“…Unfortunately, the literature on the relationship between the fatigue crack propagation behavior and grain size remains controversial, especially regarding that of alloys with multilevel microstructures. [1][2][3][4][5][6][7][8][9][10] For instance, Kang et al believe that refining grains can improve the fatigue crack propagation resistance of low-carbon martensitic Nomenclature: a, crack length; ASTM, American Society for Testing and Materials; B, thickness of compact tension specimen; C, material constant; CTOD, crack tip opening displacement; d, grain size; da/dN, fatigue crack propagation rate; db, martensitic block size; dl, martensitic lath width; dp, martensitic packet size; E, elastic modulus; EBSD, electron backscattering diffraction; FCG, fatigue crack growth; HAGBs, high-angle boundaries; LAGBs, low-angle boundaries; LSCM, laser-scanning confocal microscopy; m, material constant; N, fatigue cycles number; OICC, oxide-induced crack closure; PICC, plasticity-induced crack closure; RCPZ, cyclic plastic zone size; RICC, roughness-induced crack closure; UTS, ultimate tensile strength; W, width of compact tension specimen; YS, yield strength; ΔK, stress intensity factor; ΔK th , fatigue crack threshold value; ΔP, applied load range; v, Poisson's ratio; σy, yield strength steel because as the frequency of cracks encountered with substructure boundaries increased, the crack growth would be hindered, slowing the crack propagation rate. 1 Guo Ping and Ma et al studied the fatigue crack propagation behavior of the TC4 alloy and found that α lamellae have the strongest influence on the fatigue crack propagation rate in the near-threshold region as well as further refinement of the α lamellae improved the crack growth resistance.…”