affiliation not provided to SSRN
Keywords: aerospace engineering, high pressure turbine, Inconel 718, fatigue crack growth, finite element method, electrical discharge machining, remaining life assessment
Ti-6Al-4V alloy, hip implant, Fatigue crack growth, finite element method
Schmid factor, Frank-Read source, Hall-Petch effect, Critical Resolved Shear Stress (CRSS), Tanaka-Mura Model (TMM), Fatigue Crack Initiation (FCI).