TY - JOUR
T1 - Estimation of fretting fatigue lifetime in heterogeneous material based on microstructure characterization and multi-scale homogenization
AU - Wang, Can
AU - Zinovev, Aleksandr
AU - Terentyev, Dmitry
AU - Wang, Dadang
AU - Abdel Wahab, Magd
N1 - Score=10
Funding Information:
The authors would like to acknowledge the financial support of the grants from the China Scholarship Council (202008130124), and National Natural Science Foundation of China (Grant Nos. 52175205 and 51975510). The authors would like to thank FOD and EURO fusion project (grant number 101052200) for the financial support provided for the project ‘Fatigue damage in fusion and GEN IV reactor steels: FEM modelling and experimental study’.
Publisher Copyright:
© 2023 Elsevier Ltd
PY - 2023/8
Y1 - 2023/8
N2 - Fretting fatigue is a complex phenomenon that is affected by multiaxial stress and contact problems. In the contact surface, due to the cyclic load, a relatively small displacement is generated, and the stress concentration is established as well. To assess the fretting fatigue endurance complimentary to experimental efforts, the Finite Element Method (FEM) has become a useful tool combined with theoretical approaches. Meanwhile, most (if not all) of commercially available structural materials can be regarded as heterogeneous materials due to the existence of secondary phases and some fabrication defects and porosity. Therefore, to further understand the mechanism of fretting fatigue, knowledge of the material’s microstructure is important. In this study, several microstructure characterization techniques are applied to characterize precipitates and micro-voids in aluminium alloy AA2024-T3. These techniques are Transmission Electron Microscopy (TEM) and Energy Dispersive Spectroscopy (EDS). To account for the precipitates, the homogenization method is adopted in this study. Additionally, a 3D structure non-destructive reconstruction technique is applied to obtain accurate information on micro-voids. The fretting fatigue lifetime is estimated by using the critical plane approach combined with the theory of critical distance. The numerical results are compared with experimental data showing a good agreement. The influence of micro-voids on the fretting fatigue endurance is studied and discussed as well.
AB - Fretting fatigue is a complex phenomenon that is affected by multiaxial stress and contact problems. In the contact surface, due to the cyclic load, a relatively small displacement is generated, and the stress concentration is established as well. To assess the fretting fatigue endurance complimentary to experimental efforts, the Finite Element Method (FEM) has become a useful tool combined with theoretical approaches. Meanwhile, most (if not all) of commercially available structural materials can be regarded as heterogeneous materials due to the existence of secondary phases and some fabrication defects and porosity. Therefore, to further understand the mechanism of fretting fatigue, knowledge of the material’s microstructure is important. In this study, several microstructure characterization techniques are applied to characterize precipitates and micro-voids in aluminium alloy AA2024-T3. These techniques are Transmission Electron Microscopy (TEM) and Energy Dispersive Spectroscopy (EDS). To account for the precipitates, the homogenization method is adopted in this study. Additionally, a 3D structure non-destructive reconstruction technique is applied to obtain accurate information on micro-voids. The fretting fatigue lifetime is estimated by using the critical plane approach combined with the theory of critical distance. The numerical results are compared with experimental data showing a good agreement. The influence of micro-voids on the fretting fatigue endurance is studied and discussed as well.
KW - Fretting fatigue
KW - Heterogeneous
KW - Microstructure characterization
KW - Homogenization method
KW - Precipitates
KW - Micro-voids
KW - TCD method
UR - http://www.scopus.com/inward/record.url?scp=85161287884&partnerID=8YFLogxK
U2 - 10.1016/j.tafmec.2023.103949
DO - 10.1016/j.tafmec.2023.103949
M3 - Article
SN - 0167-8442
VL - 126
JO - Theoretical and Applied Fracture Mechanics
JF - Theoretical and Applied Fracture Mechanics
M1 - 103949
ER -