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Nonlinear frequency prediction and uncertainty analysis for fully clamped laminates by using a self-developed multi-scale neural networks system: Nonlinear frequency uncertainty analysis by the self-developed neural network system

Research output: Contribution to journalArticlepeer-review

Abstract

To improve design accuracy and reliability of structures, this study solves the uncertain natural frequencies with consideration for geometric nonlinearity and structural uncertainty. Frequencies of the laminated plate with all four edges clamped (CCCC) are derived based on Navier's method and Galerkin's method. The novelty of the current work is that the number of unknowns in the displacement field model of a CCCC plate with free midsurface (CCCC-2 plate) is only three compared with four or five in cases of other exposed methods. The present analytical method is proved to be accurate and reliable by comparing linear natural frequencies and nonlinear natural frequencies with other models available in the open literature. Furthermore, a novel method for analyzing effects of mean values and tolerance zones of uncertain structural parameters on random frequencies is proposed based on a self-developed Multiscale Feature Extraction and Fusion Network (MFEFN) system. Compared with a direct Monte Carlo Simulation (MCS), the MFEFN-based procedure significantly reduces the calculation burden with a guarantee of accuracy. Our research provides a method to calculate nonlinear natural frequencies under two boundary conditions and presentes a surrogate model to predict frequencies for accuracy analysis and optimization design.

Original languageEnglish
Article number103466
JournalChinese Journal of Aeronautics
Volume38
Issue number9
DOIs
StatePublished - Sep 2025
Externally publishedYes

Keywords

  • Geometric nonlinearity
  • Laminates
  • Multiscale feature extraction and fusion networks (MFEFN)
  • Natural frequency
  • Uncertainty analysis

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