Experimental and numerical research on the dynamic response of sandwich structure with M-type foldcore under low-velocity impact

被引:7
作者
Deng, Yunfei [1 ]
Yin, Yuan [1 ]
Hu, Xiaoyu [1 ]
Li, Xiang [1 ]
机构
[1] Civil Aviat Univ China, Coll Aeronaut Engn, Tianjin 300300, Peoples R China
基金
中国国家自然科学基金;
关键词
Foldcore sandwich; low-velocity impact; impact characteristics; numerical model; specific energy absorption; BEHAVIOR; DAMAGE; SIMULATION; PLATES;
D O I
10.1080/15376494.2022.2145533
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In the field of lightweight structures, foldcore sandwich structure is regarded as a promising replacement for conventional honeycomb sandwich structure. In this study, a new M-type glass fiber foldcore structure was fabricated by hot-pressing molding technology, and the effects of various factors on the low-velocity impact characteristics were investigated. In addition, a 3 D progressive damage numerical model matching the experimental results was established. The results showed that the impact energy exerted a certain influence on the response characteristics of the sandwich structure, but did not change the development trend of the load curve. The sandwich panel was able to achieve the overall load-carrying potential for the impactor whose size was longer than the foldcore span (25 mm). In addition, as the sharpness of the impactor increased, the damage range of the sandwich panel became concentrated and the load-bearing capacity gradually decreased. As revealed by the findings, the maximum load and specific energy absorption of laminated sandwich panels were improved by 150 and 40% respectively compared to single sandwich panel at base position. Therefore, it is beneficial to appropriately reduce the core span and increase the number of laminations to improve impact resistance of foldcore sandwich in practical applications.
引用
收藏
页码:1932 / 1951
页数:20
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