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Author:

Guo, X. (Guo, X..) | Zhang, Y. (Zhang, Y..) | Luo, Z. (Luo, Z..) | Cao, D. (Cao, D..)

Indexed by:

EI Scopus SCIE

Abstract:

Linear and nonlinear vibration characteristics of the graphene platelet-reinforced composite (GPLRC) laminated plates are investigated. Based on the first-order shear theory and von Karman geometric nonlinearity, the energy expressions of the GPLRC laminates are established. The boundary elastic potential energy is established by penalty function method to simulate different boundary conditions. The linear and nonlinear frequencies of the GPLRC laminated plate are calculated by introducing boundary potential energy into Rayleigh–Ritz method. The convergence and accuracy of the method are verified by numerical examples, and the effects of different parameters on frequency are analyzed. Considering the cantilever boundary conditions, the nonlinear motion governing equations of the GPLRC laminated plate are obtained by Hamilton principle. The two-degree-freedom ordinary differential motion equations of the laminates are derived by Galerkin method. Considering the fundamental parameter resonance and 1:1 internal resonance, the amplitude–frequency response curves of the structure under transverse excitation are obtained. The effects of transverse excitation and damping coefficient on nonlinear vibration characteristics of the GPLRC laminated plates are investigated by numerical simulation. © 2023 Elsevier Ltd

Keyword:

Internal resonance Rayleigh–Ritz method Nonlinear vibration GPLRC

Author Community:

  • [ 1 ] [Guo X.]Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing, 100124, China
  • [ 2 ] [Guo X.]Beijing Key Laboratory of Nonlinear Vibrations and Strength of Mechanical Structures, Beijing, 100124, China
  • [ 3 ] [Zhang Y.]Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing, 100124, China
  • [ 4 ] [Zhang Y.]Beijing Key Laboratory of Nonlinear Vibrations and Strength of Mechanical Structures, Beijing, 100124, China
  • [ 5 ] [Luo Z.]Key Laboratory of Vibration and Control of Aero-Propulsion System, Ministry of Education, Northeastern University, 110006, China
  • [ 6 ] [Cao D.]Faculty of Materials and Manufacturing, Beijing University of Technology, Beijing, 100124, China
  • [ 7 ] [Cao D.]Beijing Key Laboratory of Nonlinear Vibrations and Strength of Mechanical Structures, Beijing, 100124, China

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Source :

Thin-Walled Structures

ISSN: 0263-8231

Year: 2023

Volume: 186

6 . 4 0 0

JCR@2022

ESI Discipline: ENGINEERING;

ESI HC Threshold:19

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count: 20

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 9

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