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作者:

Zhang, Wei (Zhang, Wei.) | Lu, Shufeng (Lu, Shufeng.)

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摘要:

This paper focus on the nonlinear numerical analysis for an extruding cantilever laminated composite plates subjected to transversal and in-plane excitation. Based on the ReddyaˆTMs shear deformable plate theory, the nonlinear partial differential equations of motion were established by using the Hamilton Principal. And then, after choosing suitable vibration mode-shape functions, the Galerkin method was used to reduce the governing partial differential equations to a two-degree-of-freedom nonlinear ordinary differential equation. Finally, we numerical solved the nonlinear ordinary differential equation, and analyzed the influences of varying extruding speeds and thickness of plates on the stability of the plates. Copyright © 2012 by ASME.

关键词:

Degrees of freedom (mechanics) Design Equations of motion Galerkin methods Laminated composites Laminating Nanocantilevers Nonlinear equations Ordinary differential equations Partial differential equations Vibrations (mechanical)

作者机构:

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

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年份: 2012

期: PARTS A AND B

卷: 1

页码: 807-811

语种: 英文

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SCOPUS被引频次: 1

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