Progressive Fatigue Damage Modeling of Cross-ply Laminates, I: Modeling Strategy

被引:36
作者
Shokrieh, M. M. [1 ]
Taheri-Behrooz, F. [1 ]
机构
[1] Iran Univ Sci & Technol, Composites Res Lab, Dept Mech Engn, Tehran 1684613114, Iran
关键词
progressive fatigue damage modeling; carbon/epoxy; cross-ply composites; stiffness degradation; strength degradation; CARBON-FIBER COMPOSITES; LIFE PREDICTION; TRANSVERSE CRACKING; FAILURE CRITERION; RESIDUAL STRENGTH; UNIAXIAL FATIGUE; BEHAVIOR; STRESS;
D O I
10.1177/0021998309351604
中图分类号
TB33 [复合材料];
学科分类号
摘要
The main goal of this research is the fatigue simulation of cross-ply laminates under cyclic tension-tension loading conditions. For this purpose, a progressive fatigue damage model is developed based on two main assumptions. First, it is assumed that off-axis plies are responsible for stress redistribution into the laminate. Second, on-axis plies are responsible for strength reduction and control failure of the laminate. Developed model is capable of predicting the fatigue life and residual strength of cross-ply laminates with a limited experimental data and acceptable accuracy. The results of the model are compared with the experimental data provided in the second part of the present article.
引用
收藏
页码:1217 / 1231
页数:15
相关论文
共 48 条
[1]  
Adam, 1992, ADV COMPOS LETT, V1, P23
[2]   LIFE PREDICTION FOR FATIGUE OF T800/5245 CARBON-FIBER COMPOSITES .2. VARIABLE-AMPLITUDE LOADING [J].
ADAM, T ;
GATHERCOLE, N ;
REITER, H ;
HARRIS, B .
INTERNATIONAL JOURNAL OF FATIGUE, 1994, 16 (08) :533-547
[3]   FATIGUE LIFE PREDICTION FOR HYBRID COMPOSITES [J].
ADAM, T ;
FERNANDO, GF ;
DICKSON, RF ;
REITER, H ;
HARRIS, B .
INTERNATIONAL JOURNAL OF FATIGUE, 1989, 11 (04) :233-237
[4]   A POWER LAW FATIGUE DAMAGE MODEL FOR FIBER-REINFORCED PLASTIC LAMINATES [J].
ADAM, T ;
DICKSON, RF ;
JONES, CJ ;
REITER, H ;
HARRIS, B .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 1986, 200 (03) :155-166
[5]  
[Anonymous], ASTM STP
[6]  
[Anonymous], ASTM STP
[7]  
[Anonymous], ASTM STP
[8]  
Berthelot J.-M., 2003, Applied Mechanics Review, V56, P111, DOI 10.1115/1.1519557
[9]   Modelling the transverse cracking in cross-ply laminates: application to fatigue [J].
Berthelot, JM ;
Le Corre, JF .
COMPOSITES PART B-ENGINEERING, 1999, 30 (06) :569-577
[10]  
Boller K.H., 1957, MOD PLAST, V34, P163