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[11] .Dang L, He X, Tang D, et al. A fatigue life posterior analysis approach for laser-directed energy deposition Ti-6Al-4V alloy based on pore-induced failures by kernel ridge [J]. Engineering Fracture Mechanics, 2023, 289: 109433.
[12] .He X, Dong Y, Yang B, et al. A wide range stress intensity factor solution for an eccentrically cracked middle tension specimen with clamped ends [J]. Engineering Fracture Mechanics, 2018, 191: 461-75.
[13] .He X, Dong Y, Sui F, et al. Fleet economic life prediction: A probabilistic approach including load spectrum variation and structural property variation [J]. Engineering Fracture Mechanics, 2016, 163: 189-205.
[14] .He X, Tan M, Xing J T. An investigation on fatigue crack growth rates through a designed nonsymmetric crack growth test [J]. Engineering Fracture Mechanics, 2012, 96: 510-27.
[15] .Tang D, He X, Wu B, et al. The effect of porosity defects on the mid-cycle fatigue behavior of directed energy deposited Ti-6Al-4V [J]. Theoretical and Applied Fracture Mechanics, 2022, 119: 103322.
[16] .Wang T, He X, Wang J, et al. Detail fatigue rating method based on bimodal Weibull distribution for DED Ti-6.5Al-2Zr-1Mo-1V titanium alloy [J]. Chinese Journal of Aeronautics, 2022, 35(4): 281-91.
[17] .Jiao R, He X, Li Y. Individual aircraft life monitoring: An engineering approach for fatigue damage evaluation [J]. Chinese Journal of Aeronautics, 2018, 31(4): 727-39.
[18] .He X, Wang T, Wang X, et al. Fatigue behavior of direct laser deposited Ti-6.5Al-2Zr-1Mo-1V titanium alloy and its life distribution model [J]. Chinese Journal of Aeronautics, 2018, 31(11): 2124-35.
[19] .Wang T, He X, Wang X, et al. P-S-N Curve Description of Laser Metal Deposition Ti-6.5Al-2Zr-1Mo-1V Titanium Alloy after Duplex Annealing [J]. Materials, 2019, 12(3): 418.
[20] .He X, Sui F, Zhai B, et al. Probabilistic and testing analysis for the variability of load spectrum damage in a fleet [J]. Engineering Failure Analysis, 2013, 33: 419-29.

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