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contributor authorWu
contributor authorHao;Du
contributor authorXiaoping
date accessioned2022-08-18T13:09:06Z
date available2022-08-18T13:09:06Z
date copyright4/28/2022 12:00:00 AM
date issued2022
identifier issn2332-9017
identifier otherrisk_008_04_041201.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4287521
description abstractReliability can be predicted by a limit-state function, which may vary with time and space. This work extends the envelope method for a time-dependent limit-state function to a time- and space-dependent limit-state function. The proposed method uses the envelope function of time- and space-dependent limit-state function. It at first searches for the most probable point (MPP) of the envelope function using the sequential efficient global optimization in the domain of the space and time under consideration. Then the envelope function is approximated by a quadratic function at the MPP for which analytic gradient and Hessian matrix of the envelope function are derived. Subsequently, the second-order saddlepoint approximation method is employed to estimate the probability of failure. Three examples demonstrate the effectiveness of the proposed method. The method can efficiently produce an accurate reliability prediction when the MPP is within the domain of the space and time under consideration.
publisherThe American Society of Mechanical Engineers (ASME)
titleEnvelope Method for Time- and Space-Dependent Reliability Prediction
typeJournal Paper
journal volume8
journal issue4
journal titleASCE-ASME J Risk and Uncert in Engrg Sys Part B Mech Engrg
identifier doi10.1115/1.4054171
journal fristpage41201-1
journal lastpage41201-9
page9
treeASCE-ASME J Risk and Uncert in Engrg Sys Part B Mech Engrg:;2022:;volume( 008 ):;issue: 004
contenttypeFulltext


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