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Author:

Zhang, Wei (Zhang, Wei.) (Scholars:张伟) | Huang, Yutong (Huang, Yutong.)

Indexed by:

EI Scopus

Abstract:

The nonlinear dynamic behavior ofalaminated composite cantilever plateis investigatedin this paper.The extended Melnikov method is employed to predict the multi-pulse chaotic motionsof the cantilever plate. The model is based on the wing flutter of the airplane.The cantilever plate is considered to be subjected to the in-plane and transversal excitations.TheReddy's high-order shear deformation theory as well as von Ka´rma´n type equations are used to establishthe equation of motion for the cantilever plate. Applyingthe Galerkin procedureto the partial differential governingequations of motion for the system, we obtain equationsof transverse displacement. Then the method of multiple scalesis usedto obtain the averagedequations. Finally,the extended Melnikov methodis usedto analyzethenonlinear behavior in the cantileverplatesystem.Thetheoretical result showsthat thereexistsmulti-pulse jumping movement.Thenumerical results also reveal such chaotic phenomenon. Copyright © 2011 by ASME.

Keyword:

Shear deformation Nanocantilevers Design Dynamics Equations of motion

Author Community:

  • [ 1 ] [Zhang, Wei]College of Mechanical Engineering, Beijing University of Technology, Beijing, 100124, China
  • [ 2 ] [Huang, Yutong]College of Mechanical Engineering, Beijing University of Technology, Beijing, 100124, China

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Source :

Year: 2011

Issue: PARTS A AND B

Volume: 4

Page: 1057-1065

Language: English

Cited Count:

WoS CC Cited Count:

SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 1

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