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Full Length Article | Open Access

Higher-order vibration of thick composite and sandwich plates based on an alternative higher-order model

Jinghui DENGaTangzhen WUaZhen WUb( )Zhengliang LIUbXiaohui RENc
China Helicopter Research and Development Institute, Jingdezhen 333001, China
School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China
School of Mechanical Engineering, Xi’an Aeronautical University, Xi’an 710065, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

The transverse stretching vibration of thick sandwich plates, which is attributed to largely different stiffness at the adjacent layers, is a challenging issue, and efficient approach for such issue is less reported in the published literature. Thus, natural frequencies corresponding to stretching vibration modes are generally neglected in engineering design, which might impact structural safety as frequencies of the exciting force are close to transverse stretching vibration frequencies. This paper proposes an alternative higher-order model for dynamic analysis corresponding to the higher-order vibration modes. The proposed model is classified in the displacement-based equivalent single-layer theory, as the number of displacement parameters in the proposed model is independent of the layer number. The continuity of displacements and transverse shear stresses can be fulfilled at the interfaces between the adjacent layers of structures. To demonstrate the capability of the proposed model, typical examples are analyzed by utilizing the proposed model, the three-dimensional finite element method and the chosen higher-order models. By comparing with the exact three-dimensional elasticity solutions, it is found that the proposed model can yield more accurate natural frequencies corresponding to the higher-order displacement modes than the selected models. Moreover, the factors influencing reasonable prediction of the higher-order frequencies are investigated in detail, which can provide a reference for the accurate prediction of the higher-order frequencies.

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Chinese Journal of Aeronautics
Pages 406-420

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Cite this article:
DENG J, WU T, WU Z, et al. Higher-order vibration of thick composite and sandwich plates based on an alternative higher-order model. Chinese Journal of Aeronautics, 2023, 36(3): 406-420. https://doi.org/10.1016/j.cja.2022.11.023

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Received: 02 December 2021
Revised: 24 December 2021
Accepted: 31 December 2021
Published: 26 November 2022
© 2022 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/).