Dynamic response of the S-shaped composite foldcore sandwich structure under high-velocity impact loads

被引:9
作者
Deng, Yunfei [1 ]
Tian, Rui [2 ]
Hu, Ang [2 ]
Jia, Huiru [3 ]
Yang, Yonggang [4 ]
机构
[1] Civil Aviat Univ China, Key Lab Civil Aviat Aircraft Airworthiness Certif, Tianjin, Peoples R China
[2] Civil Aviat Univ China, Coll Aeronaut Engn, Tianjin, Peoples R China
[3] Civil Aviat Univ China, Sino European Inst Aviat Engn, Tianjin, Peoples R China
[4] Civil Aviat Univ China, Coll Traff Sci & Technol, Tianjin, Peoples R China
关键词
S-shaped foldcore; sandwich structure; high-velocity impact; composite material; dynamic response; CORE STRUCTURES; BEHAVIOR; DAMAGE;
D O I
10.1080/15376494.2022.2053902
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The dynamic response of the S-shaped foldcore sandwich structure was investigated at high-velocity impact load by combining the experimental and numerical methods. The ballistic tests were performed with a blunt projectile at different velocities, ranging from 49.7 m/s to 154 m/s, and the ballistic limit velocity (BLV) was estimated. The test results show that the impact location exerted great influence on the failure modes and energy absorption of the core. The BLVs of the sandwich structure are 64.2 m/s and 56.2 m/s for node and base impacts, respectively. And the different modes are observed for the top face sheet, the core and the bottom face sheet. The corresponding numerical simulations were performed by using Abaqus finite element software. The simulation results show that the BLVs predicted by the simulation correlated well with the tests. The failure modes of the sandwich structures with fiber fracture, delamination and compression failure are predicted reasonably. For the node impact conditions, the absorbed energy of the core is significantly higher than that of the top and bottom face sheet. For the base impact conditions, there is no significant difference on the energy consumed for three components of the structures.
引用
收藏
页码:2240 / 2257
页数:18
相关论文
共 28 条
[1]  
[Anonymous], 2020, COMPOS PART A-APPL S, V139, P63
[2]   Modelling of the Behaviour of Aramid Folded Cores Up to Global Crushing [J].
Baranger, E. ;
Cluzel, C. ;
Guidault, P-A .
STRAIN, 2011, 47 :170-178
[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]  
[蔡克乾 Cai Keqian], 2015, [材料导报, Materials Review], V29, P129
[5]   The behaviour of curved-crease foldcores under low-velocity impact loads [J].
Gattas, J. M. ;
You, Z. .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2015, 53 :80-91
[6]   Miura-Base Rigid Origami: Parametrizations of Curved-Crease Geometries [J].
Gattas, Joseph M. ;
You, Zhong .
JOURNAL OF MECHANICAL DESIGN, 2014, 136 (12)
[7]   Experimental and numerical research on the low velocity impact behavior of hybrid corrugated core sandwich structures [J].
He, Wentao ;
Liu, Jingxi ;
Tao, Bo ;
Xie, De ;
Liu, Jiayi ;
Zhang, Min .
COMPOSITE STRUCTURES, 2016, 158 :30-43
[8]   Experimental and numerical analysis of composite folded sandwich core structures under compression [J].
Heimbs, S. ;
Middendorf, P. ;
Kilchert, S. ;
Johnson, A. F. ;
Maier, M. .
APPLIED COMPOSITE MATERIALS, 2007, 14 (5-6) :363-377
[9]   Sandwich structures with textile-reinforced composite foldcores under impact loads [J].
Heimbs, S. ;
Cichosz, J. ;
Klaus, M. ;
Kilchert, S. ;
Johnson, A. F. .
COMPOSITE STRUCTURES, 2010, 92 (06) :1485-1497
[10]   Sandwich structures technology in commercial aviation - Present applications and future trends [J].
Herrmann, AS ;
Zahlen, PC ;
Zuardy, I .
SANDWICH STRUCTURES7: ADVANCING WITH SANDWICH STRUCTURES AND MATERIALS, 2005, :13-26