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This document presents a peridynamic model for simulating corrosion-fatigue failure behavior in aero-engine parts, which are significantly affected by environmental conditions. The model establishes a coupling between mechanical and chemical fields, and its validity is demonstrated through predictions of corrosion-fatigue crack growth in S355 steel and Ti-6Al-4V alloy samples. The results indicate that the model effectively captures the influence of corrosion on fatigue crack growth rates, providing a theor

Author
ltian9831
Language
EN

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