Predicting Fatigue Crack Growth and Fatigue Life Under Variable Amplitude Loading
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Predicting Fatigue Crack Growth and Fatigue Life Under Variable Amplitude Loading A probabilistic approach to the description of fatigue crack growth and fatigue life estimation of a component subjected to variable amplitude loading is presented in the paper. The core of the model is a differential equation originated from the Paris formula. In order to consider the influence of overload-underload cycles existing in an exploitive load spectrum on crack growth rate for an aeronautical aluminum alloy sheet, the modified Willenborg retardation model was applied.
2011 ◽
Vol 462-463
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pp. 489-494
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1989 ◽
pp. 1367-1375
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1973 ◽
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2016 ◽
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1991 ◽
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2020 ◽
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pp. 105588
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