Numerical simulation of hypervelocity impacts of a projectile on laminated composite plate targets by means of improved SPH method

被引:59
作者
Shintate, K
Sekine, H
机构
[1] Tohoku Univ, Dept Aeronaut & Space Engn, Aoba Ku, Sendai, Miyagi 9808579, Japan
[2] Japan Aerosp Explorat Agcy, Tsukuba Space Ctr, Tsukuba, Ibaraki 3058505, Japan
关键词
polymer-matrix composite (PMCs); impact behaviour; numerical analysis improved smoothed particle hydrodynamics method;
D O I
10.1016/j.compositesa.2004.02.011
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper is concerned with the numerical simulation of hypervelocity impacts (HVIs) of a projectile on laminated composite plate targets. When the numerical simulation of HVIs is performed by means of a conventional smoothed particle hydrodynamics (SPH) method, loss of interactions among particles causes numerical fractures. To prevent the numerical fractures, the improved SPH method with new particle generation and particle merger techniques is used. For the laminated composite plate targets of weak delamination strength, a numerical laminated plate model for the SPH method is proposed to realize the discontinuity of stresses between neighboring layers of the laminated composite plate targets. The numerical simulation was carried out for an aluminum projectile striking to laminated graphite/epoxy (Gr/Ep) composite plate targets with several different layup configurations. Through the numerical simulation, the HVI responses of the projectile on the laminated composite plate targets are discussed. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:683 / 692
页数:10
相关论文
共 19 条
[1]   Numerical simulation of rod particles hypervelocity impact effectiveness at various attack angles [J].
Bashurov, VV ;
Bebenin, GV ;
Ioilev, AG .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1997, 20 (1-5) :79-88
[2]   SIMULATIONS OF BRITTLE SOLIDS USING SMOOTH PARTICLE HYDRODYNAMICS [J].
BENZ, W ;
ASPHAUG, E .
COMPUTER PHYSICS COMMUNICATIONS, 1995, 87 (1-2) :253-265
[3]   High-velocity impact of graphite/epoxy composite laminates [J].
Chen, JK ;
Allahdadi, FA ;
Carney, TC .
COMPOSITES SCIENCE AND TECHNOLOGY, 1997, 57 (9-10) :1369-1379
[4]   The effects of projectile shape on laminated composite perforation [J].
Chen, JK ;
Medina, DF .
COMPOSITES SCIENCE AND TECHNOLOGY, 1998, 58 (10) :1629-1639
[5]  
Hayhurst CJ, 1997, INT J IMPACT ENG, V20, P337
[6]   Computational simulation of the hypervelocity impact of Al-spheres on thin plates of different materials [J].
Hiermaier, S ;
Konke, D ;
Stilp, AJ ;
Thoma, K .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1997, 20 (1-5) :363-374
[7]   INCORPORATION OF AN SPH OPTION INTO THE EPIC CODE FOR A WIDE-RANGE OF HIGH-VELOCITY IMPACT COMPUTATIONS [J].
JOHNSON, GR ;
PETERSEN, EH ;
STRYK, RA .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1993, 14 (1-4) :385-394
[8]  
JOHNSON GR, 1985, J ENG FRACT MECH, V21, P1
[9]   A numerical simulation method and its validation for debris impact against the whipple bumper shield [J].
Katayama, M ;
Kibe, S ;
Toda, S .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1995, 17 (4-6) :465-476
[10]   Normal and oblique hypervelocity impacts on carbon fibre/peek composites [J].
Lamontage, CG ;
Manuelpillai, GN ;
Taylor, EA ;
Tennyson, RC .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1999, 23 (01) :519-532