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参数相关性驱动的复合材料加筋板屈曲可靠性及灵敏性分析

Translated title of the contribution: Parameter correlation-driven buckling reliability and sensitivity analysis for composite stiffened panels
  • Xiaofeng Xue
  • , Yizhe Cao
  • , Yunwen Feng
  • , Zhicen Song
  • , Hao Hu
  • Northwestern Polytechnical University Xian
  • National Key Laboratory of Aircraft Configuration Design

Research output: Contribution to journalArticlepeer-review

Abstract

To address the reduced accuracy in reliability analysis of composite structures due to parameter correlations, this study proposes a Copula-Kriging synergistic reliability method (CK-SRM). By integrating joint probability modeling and surrogate model optimization, CK-SRM quantifies the statistical dependencies of elastic parameters, overcoming the limitations of traditional independent assumptions. The model is validated via buckling tests and engineering computational methods. A Kriging surrogate model is constructed using Latin hypercube sampling and parametric finite element modeling to predict buckling loads. A quantitative mapping relationship among parameter correlations, reliability, and load-bearing capacity is established. Gaussian Copula-based sampling is employed to analyze reliability and structural capacity under single flight probability of failure of 10−7. Sensitivity analysis evaluates the impacts of parameter correlations. Results demonstrate that considering parameter correlations improves the load-bearing capacity of composite stiffened panels by 4.7% compared to deterministic design based on the safety factor method. This method provides critical insights for optimizing composite stiffened panel designs, enhancing structural safety, and fully leveraging material performance.

Translated title of the contributionParameter correlation-driven buckling reliability and sensitivity analysis for composite stiffened panels
Original languageChinese (Traditional)
Pages (from-to)3897-3910
Number of pages14
JournalFuhe Cailiao Xuebao/Acta Materiae Compositae Sinica
Volume43
Issue number6
DOIs
StatePublished - Jun 2026

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