Chun Hu, Xin Huang, Shaolin Li, Hongyu Qi, Xiaoguang Yang, Duoqi Shi
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引用次数: 0
Abstract
The high-temperature components of aeroengines operate under high-temperature and fatigue-loading conditions, resulting in complex crack-related issues. This study presents fatigue crack growth (FCG) experiments under mixed-mode loading performed on compact tension shear specimens fabricated from a nickel-based superalloy, tested at 550°C under varying thicknesses. The influence of specimen thickness on FCG behavior under mixed-mode loading was analyzed through experimental investigations and finite element method simulations. The expanded FCG model, incorporating thickness effects based on closure theory, enables more precise predictions of crack growth rates under mixed-mode loading conditions. Additionally, the FCG da/dN − ΔK curve for nickel-based superalloys exhibits a vertical shift with varying specimen thickness, while the FCG angle under mixed-mode loading remains unaffected by thickness. These findings provide valuable insights for improving damage tolerance design in aircraft engines.
期刊介绍:
Fatigue & Fracture of Engineering Materials & Structures (FFEMS) encompasses the broad topic of structural integrity which is founded on the mechanics of fatigue and fracture, and is concerned with the reliability and effectiveness of various materials and structural components of any scale or geometry. The editors publish original contributions that will stimulate the intellectual innovation that generates elegant, effective and economic engineering designs. The journal is interdisciplinary and includes papers from scientists and engineers in the fields of materials science, mechanics, physics, chemistry, etc.