wall thicknesses were fabricated by selective laser melting (SLM). The deformation processes of honeycomb core were captured by a high-speed camera. And deflection history of back face sheet was obtained using three-dimensional digital imaging correlation method (DIC) analysis system. Failure modes and deformation mechanisms of the sandwich arch were investigated. According to experiment results, the local negative Poisson's ratio deformation was found in honeycomb core. Then, a finite element (FE) model was established to study the dynamic deformation evolution of two face sheets and auxetic reentrant honeycomb core. The results showed that the honeycomb cells were not always undergoing shrinkage deformation and flowing into the loading center, while the local expand deformations of honeycomb core were also found.
引用
收藏
页数:13
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