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A General Mode Approach to Nonlinear Flexural Vibrations of Laminated Rectangular Plates

C. Y. Chia, +1 more
- 01 Sep 1978 - 
- Vol. 45, Iss: 3, pp 623-628
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This article is published in Journal of Applied Mechanics.The article was published on 1978-09-01. It has received 48 citations till now.

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Thermal effects on nonlinear vibration behavior of viscoelastic nanosize plates

TL;DR: In this paper, the nonlinear thermomechanical vibration behavior of viscoelastic nanoplates is investigated based on nonlocal elasticity theory, and the geometrical nonlinearity is modeled while governing equations are solved applying semi-analytical differential quadrature method (DQM).
Journal ArticleDOI

Large-deflection and large-amplitude free vibrations of laminated composite-material plates

TL;DR: In this paper, a finite-element analysis of the large-deflection theory, including transverse shear, including laminated anisotropic composite plates, is presented, showing the parametric effects of plate aspect ratio, side-to-thickness ratio, orientation of layers, and anisotropy.
Journal ArticleDOI

Non-linear bending of thick rectangular, laminated composite plates

TL;DR: In this paper, a shear deformable theory accounting for the transverse shear and large rotations is employed in the construction of a variational statement and associated finite element models of layered composite plates.
Journal ArticleDOI

Nonlinear electroelastic vibration analysis of NEMS consisting of double-viscoelastic nanoplates

TL;DR: In this article, the nonlinear electroelastic vibration behavior of viscoelastic nanoplates is investigated based on nonlocal elasticity theory, and the geometrical nonlinearity is modeled while governing equations are derived through Hamilton's principle and they are solved applying semi-analytical generalized differential quadrature (GDQ) method.
Journal ArticleDOI

Large amplitude free vibration analysis of cross-ply composite and sandwich laminates with a refined theory and C° finite elements

TL;DR: In this article, a refined higher-order shear deformation theory has been developed for large amplitude, in the sense of von Karman, free vibration analysis of fibre reinforced cross-ply composite and sandwich laminates by assuming cubic variations of in-plane displacement components and a constant transverse displacement component through the thickness of the laminate.