Aug 2026· Applied Sciences· Vol 16, pp. 8206· 0 citations· 24 references
Abstract
Predicting the fatigue lives of high-performance alloys, specifically aluminum 7075-T6 and Inconel 718, is essential for ensuring structural integrity in applications such as aerospace and energy. While Poisson’s ratio is typically treated as a constant within fracture mechanics and finite element analysis, it has been found to vary significantly with increased temperatures and substantial amounts of plastic deformation. Variations in Poisson’s ratio can, therefore, have a significant impact on local stress fields around cracks and the behavior at crack tips. This study introduces a novel approach by systematically isolating the effects of varying Poisson’s ratios on fatigue life cycles, stress distributions, and fatigue crack growth using finite element analysis with the robust ANSYS SMART crack growth feature. The results indicate a stark difference in the effects of Poisson’s ratio on the fatigue life of aluminum 7075-T6 compared to Inconel 718. A strong negative correlation exists between Poisson’s ratio and fatigue life cycle numbers for aluminum 7075-T6, whereas a more linear trend is observed for all fatigue life cycle numbers of Inconel 718. The underlying reasons for these trends lie in the differing sensitivities of elastic, shear, and bulk moduli between the two alloys. Overall, a higher Poisson’s ratio intensifies the maximum principal stress for both alloys. Additionally, an increase in Poisson’s ratio leads to a decrease in von Mises stress for both metals. Furthermore, these numerical results demonstrate that an increase in Poisson’s ratio corresponds to a decrease in the cyclic plastic zone size at the crack tip for both alloys, indicating enhanced hydrostatic constraint and reduced shear deformation. The findings presented herein underscore the necessity of eliminating the use of static values for Poisson’s ratio when evaluating the structural performance of high-performance alloys under extreme operational environments. Additionally, this research highlights several key areas where existing modeling approaches are lacking and establishes a framework for developing improved constitutive models for fatigue life prediction.
ABSTRACT This study presents a detailed technical analysis of the influence of strain rate and temperature on the microstructure and mechanical properties of the Ti 6Al 4V alloy during forging. As a process governed by compressive forces, forging involves critical parameters such as temperature, strain rate, friction a...
João Victor Do Carmo, A. D. da Silva, F. Cangue et al.· Matéria· 0 citations
This study uses a fracture mechanics-based method to assess fatigue crack growth life, using numerical simulations done with finite element analysis (FEA). We did a step-by-step check to assess how several key parameters—namely, load amplitude, stress ratio, the Paris law constants C and m, and initial crack size—affec...
In this study, the fatigue life prediction simulation of Chen et al. for TC4 titanium alloy components with surface defects is reconstructed and validated. When a scratch defect with a depth of 0.25 mm is introduced into the simulation, stress concentration occurs at the scratch root, and the predicted fatigue life rea...
T. Lê, Le Minh Duc, H. T. Nguyen· Journal of Science and Trans...· 0 citations
Compliant mechanisms, which derive motion through the elastic deformation of flexible members, offer distinct advantages over traditional mechanisms, including reduced part count, enhanced reliability, and smooth, frictionless operation. However, their fatigue life is a critical design concern due to the continuous cyc...
S. Solepatil, N. Deore· ITEGAM- Journal of Engineeri...· 0 citations
The long‑term performance and structural integrity of steam‑turbine discs are strongly influenced by crack‑growth behavior under combined thermal stresses and mechanical loading. In this study, a comprehensive analytical framework based on finite element analysis (FEA), mixed‑mode fracture‑mechanics evaluation (Modes I...
Mohammad Farahi, Arina Agharafiee, A. Ebrahimi et al.· Journal of Modern Mechanical...· 0 citations