RESIDUAL STRENGTH OF COMPOSITES WITH MULTIPLE IMPACT DAMAGE

被引：8
作者：
JONES, R
机构：
[1] Department of Mechanical Engineering, Monash University, Clayton, Vic. 3168, Wellington Road
来源：
COMPOSITE STRUCTURES | 1994年 / 28卷 / 04期
关键词：
D O I：
10.1016/0263-8223(94)90117-1
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
In recent years attention has focused on damage interaction, with particular emphasis on multi-site damage. Whilst most attention has focused on fuselage lap joints, related problems occur in composite structures which are subjected to multiple impact damage. This paper reveals that for composites there is little interaction between damaged regions, provided they are separated by more than one diameter. This methodology was verified via a coupon test program and an experimental evaluation of two damaged F/A-18 horizontal stabilators.
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页码：347 / 356
页数：10
相关论文
共 31 条
[11]  
JONES R, 1988, J THEORET APPL FRACT, V9, P83
[12]  
JONES R, 1992, S STRUCTURAL INTEGRI
[13]  
JONES R, 1991, STRUCTURAL INTEGRITY, P199
[14]  
Jones Robert B., 1988, COMPOSITE MATERIALS, P49
[15]  
KURACHI EA, 1986, 31ST NAT SAMPL S EXH
[16]   ENVIRONMENTAL EVALUATION OF REPAIRS TO FUSELAGE LAP JOINTS [J].
MOLENT, L ;
BRIDGFORD, N ;
REES, D ;
JONES, R .
COMPOSITE STRUCTURES, 1992, 21 (02) :121-130
[17]   REPAIR OF IMPACT DAMAGED COMPOSITES [J].
PAUL, J ;
JONES, R .
ENGINEERING FRACTURE MECHANICS, 1992, 41 (01) :127-&
[18]  
PAUL J, 1909, 503 AER RES LAB AIRC
[19]  
PAUL J, 1989, 510 AER RES LAB AIRC
[20]  
PAUL J, 1991, P INT C AIRCRAFT DAM, P39
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