Study on ballistic energy absorption of laminated and sandwich composites

被引:2
作者
Cui, XD [1 ]
Zeng, T [1 ]
Fang, DN [1 ]
机构
[1] Tsinghua Univ, Dept Mech Engn, Beijing 100084, Peoples R China
来源
FRACTURE AND STRENGTH OF SOLIDS VI, PTS 1 AND 2 | 2006年 / 306-308卷
关键词
ballistic impact; energy absorbing mechanisms; laminated composites; sandwich composite;
D O I
10.4028/www.scientific.net/KEM.306-308.739
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The impact response and energy absorbing characteristics of laminated, foam sandwich and honeycomb sandwich composites under ballistic impact have been studied in this investigation. An improved model is proposed in this paper to predict the ballistic property of the laminated composites. In this model, the material structures related to fiber lamination angles are designed in terms of their anti-impacting energy absorption capability. The ballistic limit speed and energy absorption per unit thickness of the three composites under different conditions are calculated. It is shown that honeycomb sandwich composite has the best ballistic resistance capability and energy absorption property among the three composites.
引用
收藏
页码:739 / 744
页数:6
相关论文
共 18 条
[11]  
JENQ ST, 1998, KEY ENG MATER, P141
[12]   Modelling of the energy absorption by polymer composites upon ballistic impact [J].
Morye, SS ;
Hine, PJ ;
Duckett, RA ;
Carr, DJ ;
Ward, IM .
COMPOSITES SCIENCE AND TECHNOLOGY, 2000, 60 (14) :2631-2642
[13]   AN ANALYTICAL MODEL TO PREDICT IMPACT BEHAVIOR OF SOFT ARMORS [J].
PARGALANDA, B ;
HERNANDEZOLIVARES, F .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1995, 16 (03) :455-466
[14]   Prediction of impact induced penetration and delamination in thick composite laminates [J].
Potti, SV ;
Sun, CT .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1997, 19 (01) :31-48
[15]   Penetration and perforation of composite sandwich panels by hemispherical and conical projectiles [J].
Reddy, TY ;
Wen, HM ;
Reid, SR ;
Soden, PD .
JOURNAL OF PRESSURE VESSEL TECHNOLOGY-TRANSACTIONS OF THE ASME, 1998, 120 (02) :186-194
[16]   A simple model to predict residual velocities of thick composite laminates subjected to high velocity impact [J].
Sun, CT ;
Potti, SV .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1996, 18 (03) :339-353
[17]   Penetration and perforation of thick FRP laminates [J].
Wen, HM .
COMPOSITES SCIENCE AND TECHNOLOGY, 2001, 61 (08) :1163-1172
[18]  
WOODWARD RL, 1988, INT J IMPACT ENG, V23, P117