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Fatigue reliability method with in-service inspectionsThe 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.
Document ID
19950008061
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harkness, H. H.
(Northwestern Univ. Evanston, IL, United States)
Fleming, M.
(Northwestern Univ. Evanston, IL, United States)
Moran, B.
(Northwestern Univ. Evanston, IL, United States)
Belytschko, T.
(Northwestern Univ. Evanston, IL, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance
Subject Category
Quality Assurance And Reliability
Accession Number
95N14475
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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