Progressive failure analysis of pin-loaded laminated composites using penalty finite element method

被引:24
作者
Kim, SJ [1 ]
Hwang, JS
Kim, JH
机构
[1] Seoul Natl Univ, Dept Aerosp Engn, Seoul 151742, South Korea
[2] Korea Aerosp Res Inst, Taejon 305600, South Korea
关键词
D O I
10.2514/2.354
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A progressive failure analysis is carried out to predict the failure strengths and failure modes of pin-loaded laminated composite plates using the penalty finite element method. To consider contact condition in the pin hole interface, an exterior penalty method and the Coulomb friction law are used. Damage accumulations in the laminates are evaluated by using Hashin's failure criteria combined with the proposed property degradation model, Using a finite element code developed based on the present formulation, contact stresses are obtained and verified, Predictions of failure strengths and the failure modes compare well with available experimental data. Finally, a parametric study considering geometries and clearance is performed to identify the failure characteristics of the pin loaded laminated composite plate, The numerical results show the importance of geometric parameters and clearance on both the failure strengths and the failure modes.
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收藏
页码:75 / 80
页数:6
相关论文
共 27 条
[1]   STATIC STRENGTH PREDICTION OF BOLTED JOINT IN COMPOSITE-MATERIAL [J].
AGARWAL, BL .
AIAA JOURNAL, 1980, 18 (11) :1371-1375
[2]   A NUMERICAL-ANALYSIS OF A CLASS OF CONTACT PROBLEMS WITH FRICTION IN ELASTOSTATICS [J].
CAMPOS, LT ;
ODEN, JT ;
KIKUCHI, N .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1982, 34 (1-3) :821-845
[3]   POST-FAILURE ANALYSIS OF BOLTED COMPOSITE JOINTS IN TENSION OR SHEAR-OUT MODE FAILURE [J].
CHANG, FK ;
CHANG, KY .
JOURNAL OF COMPOSITE MATERIALS, 1987, 21 (09) :809-833
[4]   THE EFFECT OF PIN LOAD DISTRIBUTION ON THE STRENGTH OF PIN LOADED HOLES IN LAMINATED COMPOSITES [J].
CHANG, FK .
JOURNAL OF COMPOSITE MATERIALS, 1986, 20 (04) :401-408
[5]   DESIGN OF COMPOSITE LAMINATES CONTAINING PIN LOADED HOLES [J].
CHANG, FK ;
SCOTT, RA ;
SPRINGER, GS .
JOURNAL OF COMPOSITE MATERIALS, 1984, 18 (03) :279-289
[6]   FAILURE OF COMPOSITE LAMINATES CONTAINING PIN LOADED HOLES - METHOD OF SOLUTION [J].
CHANG, FK ;
SCOTT, RA ;
SPRINGER, GS .
JOURNAL OF COMPOSITE MATERIALS, 1984, 18 (03) :255-278
[7]  
De Jong T, 1982, LR350 TU DELFT
[8]  
Duvaut G., 1976, GRUNDLEHREN MATH WIS, DOI 10.1007/978-3-642-66165-5
[9]   FAILURE CRITERIA FOR UNIDIRECTIONAL FIBER COMPOSITES [J].
HASHIN, Z .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1980, 47 (02) :329-334
[10]   THE EFFECTS OF PIN ELASTICITY, CLEARANCE, AND FRICTION ON THE STRESSES IN A PIN-LOADED ORTHOTROPIC PLATE [J].
HYER, MW ;
KLANG, EC ;
COOPER, DE .
JOURNAL OF COMPOSITE MATERIALS, 1987, 21 (03) :190-206