“…Nickel-based superalloys have been found the widespread use of the aeronautical and aerospace industry, [1][2][3] due to their excellent high-temperature strength, [4] fatigue capability, creep resistance, corrosion, and oxidation resistance. [5,6] For disk superalloys, Inconel 718, strengthened by the Ni 3 Nb phase known as gamma double prime (γ 00 ), is still widely used at temperature up to %650 C caused by the thermodynamically unstable γ 00 precipitate at higher temperatures. To meet the need of turbine disks in the next-generation engine, several novel superalloys have been developed in previous studies, such as Allvac 718Plus, [7] Udimet 720Li, [8,9] AD730, [10] FGH100L, [11] GH4151, [12] and GH4065.…”