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- W933996250 abstract "The equation da/dN = C[(K I G - K I m i n ) + ΔK T ][(K I m a x - K I G ) - ΔK T ] 2 had been proposed by the author to predict crack growth rates. By adopting this functional relation and setting K I G = 0.5 K I m a x (K I G ∼ K I n p e n under constant-amplitude cyclic loading), there are the two parameters, C and ΔK I , left to be determined from experimental data. The parameters C and AK T for several structural alloys as a function of temperature between room temperature and 811 K had been analyzed. It was found that the fatigue tolerance range ΔK T decreased linearly with increasing temperature. Initially, the parameter C increases nearly linearly with increasing temperature and then increases steeply at higher temperatures. In the present work, this temperature dependence is shown to be found between 4 and 911 K by analyzing low-temperature as well as additional high-temperature data for Inconel 718 and Inconel X-750. By assuming the observed qualitative temperature dependence of C and ΔK T as being correct, available crack growth rates for Type 304 stainless steel obtained at temperatures ranging from 4 to 922 K were analyzed with respect to C and ΔK T ." @default.
- W933996250 created "2016-06-24" @default.
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- W933996250 date "2009-03-17" @default.
- W933996250 modified "2023-09-25" @default.
- W933996250 title "Fatigue Crack Growth Rates as a Function of Temperature" @default.
- W933996250 doi "https://doi.org/10.1520/stp28795s" @default.
- W933996250 hasPublicationYear "2009" @default.
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