High Velocity Impact Response of Composite Lattice Core Sandwich Structures

被引：26

作者：

Wang, Bing ^{[1
]}

Zhang, Guoqi ^{[1
]}

Wang, Shixun ^{[2
]}

Ma, Li ^{[1
]}

Wu, Linzhi ^{[1
]}

机构：

[1] Harbin Inst Technol, Ctr Composite Mat, Harbin 150001, Peoples R China

[2] Beijing Inst Astronaut Syst Engn, Beijing 100076, Peoples R China

来源：

APPLIED COMPOSITE MATERIALS | 2014年 / 21卷 / 02期

基金：

美国国家科学基金会;

关键词：

Carbon fiber; Impact behaviour; Finite element analysis (FEA); STEEL SPHERE; HYPERVELOCITY IMPACT; BALLISTIC IMPACT; PERFORATION; CFRPS; PLATES; SIMULATION; HONEYCOMB; LAMINATE; BEHAVIOR;

D O I：

10.1007/s10443-013-9345-4

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

In this research, carbon fiber reinforced polymer (CFRP) composite sandwich structures with pyramidal lattice core subjected to high velocity impact ranging from 180 to 2,000 m/s have been investigated by experimental and numerical methods. Experiments using a two-stage light gas gun are conducted to investigate the impact process and to validate the finite element (FE) model. The energy absorption efficiency (EAE) in carbon fiber composite sandwich panels is compared with that of 304 stainless-steel and aluminum alloy lattice core sandwich structures. In a specific impact energy range, energy absorption efficiency in carbon fiber composite sandwich panels is higher than that of 304 stainless-steel sandwich panels and aluminum alloy sandwich panels owing to the big density of metal materials. Therefore, in addition to the multi-functional applications, carbon fiber composite sandwich panels have a potential advantage to substitute the metal sandwich panels as high velocity impact resistance structures under a specific impact energy range.

引用

页码：377 / 389

页数：13

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