Mode I Fatigue of Fibre Reinforced Polymeric Composites: A Review

• Published in: Polymers Vol. 14; no. 21; p. 4558
• Main Authors: Gao, Xingzhong, Umair, Muhammad, Nawab, Yasir, Latif, Zeeshan, Ahmad, Sheraz, Siddique, Amna, Yang, Hongyue
• Format: Journal Article
• Language: English
• Published: Basel MDPI AG 27.10.2022; MDPI
• Subjects: Analysis; Carbon; Composite materials; Crack propagation; Cracks; Cyclic loads; Dissimilar materials; Failure analysis; Fatigue; Fatigue failure; Fatigue testing machines; Fatigue tests; Fiber composites; Gas turbine engines; Laminated materials; Laminates; Life prediction; Materials; Mechanical properties; Numerical methods; Preforms; Review; Service life; Stress concentration; Yang Mu
• ISSN: 2073-4360; 2073-4360
• DOI: 10.3390/polym14214558

Composites are macroscopic combinations of chemically dissimilar materials preferred for new high-tech applications where mechanical performance is an area of interest. Mechanical apprehensions chiefly include tensile, creep, and fatigue loadings; each loading comprises different modes. Fatigue is cyclic loading correlated with stress amplitude and the number of cycles while defining the performance of a material. Composite materials are subject to various modes of fatigue loading during service life. Such loadings cause micro invisible to severe visible damage affecting the material’s performance. Mode I fatigue crack propagates via opening lamina governing a visible tear. Recently, there has been an increasing concern about finding new ways to reduce delamination failure, a life-reducing aspect of composites. This review focuses on mode I fatigue behaviours of various preforms and factors determining failures considering different reinforcements with respect to fibres and matrix failures. Numerical modelling methods for life prediction of composites while subjected to fatigue loading are reviewed. Testing techniques used to verify the fatigue performance of composite under mode I load are also given. Approaches for composites’ life enhancement against mode I fatigue loading have also been summarized, which could aid in developing a well-rounded understanding of mode I fatigue behaviours of composites and thus help engineers to design composites with higher interlaminar strength.