Composite adhesive joints under cyclic loading

被引:55
作者
de Goeij, WC [1 ]
van Tooren, MJL [1 ]
Beukers, A [1 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Sect Prod Technol, NL-2600 GB Delft, Netherlands
关键词
composite; joint; adhesive; fatigue;
D O I
10.1016/S0261-3069(99)00032-1
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
With the increasing use of adhesive bonding in structural joints in many applications, the interest in the behaviour of adhesive joints under cyclic loading has increased as well. Much work has already been performed on the analysis of adhesively bonded joints under static loading. Also the damage growth and failure mechanisms of adhesive joints under cyclic loading has been investigated, to a less extent for joints in composite structures. A major difficulty is the large amount of parameters that can be of influence on crack initiation and growth in adhesive joints. This makes it hard to characterise the debond behaviour of a joint. This article is intended to give an overview of studies performed on adhesive composite joints under cyclic loading on and to serve as a starting point for designers who need information on experimental and analytical methods of composite adhesive joints. (C) 1999 Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:213 / 221
页数:9
相关论文
共 34 条
[1]  
ALLEN RC, 1986, I MECH ENG C PUBLICA, V6, P169
[2]  
BACH PW, 1988, 8878 ECN, P26
[3]   EFFECT OF TEMPERATURE ON ADHESIVE FRACTURE BEHAVIOR OF AN ELASTOMER EPOXY RESIN [J].
BASCOM, WD ;
COTTINGTON, RL .
JOURNAL OF ADHESION, 1976, 7 (04) :333-346
[4]  
CLARKE JD, 1986, I MECH ENG C PUBLICA, V6, P113
[5]  
DENOUDEN G, 1991, METAALKUNDE 1
[6]  
GILMORE RB, 1994, COMPOSITE BONDING AS, V1227, P82
[7]  
HUNSTON DL, 1984, ADHESIVE JOINTS, P789
[8]   FATIGUE CRACK-GROWTH IN STRUCTURAL ADHESIVES [J].
JABLONSKI, DA .
JOURNAL OF ADHESION, 1980, 11 (02) :125-143
[9]  
Johnson W., 1985, ASTM STP, V876, P189
[10]  
JOHNSON WS, J COMPOSITES TECHNOL, V8, P3