The blast resistance of sandwich composites with stepwise graded cores

被引:174
作者
Wang, Erheng [1 ]
Gardner, Nate [1 ]
Shukla, Arun [1 ]
机构
[1] Univ Rhode Isl, Dept Mech Engn & Appl Mech, Dynam Photomech Lab, Kingston, RI 02881 USA
关键词
Sandwich structures; Discretely layered core; Shock wave loading; Dynamic failure; High speed imaging; PLATES; PANELS; BEAMS;
D O I
10.1016/j.ijsolstr.2009.06.004
中图分类号
O3 [力学];
学科分类号
070301 [无机化学];
摘要
Shock tube experiments were performed to study the dynamic response of sandwich panels with E-Glass Vinyl Ester (EVE) composite face sheets and stepwise graded styrene foam cores. Two types of core configurations, with identical areal density, were subjected to the shock wave loading. The core layers were arranged according to the density of the respective foam; configuration 1 consisted of low/middle/high density foams and configuration 2 consisted of middle/low/high density foams. The method to calculate the incident and reflected energies of the shock wave, as well as the deformation energy of the specimen, were proposed based on the shock wave pressure profiles and the high speed deflection images that were obtained. The experimental results showed that configuration 1 outperformed configuration 2 in regards to their blast resistance. Significant core material compression was observed in configuration 1, while in configuration 2 the core layers disintegrated and the front skin (blast side) fractured into two pieces along the midsection. The estimated energies were then calculated for both configurations. The total energy difference between the incident and reflected energies was almost identical, even though the deformation energy for configuration 2 was larger. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:3492 / 3502
页数:11
相关论文
共 14 条
[1]
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
[2]
A split Hopkinson bar technique for low-impedance materials [J].
Chen, W ;
Zhang, B ;
Forrestal, MJ .
EXPERIMENTAL MECHANICS, 1999, 39 (02) :81-85
[3]
Courant R., 1999, Supersonic Flow and Shock Waves
[4]
Mechanical response of metallic honeycomb sandwich panel structures to high-intensity dynamic loading [J].
Dharmasena, Kumar P. ;
Wadley, Haydn N. G. ;
Xue, Zhenyu ;
Hutchinson, John W. .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2008, 35 (09) :1063-1074
[5]
The resistance of clamped sandwich beams to shock loading [J].
Fleck, NA ;
Deshpande, VS .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2004, 71 (03) :386-401
[6]
Li R.F., 2008, T ASME, V75, P125
[7]
Dynamic characterization of layered and graded structures under impulsive loading [J].
Li, Y ;
Ramesh, KT ;
Chin, ESC .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2001, 38 (34-35) :6045-6061
[8]
The response of clamped sandwich plates with lattice cores subjected to shock loading [J].
McShane, GJ ;
Radford, DD ;
Deshpande, VS ;
Fleck, NA .
EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2006, 25 (02) :215-229
[9]
NURICK GN, 2009, EXPT COMPOS IN PRESS, DOI DOI 10.1016/J.COMPSTRUCT.2009.04.009
[10]
Shock loading response of sandwich panels with 3-D woven E-glass composite skins and stitched foam core [J].
Tekalur, Srinivasan Arjun ;
Bogdanovich, Alexander E. ;
Shukla, Arun .
COMPOSITES SCIENCE AND TECHNOLOGY, 2009, 69 (06) :736-753