Fatigue crack propagation behavior of IN718 superalloy aged with temperature/stress coupled field
Source abstract
Abstract
Abstract Fatigue crack propagation behavior of IN718 superalloy aged with or without stress was investigated. The alloy aged with stress exhibited a higher fatigue crack growth rate and a lower fatigue threshold compared to that without stress. Both the restricted dislocation planar slip and the decreased difference in orientation of the activated slip system between adjacent grains were promoted by coarse γ″ phases, which increased the local plastic deformation and reduced the crack deflection. The accelerated coarse γ″ phase caused by applied stress was the key factor for the degradation of fatigue crack propagation resistance of the alloy aged with stress.
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Research context
OpenAlex topics: High Temperature Alloys and Creep · Fatigue and fracture mechanics · Aluminum Alloy Microstructure Properties
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
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