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Article
Microstructural evolution of DS CM186LC during creep and thermal exposure
Thermal exposure tests were carried out at the same temperature and duration as those of creep tests. Growth of γ′ either in the matrix or in the interdendritic regions was observed during high temperature the...
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Article
High temperature mechanical properities and creep crack initiation of DS CM186LC for nozzle guide vane
The second generation DS alloy, CM186LC is used in the as-cast and double aged condition which has creep-rupture properities equivalent to the first generation single crystal alloys CMSX-2 and CMSX-3. In produ...
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Article
Quantitative models on corrosion fatigue crack growth rates in metals: Part II. application of fatigue crack growth rate modeling for nickel-based superalloys at elevated temperatures
Nickel-based superalloys exhibit sustained load crack growth at elevated temperatures, which significantly contributes to the total fatigue crack growth rate when Kmax is above the threshold value for sustained l...
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Article
Quantitative models on corrosion fatigue crack growth rates in metals: Part I. Overview of quantitative crack growth models
Approaches to predict da/dN-ÀK for environmental situations; including empirical interpolative equations, linear superposition of mechanical fatigue and time-based environmental cracking, and mechanism-based m...