Article ID Journal Published Year Pages File Type
768871 Engineering Failure Analysis 2011 9 Pages PDF
Abstract

Creep–fatigue crack growth behaviour of a nickel-based powder metallurgy superalloy has been investigated. Experiments were conducted at 750 °C with various dwell times. Results show that dwell time induced creep damage is significant by transforming a transgranular dominating cracking mode into a completely intergranular one. The observed dependence of crack growth rate on the dwell time and ΔK is complex indicating that the interaction between creep and fatigue is significant. Therefore, a factor reflecting the degree of the interaction was proposed to help modelling the creep–fatigue crack growth rates. The results are encouraging.

Related Topics
Physical Sciences and Engineering Engineering Industrial and Manufacturing Engineering
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