Study on low-velocity impact response and residual strength of ultralight all-CFRP sandwich structure

被引:0
|
作者
Chu, Ziqi [1 ,2 ]
Chen, Xiaojian [1 ,3 ]
Tian, Shubin [1 ,2 ]
Wu, Linzhi [1 ,2 ,4 ]
Wu, Qianqian [4 ]
Yu, Guocai [1 ,2 ]
机构
[1] Harbin Engn Univ, Key Lab Adv Ship Mat & Mech, 145 Nantong St, Harbin 150001, Peoples R China
[2] Harbin Engn Univ, Coll Aerosp & Civil Engn, Dept Engn Mech, Harbin, Peoples R China
[3] China Acad Launch Vehicle Technol, Beijing, Peoples R China
[4] Harbin Inst Technol, Ctr Composite Mat, 2 Yikuang St, Harbin 150001, Peoples R China
基金
中国国家自然科学基金;
关键词
All-CRRP sandwich structure; stretching process; low-velocity impact; residual strength; failure mechanism;
D O I
10.1177/10996362241287409
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The all-CFRP sandwich structure with ultralight honeycomb is designed and manufactured by stretching process. Two scenarios, including global and local impact, are considered to reveal the characteristics of impact resistance. The effects of different impact energies and core densities on energy absorption and failure mechanism are thoroughly discussed. Meanwhile, the post-impact residual compressive strength is carried out to evaluate the influence of impact on structural strength and stability. The results show that under the global impact, the impact resistance is related to core density, and the energy absorption is mainly from honeycomb core. While under the local impact, as the impact energy increases, the failure mechanism of the structure changes from core crushing to penetration. The research provides a guidance for low-velocity impact performance and structural optimization design of sandwich structures.
引用
收藏
页码:1661 / 1683
页数:23
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