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Full Length Article | Open Access

An interval finite element method based on bilevel Kriging model

Zhongyang YAOaShaohua WANGbPengge WUcBingyu NIaChao JIANGa( )
State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body, College of Mechanical and Vehicle Engineering, Hunan University, Changsha 410082, China
Flight Automatic Control Research Institute of AVIC, Xi’an 710065, China
Agriculture Equipment Institute of Hunan, Hunan Academy of Agricultural Sciences, Changsha 410125, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

This study introduces a new approach utilizing an interval finite element method combined with a bilevel Kriging model to determine the bounds of structural responses in the presence of spatial uncertainties. A notable benefit of this approach is its ability to determine the response bounds across all degrees of freedom with a small sample size, which means that it has high efficiency. Firstly, the spatially varying uncertain parameters are quantified using an interval field model, which is described by a series of standard interval variables within a truncated interval Karhunen-Loève (K-L) series expansion. Secondly, considering that the bound of structural response is a function of spatial position with the property of continuity, a surrogate model for the response bound is constructed, namely the first-level Kriging model. The training samples required for this surrogate model are obtained by establishing the second-level Kriging model. The second-level Kriging model is established to describe the structural responses at particular locations relative to the interval variables so as to facilitate the upper and lower bounds of the node response required by the first-level Kriging model. Finally, the accuracy and effectiveness of the method are verified through examples.

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Chinese Journal of Aeronautics
Pages 1-11

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Cite this article:
YAO Z, WANG S, WU P, et al. An interval finite element method based on bilevel Kriging model. Chinese Journal of Aeronautics, 2024, 37(12): 1-11. https://doi.org/10.1016/j.cja.2024.09.035

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Received: 13 June 2024
Revised: 01 July 2024
Accepted: 02 September 2024
Published: 26 September 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).