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- W2100076969 abstract "This paper describes results of an elevated temperature fatigue crack growth study in IN-100, a nickel-base superalloy. The objective of this study was to determine if conventional fracture mechanics techniques can predict crack growth under conditions expected to occur in jet engine turbine disks. Results are reported for two types of experiments. The first group of tests examines isolated load events that may occur in a turbine disk load history. The influence of tensile overloads, compressive underloads, overload/underload sequences, and periods of sustained load on subsequent constant amplitude fatigue crack growth are discussed. The second group of specimens was subjected to a spectrum load history that combines many of the isolated load events. Cumulative damage crack growth predictions are performed by several procedures and shown to agree quite well with the experimental results. The influence of specimen thickness is considered for both the isolated event and the spectrum loading experiments." @default.
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- W2100076969 date "2009-03-16" @default.
- W2100076969 modified "2023-09-24" @default.
- W2100076969 title "Effects of Gas Turbine Engine Load Spectrum Variables on Crack Propagation" @default.
- W2100076969 doi "https://doi.org/10.1520/stp27485s" @default.
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