| Citation: | CAO Duanxing, YANG Yang, CHEN Xinwen, et al. A fatigue life prediction method for composite materials considering interlayer stress[J]. Journal of Aerospace Power, 2026, 41(2):20230644 doi: 10.13224/j.cnki.jasp.20230644 |
In response to the phenomenon that composite laminates are prone to delamination under fatigue load, which often starts from the edge, analytical methods were used to solve the interlayer stress of composite laminates and obtain the distribution of interlayer stress at each interface under tensile and bending loads. The concept of local average stress was proposed to process the interlayer stress near the free boundary. The improved Hashin delamination failure criterion was used as the delamination criterion to select the local average stress between dangerous layers, which was introduced into the composite Stress-Fatigue life N (Abbreviated as
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