1. K.S. Li, L.Y. Cheng, Y. Xu, R.Z. Wang, Y. Zhang, X.C. Zhang, S.T. Tu, and H. Miura, A Dual-Scale Modelling Approach for Creep-Fatigue Crack Initiation Life Prediction of Holed Structure in a Nickel-Based Superalloy. Int. J. Fatigue (2022)
2. Z. Jin. Outline of Structural Integrity of Aero-Engine. Aviation Standardization and Quality, 1990(04):27-29.
3. Y.M. Xu, S.M. Zhang, T.P. He, X.L. Liu, and X.Y. Chang Prediction of Low-Cycle Crack Initiation Life of Superalloy FGH96 with Inclusion Powder Based on Damage Mechanics. Trans. Nonferrous Met. Soc. China 1–25 (2021)
4. K.S. Li, R.Z. Wang, G.J. Yuan, S.P. Zhu, X.C. Zhang, S.T. Tu, and H. Miura, A Crystal Plasticity-Based Approach for Creep-Fatigue Life Prediction and Damage Evaluation in a Nickel-Based Superalloy, Int. J. Fatigue, 2021, 143, p 106031.
5. L. Zhu, X. Hu, R. Jiang, Y. Song, and S. Qu. Experimental Investigation of Small Fatigue Crack Growth Due to Foreign Object Damage in Titanium Alloy TC4. Mater. Sci. Eng. A. (2019)