NASA NTRS · 19950008061
Fatigue reliability method with in-service inspections
Abstract
The first reliability method (FORM) has traditionally been applied in a fatigue reliability setting to one inspection interval at a time, so that the random distribution of crack lengths must be recharacterized following each inspection. The FORM presented here allow each analysis to span several inspection periods without explicit characterization of the crack length distribution upon each inspection. The method thereby preserves the attractive feature of FORM in that relatively few realizations in the random variable space need to be considered. Examples are given which show that the present methodology gives estimates which are in good agreement with Monte Carlo simulations and is efficient even for complex components.
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Harkness, H. H., Fleming, M., Moran, B., Belytschko, T.. 1994-09-01. Fatigue reliability method with in-service inspections. https://ntrs.nasa.gov/citations/19950008061
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