The impact response of graded foam sandwich structures

被引:113
作者
Zhou, J. [1 ]
Guan, Z. W. [1 ]
Cantwell, W. J. [2 ]
机构
[1] Univ Liverpool, Sch Engn, Liverpool L69 3GH, Merseyside, England
[2] KUSTAR, Dept Aerosp Engn, Abu Dhabi, U Arab Emirates
关键词
Graded foam; Perforation; Finite element; Impact; Progressive failure; Sandwich; LOW-VELOCITY IMPACT; CORE; PANELS; FAILURE; BEAMS; PERFORATION; BEHAVIOR;
D O I
10.1016/j.compstruct.2012.10.037
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Low velocity impact tests have been undertaken on sandwich structures based on cores fabricated by bonding foams of different densities together. Here, a range of linear PVC, crosslinked PVC and PEI foams were bonded together to produce a three layer core. Carbon fibre skins were then bonded to the core and the structures were loaded by a drop-weight impact carriage with a hemispherical head. It has been observed that the majority of the panels failed in a through-thickness shearing mode, leaving a clear cylindrical hole in the multi-layered core. A limited number of structures also exhibited cone cracking on the exit surface, due to failure in a mixed tensile/shear mode. The impact response of the graded sandwich structures was modelled by finite element analysis and the predicted load displacement responses and failure modes compared. Agreement between the FE model and the experimental data was good across the range of structures investigated, with the model accurately predicting the impact responses and failure characteristics observed within the panels. It has also been shown that graded core structures can out-perform their monolithic counterparts. Finally when normalised by their unit cost, significant differences in the perforation resistances of the structures have been observed. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:370 / 377
页数:8
相关论文
共 19 条
[1]  
ABAQUS, 2010, THEOR MAN VERS 6 9
[2]   An elasticity-equilibrium-based zigzag theory for axisymmetric bending and stress analysis of the functionally graded circular sandwich plates, using a Maclaurin-type series solution [J].
Alipour, M. M. ;
Shariyat, M. .
EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2012, 34 :78-101
[3]   Low-velocity impact response of sandwich beams with functionally graded core [J].
Apetre, NA ;
Sankar, BV ;
Ambur, DR .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2006, 43 (09) :2479-2496
[4]   Failure mode investigation of sandwich beams with functionally graded core [J].
Avila, Antonio F. .
COMPOSITE STRUCTURES, 2007, 81 (03) :323-330
[5]   Modelling of composite sandwich structures with honeycomb core subjected to high-velocity impact [J].
Buitrago, Brenda L. ;
Santiuste, Carlos ;
Sanchez-Saez, Sonia ;
Barbero, Enrique ;
Navarro, Carlos .
COMPOSITE STRUCTURES, 2010, 92 (09) :2090-2096
[6]   Designing the energy absorption capacity of functionally graded foam materials [J].
Cui, Liang ;
Kiernan, Stephen ;
Gilchrist, Michael D. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2009, 507 (1-2) :215-225
[7]   Multi-axial yield behaviour of polymer foams [J].
Deshpande, VS ;
Fleck, NA .
ACTA MATERIALIA, 2001, 49 (10) :1859-1866
[8]   3D finite element simulation of sandwich panels with a functionally graded core subjected to low velocity impact [J].
Etemadi, E. ;
Khatibi, A. Afaghi ;
Takaffoli, M. .
COMPOSITE STRUCTURES, 2009, 89 (01) :28-34
[9]   Numerical modelling of perforation failure in fibre metal laminates subjected to low velocity impact loading [J].
Fan, J. ;
Guan, Z. W. ;
Cantwell, W. J. .
COMPOSITE STRUCTURES, 2011, 93 (09) :2430-2436
[10]   Performance of functionally graded sandwich composite beams under shock wave loading [J].
Gardner, Nate ;
Wang, Erheng ;
Shukla, Arun .
COMPOSITE STRUCTURES, 2012, 94 (05) :1755-1770