Dynamic mechanical behavior of foam-core composite sandwich structures subjected to low-velocity impact

被引:14
作者
He, Yanbin [1 ,2 ,3 ]
Zhang, Xiaoqing [1 ,3 ]
Long, Shuchang [1 ]
Yao, Xiaohu [1 ,3 ]
He, Lingfeng [1 ]
机构
[1] South China Univ Technol, Sch Civil Engn & Transportat, Dept Engn Mech, Guangzhou 510640, Guangdong, Peoples R China
[2] Guangzhou Civil Aviat Coll, Guangzhou 510640, Guangdong, Peoples R China
[3] Beijing Inst Technol, State Key Lab Explos Sci & Technol, Beijing 100081, Peoples R China
关键词
Composite sandwich structures; Low-velocity impact; Foam core; PANELS; PREDICTION; DAMAGE;
D O I
10.1007/s00419-016-1138-4
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The dynamic response of foam-core composite sandwich plates subjected to low-velocity impact is thoroughly investigated by means of drop-weight impact tests and numerical simulations in this paper. The influences of impact energy, foam-core thickness, and punch-head shape and size on the impact mechanical behavior including the impact force time history, the dynamic displacement time history, the residual plastic deformation, the energy absorption capacity, and the back plate deflection are contrastively studied through the control-variant approaches. Several conclusions drawn are useful and helpful to the related product design. The top faceplates of specimens with large foam-core thickness are demonstrated to be vulnerable to the low-velocity impact under stepped levels of impact energy, while large foam-core thickness can reduce deformation of the interior plates effectively. Moreover, among the three representative types of punch heads, the sharper hemispherical one is checked to be the most destructive with the lowest impact force peak. Besides, a finite element model was built to investigate the damage of faceplates and foam cores. The numerical method was proved to be accurate and efficient. A series of results were obtained revealing the damage mode of faceplates and cores under different impact energies.
引用
收藏
页码:1605 / 1619
页数:15
相关论文
共 32 条
[21]   Delamination prediction in composite laminates under low-velocity impact [J].
Long, Shuchang ;
Yao, Xiaohu ;
Zhang, Xiaoqing .
COMPOSITE STRUCTURES, 2015, 132 :290-298
[22]   The response of honeycomb sandwich panels under low-velocity impact loading [J].
Meo, M ;
Vignjevic, R ;
Marengo, G .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2005, 47 (09) :1301-1325
[23]   Impact damage testing on composite marine sandwich panels. Part 2: Instrumented drop weight [J].
Muscat-Fenech, Claire De Marco ;
Cortis, Jeremy ;
Cassar, Charles .
JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2014, 16 (05) :443-480
[24]   Impact modeling of foam cored sandwich plates with ductile or brittle faceplates [J].
Rajaneesh, A. ;
Sridhar, I. ;
Rajendran, S. .
COMPOSITE STRUCTURES, 2012, 94 (05) :1745-1754
[25]  
Srivastava V.K., 2012, INT J COMPOS MAT, V2, P63
[26]   Experimental investigation of 3D sandwich structure with core reinforced by composite columns [J].
Wang, Bing ;
Wu, Linzhi ;
Jin, Xin ;
Du, Shanyi ;
Sun, Yuguo ;
Ma, Li .
MATERIALS & DESIGN, 2010, 31 (01) :158-165
[27]   Experimental and numerical study on the low-velocity impact behavior of foam-core sandwich panels [J].
Wang, Jie ;
Waas, Anthony M. ;
Wang, Hai .
COMPOSITE STRUCTURES, 2013, 96 :298-311
[28]   Theoretical and experimental study of foam-filled lattice composite panels under quasi-static compression loading [J].
Wu, Zhimin ;
Liu, Weiqing ;
Wang, Lu ;
Fang, Hai ;
Hui, David .
COMPOSITES PART B-ENGINEERING, 2014, 60 :329-340
[29]   Study on impact properties of through-thickness stitched foam sandwich composites [J].
Xia Fan ;
Wu Xiao-Qing .
COMPOSITE STRUCTURES, 2010, 92 (02) :412-421
[30]   Scaling effects in the low velocity impact response of sandwich structures [J].
Yang, F. J. ;
Hassan, M. Z. ;
Cantwell, W. J. ;
Jones, N. .
COMPOSITE STRUCTURES, 2013, 99 :97-104