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- W1499681652 abstract "Abstract : An experimental investigation was conducted to evaluate the effects of hold-times on the fatigue crack growth rate of Inconel 718 to 649 C using compact tension specimens. Tests were run under computer controlled constant K conditions using compliance to determine crack length. Hold-times ranging from 5 to 50 s were applied at maximum, minimum, and intermediate load levels. The data show that hold-times at maximum load were the most damaging in terms of crack growth rate. Hold times greater than 5 s led to purely time-dependent crack growth behavior which was predictable from sustained load data using K as a correlating parameter. Hold-times at a minimum or intermediate load levels had little or no effect on crack growth rate. A linear cumulative damage model based solely on fatique and sustained load data was found to be adequate for spectrum loading as long as the hold-times were at maximum load. Additional keywords: gas turbine engines; Air Force equipment; aircraft engines. (Author)" @default.
- W1499681652 created "2016-06-24" @default.
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- W1499681652 date "2008-12-08" @default.
- W1499681652 modified "2023-09-23" @default.
- W1499681652 title "Hold-Time Effects in Elevated Temperature Fatigue Crack Propagation" @default.
- W1499681652 doi "https://doi.org/10.1520/stp17394s" @default.
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