An enhanced fatigue damage model based on strength degradation of composite materials

An enhanced nonlinear fatigue damage cumulative model proposed is based on the strength degradation characteristics of composites, aiming to investigate damage progression under fatigue loading. Building upon this foundation, given the assumption of a linear correlation between fatigue cumulative da...

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Veröffentlicht in:Fatigue & fracture of engineering materials & structures 2024-11, Vol.47 (11), p.4012-4029
Hauptverfasser: Liu, Sanxing, Liu, Zhi, Zhou, Kai, Liu, Ying, Xiong, Xingjia, Liao, Tao, Ye, Nanhai
Format: Artikel
Sprache:eng
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Zusammenfassung:An enhanced nonlinear fatigue damage cumulative model proposed is based on the strength degradation characteristics of composites, aiming to investigate damage progression under fatigue loading. Building upon this foundation, given the assumption of a linear correlation between fatigue cumulative damage and stress level, a methodology is presented for extrapolating the damage curve of untested stress levels from that of tested stress levels. The model substantiates its reliability by validating against experimental data from several distinct material types. The reliability of the model has been validated using experimental data from multiple groups of materials. The experimental results indicate that the model can effectively reflect the fatigue damage development characteristics of composite materials. Simultaneously, the predicted stress levels derived from the proposed methodology show lesser deviation from the fitted data. Finally, a life prediction method founded on the proposed model is introduced, validated for its high prediction accuracy through experimentation. Highlights An enhanced fatigue damage model of composites is established. A novel residual strength model for composites has been established. Present a methodology for calculating the stress level damage curve. The fatigue life prediction method of the proposed model is developed.
ISSN:8756-758X
1460-2695
DOI:10.1111/ffe.14418