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      Adaptive Kriging Model for Fuzzy Safety Degree Analysis to Time-Dependent Structure

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          Abstract

          Time-dependent failure possibility (TDFP) has the capability to measure the safety degree of a structure under fuzzy uncertainty over a service time interval of interest. To improve the computational efficiency in estimating TDFP, an adaptive kriging model is developed in this paper. In the proposed method, TDFP is first represented as a bilevel problem, where the outer level is a one-dimensional rooting problem with respect to the membership level of fuzzy variables and the inner level is a minimum optimization of the model response function where the interval parameters and time are regarded as the same level. Second, the dichotomy instead of the interpolation technique is employed to solve the one-dimensional rooting problem. Third, the numerical simulation replacing the optimization technique is used to settle the optimization problem. Finally, to greatly reduce the computational cost in estimating the TDFP especially involved in numerical simulations, an adaptive kriging model is proposed for TDFP analysis. Additionally, the proposed kriging model can be used to estimate the safety life based on the TDFP constraint. The results of a mathematical example and two aerospace engineering examples show that the proposed method significantly improves the efficiency in estimating the TDFP and the TDFP-based safety life with acceptable precision.

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          Most cited references40

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          Fuzzy sets as a basis for a theory of possibility

          L.A. Zadeh (1978)
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            Large Sample Properties of Simulations Using Latin Hypercube Sampling

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              AK-MCS: An active learning reliability method combining Kriging and Monte Carlo Simulation

                Author and article information

                Contributors
                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                29 December 2021
                May 2021
                : 59
                : 5
                : 1528-1538
                Affiliations
                Northwestern Polytechnical University , 710072 Xi’an, People’s Republic of China
                China Academy of Engineering Physics , 621999 Mianyang, People’s Republic of China
                Author notes
                [*]

                School of Aeronautics, P.O. Box 120, Shaanxi Province; 18392592026@ 123456163.com .

                [†]

                Professor, School of Aeronautics, P.O. Box 120, Shaanxi Province; zhenzhoulu@ 123456nwpu.edu.cn (Corresponding Author).

                [‡]

                School of Aeronautics, P.O. Box 120, Shaanxi Province; ning_wei062@ 123456126.com .

                [§]

                Institute of System Engineering, P.O. Box 64, Sichuan Province; 411liguij@ 123456caep.cn .

                Article
                J059834 J059834
                10.2514/1.J059834
                1e30ff90-e56b-4355-84e6-1aa76ba9bf6c
                Copyright © 2020 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 28 May 2020
                : 07 October 2020
                : 09 October 2020
                Page count
                Figures: 11, Tables: 13
                Funding
                Funded by: National Natural Science Foundation of Chinahttp://dx.doi.org/10.13039/501100001809
                Award ID: 51775439
                Funded by: The National Science and Technology Major Project
                Award ID: 2017-IV-0009-0046
                Funded by: The Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University
                Award ID: Grant No. CX201934
                Categories
                Regular Articles
                p2263, Fluid Dynamics
                p3282, Computational Fluid Dynamics
                p3304, Numerical Analysis
                p2057, Finite Element Method
                p1804, Aerodynamics
                p20603, Finite Element Software
                p3421, General Physics
                p8079, Statistical Analysis

                Engineering,Physics,Mechanical engineering,Space Physics
                Surrogate Model,Aeronautical Engineering,Allowable Stress,Elevator,Aircraft Wings,Aerodynamic Force,Finite Element Modeling,Probability Density Functions,Numerical Simulation,Aerospace Engineering

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