Circular holes in single crystal (SX) turbine blades are susceptible to creep failure at high
temperatures, due to the stress concentrations near the holes. In this study, a dislocation …

In the framework of the unified elastic-plastic constitutive theory, the cyclic response and
damage evolution of 316H steel in the low cycle fatigue (LCF) regime was analyzed and …

Defects and microstructural inhomogeneity have been recognized to have a significant
impact on the fatigue performance of titanium alloys fabricated by laser powder bed fusion …

Gas turbine blades normally operate under high‐temperatures, extreme pressure, and high‐
speed conditions, which leads to complex failure mechanisms and difficulties in fatigue life …

Aiming at the creep-fatigue interaction damage failure problem of turbine blades in
aeronautical engineering, firstly, based on the modified Kachanov-Rabotnov-Chaboche …

Grain, grain boundaries, voids, alloying elements and other anomalies have an important
impact on the stress distribution at the sub-grain meso level which consequently affect the …

This paper develops a dual-threshold modelling approach to characterize fatigue
performance and predict the fatigue life of turbine blades and their alloys under combined …

The impact of crystal orientation on the elastic stress and vibration properties of nickel-based
single-crystal turbine blades is complex and can affect their performance. By defining and …

In this present work, a damage-coupled cyclic plasticity model has been developed for more
accurate ratcheting–fatigue life estimation under strain and stress controlled ratcheting …

This paper proposes a substructure-based distributed-collaborative surrogate modeling
approach for improving the accuracy and efficiency in the estimation of the creep-fatigue …