Dynamic response and failure mechanism of S-shaped CFRP foldcore sandwich structure under low-velocity impact

被引:22
作者
Deng, Yunfei [1 ]
Zhou, Nan [1 ]
Li, Xiang [1 ]
Wang, Xuan [1 ]
Wei, Gang [1 ]
Jia, Huiru [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
Composites; Foldcore sandwich structure; Impact; Failure mechanism; Dynamic response; CORE STRUCTURES; BEHAVIOR;
D O I
10.1016/j.tws.2022.109007
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
To study the impact resistance of the S-shaped carbon-fiber foldcore sandwich structure, the S-shaped foldcore was prepared by the hot press molding process, and then the S-shaped carbon-fiber foldcore sandwich structure was designed by face-to-core bonding and curing through a secondary bonding process. Two hemispherical impactors with different diameters were used to preload different energies to impact the node position and base position of the sandwich panel, respectively, revealing the failure mechanism, response characteristics of the sandwich panel, and the influence of various variables on the impact resistance of the structure. The research shows that the panel of S-shaped foldcore sandwich structure has tensile fracture failure. The core is affected by the structural characteristics and load-bearing forms, and there are mainly two failure modes of brittle crushing fracture and tensile fracture. The load-displacement curve shows that the relative size of the impactor and the unit cell of the core has a significant influence on the impact damage behavior. The sandwich panel has better impact resistance for the impactor with diameter greater than the cell span, and the difference between different impact positions is reduced. In application, the span of the core cell can be reduced to further improve the protective effect of the structure. The sandwich structure studied in this paper is lightweight and has good impact resistance, which can be used in the field of lightweight protection in the future.
引用
收藏
页数:19
相关论文
共 45 条
[1]   On the impact response of sandwich composites with cores of balsa wood and PVC foam [J].
Atas, Cesim ;
Sevim, Cenk .
COMPOSITE STRUCTURES, 2010, 93 (01) :40-48
[2]   Numerical modeling of the geometrical defects of an origami-like sandwich core [J].
Baranger, E. ;
Guidault, P. -A. ;
Cluzel, C. .
COMPOSITE STRUCTURES, 2011, 93 (10) :2504-2510
[3]   Dynamic axial crushing of multilayer core structures of folded Chevron patterns [J].
Basily, BB ;
Elsayed, EA .
INTERNATIONAL JOURNAL OF MATERIALS & PRODUCT TECHNOLOGY, 2004, 21 (1-3) :169-185
[4]   Low-velocity impact response of composite sandwich structures: Modelling and experiment [J].
Chen, Yuan ;
Hou, Shujuan ;
Fu, Kunkun ;
Han, Xu ;
Ye, Lin .
COMPOSITE STRUCTURES, 2017, 168 :322-334
[5]   Compression response of sandwich structure with M-type CFRP foldcore [J].
Cong, Linxin ;
Sun, Yuguo .
MODERN TECHNOLOGIES IN MATERIALS, MECHANICS AND INTELLIGENT SYSTEMS, 2014, 1049 :1071-1074
[6]   Experimental investigation on low-velocity impact response of wood skinned sandwich composites with different core configurations [J].
Demircioglu, T. K. ;
Balikoglu, F. ;
Inala, O. ;
Arslan, N. ;
Ay, I. ;
Atas, A. .
MATERIALS TODAY COMMUNICATIONS, 2018, 17 :31-39
[7]  
Deng YF., 2022, ACTA AERONAUT ASTRON, V43, DOI [10.7527/S1000-6893.2021.25446, DOI 10.7527/S1000-6893.2021.25446]
[8]   Fabrication and mechanical behaviors of carbon fiber reinforced composite foldcore based on curved-crease origami [J].
Du, Yuntong ;
Song, Changping ;
Xiong, Jian ;
Wu, Linzhi .
COMPOSITES SCIENCE AND TECHNOLOGY, 2019, 174 :94-105
[9]   Compression after impact performance of carbon-fiber foam-core sandwich composites in low temperature arctic conditions [J].
Elamin, Mohammed ;
Li, Bing ;
Tan, K. T. .
COMPOSITE STRUCTURES, 2021, 261
[10]   A method for building self-folding machines [J].
Felton, S. ;
Tolley, M. ;
Demaine, E. ;
Rus, D. ;
Wood, R. .
SCIENCE, 2014, 345 (6197) :644-646