TY - JOUR
T1 - A new progressive fatigue damage model for the three-dimensional braided composites subjected to locally-variable-amplitude loading
AU - Ge, Jingran
AU - Liu, Zengfei
AU - Hu, Xinyu
AU - Liu, Xiaodong
AU - Li, Bingyao
AU - He, Chunwang
AU - Liang, Jun
N1 - Publisher Copyright:
© 2024 Elsevier Ltd
PY - 2024/7
Y1 - 2024/7
N2 - The fatigue-induced stress redistribution in three-dimensional (3D) braided composites, even when subjected to externally constant-amplitude fatigue loads, results in locally-variable-amplitude fatigue loading, significantly impacting their fatigue performance degradation. This paper is aimed to propose a novel fatigue damage analysis method to predict the fatigue behavior of 3D braided composites subjected to locally-variable-amplitude loading. To this end, the continuous damage method, residual strength, residual stiffness, and fatigue life models are combined to characterize the properties degradation of 3D braided composites with cycling. Once stress redistribution occurs, the fatigue properties degrade based on the new stress level, and the equivalent cycle number is recalculated accordingly. As the material undergoes different cycle blocks, damage accumulates, ultimately leading to failure when the overall stiffness of the material degrades to 80%. Traditional fatigue models are also employed to predict the fatigue behavior of representative volume elements for comparison. The results predicted by the present model shows good agreement with experiments. Furthermore, the influence of stress levels and architectures of 3D braided composites on fatigue performance is systematically discussed.
AB - The fatigue-induced stress redistribution in three-dimensional (3D) braided composites, even when subjected to externally constant-amplitude fatigue loads, results in locally-variable-amplitude fatigue loading, significantly impacting their fatigue performance degradation. This paper is aimed to propose a novel fatigue damage analysis method to predict the fatigue behavior of 3D braided composites subjected to locally-variable-amplitude loading. To this end, the continuous damage method, residual strength, residual stiffness, and fatigue life models are combined to characterize the properties degradation of 3D braided composites with cycling. Once stress redistribution occurs, the fatigue properties degrade based on the new stress level, and the equivalent cycle number is recalculated accordingly. As the material undergoes different cycle blocks, damage accumulates, ultimately leading to failure when the overall stiffness of the material degrades to 80%. Traditional fatigue models are also employed to predict the fatigue behavior of representative volume elements for comparison. The results predicted by the present model shows good agreement with experiments. Furthermore, the influence of stress levels and architectures of 3D braided composites on fatigue performance is systematically discussed.
KW - 3D braided composite
KW - Architecture
KW - Carbon fiber
KW - Fatigue damage analysis
KW - Locally-variable-amplitude
UR - http://www.scopus.com/inward/record.url?scp=85189860571&partnerID=8YFLogxK
U2 - 10.1016/j.ijfatigue.2024.108313
DO - 10.1016/j.ijfatigue.2024.108313
M3 - Article
AN - SCOPUS:85189860571
SN - 0142-1123
VL - 184
JO - International Journal of Fatigue
JF - International Journal of Fatigue
M1 - 108313
ER -