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Publishing Language: Chinese

RBF-enhanced direct probability integral method for stochastic buckling analysis of plate and shell structures

Chaofan WANG1, Huanlin ZHOU1, Xuan WANG1,2( )
Department of Engineering Mechanics, Hefei University of Technology, Hefei 230009, China
State Key Laboratory of Structural Analysis, Optimization and CAE Software for Industrial Equipment, Dalian University of Technology, Dalian 116024, China
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Abstract

As critical load-bearing components in aerospace, marine, and construction engineering fields, the buckling stability of plate and shell structures directly determines the safety and reliability of entire systems. However, factors such as material property variability significantly influence the distribution characteristics of critical buckling loads, the traditional deterministic analysis methods are hard to quantify the stochastic influence. The Radial Basis Function (RBF)-enhanced Direct Probability Integral Method (DPIM) is proposed to efficiently determine the probabilistic characteristics of buckling critical loads in plate and shell structures under multiple random variables, which provides theoretical foundations for stochastic buckling uncertainty quantification. By constructing a high-precision explicit surrogate model between critical buckling loads and random variables using RBF, this method effectively reduces the computational cost for implementing the time-consuming buckling finite element analysis in the original direct probability integral method. Comparative analyses with traditional DPIM and Monte Carlo simulation methods in numerical examples demonstrate that the proposed RBF-enhanced DPIM achieves remarkable computational efficiency improvements while maintaining controlled accuracy loss.

CLC number: V214.3;O342 Document code: A Article ID: 1000-6893(2026)03-232214-10

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
WANG C, ZHOU H, WANG X. RBF-enhanced direct probability integral method for stochastic buckling analysis of plate and shell structures. Acta Aeronautica et Astronautica Sinica, 2026, 47(3). https://doi.org/10.7527/S1000-6893.2025.32214

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Received: 08 May 2025
Revised: 11 August 2025
Accepted: 08 September 2025
Published: 19 September 2025
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica