Fatigue damage accumulation model and residual life prediction method of composite laminates based on strength degradation

被引:0
作者
Chen, Hao [1 ]
Liu, Sijin [2 ]
Yang, Bowen [1 ]
Han, Kaixuan [1 ]
Huo, Junzhou [1 ]
机构
[1] Dalian Univ Technol, Sch Mech Engn, Dalian 116024, Peoples R China
[2] China Railway 14th Bur Grp Corp Ltd, Jinan, Peoples R China
基金
中国国家自然科学基金;
关键词
composite laminates; variable amplitude loading; fatigue life prediction; residual intensity; loading interaction effect;
D O I
10.1177/02670836241308753
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper proposes a residual fatigue life prediction method that considers the loading interaction effect, to predict the fatigue life of composite laminates under variable amplitude loading. Based on the study of static mechanical and fatigue properties of composite laminates, the influence mechanism of the loading interaction effect on material fatigue life is analyzed, and an exponential function including adjacent load amplitudes and fatigue life is proposed as a parameter to describe the loading interaction effect. Then, an equation describing the damage evolution of composite laminates during fatigue is proposed. A simple prediction method for residual fatigue life under variable loading considering the loading interaction effect is proposed based on the damage equivalent theory. Finally, through experimental validation, it is found that the prediction error of the proposed model does not exceed 50%, which is lower than the other models mentioned in the paper.
引用
收藏
页数:12
相关论文
共 44 条
[1]   Fatigue life prediction for composite materials based on the S-N-f model [J].
An, Hai ;
Zhao, Weitao .
AIP ADVANCES, 2023, 13 (08)
[2]  
Basquin O.H., 1910, P ASTM, V10, P625, DOI DOI 10.4236/MSA.2011.212231
[3]   Cumulative Fatigue Damage of Composite Laminates: Engineering Rule and Life Prediction Aspect [J].
Batsoulas, Nikolaos D. ;
Giannopoulos, Georgios I. .
MATERIALS, 2023, 16 (08)
[4]   Effect of variable amplitude block loading on intralaminar crack initiation and propagation in multidirectional GFRP laminate [J].
Bender, J. J. ;
Bak, B. L. V. ;
Jensen, S. M. ;
Lindgaard, E. .
COMPOSITES PART B-ENGINEERING, 2021, 217
[5]   Numerical life prediction of unidirectional fiber composites under block loading conditions using a progressive fatigue damage model [J].
Brod, M. ;
Dean, A. ;
Rolfes, R. .
INTERNATIONAL JOURNAL OF FATIGUE, 2021, 147
[6]   Influence of distributed out-of-plane waviness defects on the mechanical behavior of CFRP laminates [J].
Calvo, Jose Vicente ;
Quinonero-Moya, Antonio Ramon ;
Feito, Norberto ;
Miguelez, Maria Henar ;
Giner, Eugenio .
COMPOSITE STRUCTURES, 2023, 323
[7]   A nonlinear fatigue damage accumulation model under variable amplitude loading considering the loading sequence effect [J].
Chen, Hao ;
Yang, Fan ;
Wu, Zhen ;
Yang, Bowen ;
Huo, Junzhou .
INTERNATIONAL JOURNAL OF FATIGUE, 2023, 177
[8]   Fatigue life predictions under variable amplitude loading for composite materials [J].
Duran, Jorge Alberto Rodriguez ;
Bermudez, Panters Rodriguez ;
Rodriguez-Ramos, Reinaldo .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART L-JOURNAL OF MATERIALS-DESIGN AND APPLICATIONS, 2024,
[9]   Estimation of remaining fatigue life with an energy-based model considering the effects of loading sequence and load interaction [J].
Gan, Lei ;
Wu, Hao ;
Zhong, Zheng .
INTERNATIONAL JOURNAL OF DAMAGE MECHANICS, 2023, 32 (03) :340-361
[10]   Strength and stiffness degradation modeling and fatigue life prediction of composite materials based on a unified fatigue damage model [J].
Gao, Jianxiong ;
Zhu, Pengnian ;
Yuan, Yiping ;
Wu, Zhifeng ;
Xu, Rongxia .
ENGINEERING FAILURE ANALYSIS, 2022, 137