Article ID Journal Published Year Pages File Type
7153623 Chinese Journal of Aeronautics 2018 11 Pages PDF
Abstract
This paper seeks to evaluate crack propagation properties and residual lives of metallic alloys subjected to fatigue loading at room and high temperatures. Fatigue crack growth tests were performed on Ti-6Al-4V/ELI and 7050-T7452 subjected to constant-amplitude and actual random-spectra loading at room temperature of about 25 °C and at high temperatures of 250 °C and 150 °C to determine their crack growth properties and residual lives. The damage mode and mechanisms at high temperature were compared with those at room temperature on the basis of the results of fractographic analysis. Temperature-dependent residual lives under actual random-spectra load history were evaluated based on a modified accumulation damage rule accounting for the load interaction. Good correlation was achieved between the predictions and actual experiments, demonstrating the practical and effective use of the proposed method.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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