๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Geometrically nonlinear forced vibrations of the symmetric honeycomb sandwich panels affected by the water

โœ Scribed by Li Yongqiang; Zhu Dawei


Publisher
Elsevier Science
Year
2011
Tongue
English
Weight
559 KB
Volume
93
Category
Article
ISSN
0263-8223

No coin nor oath required. For personal study only.

โœฆ Synopsis


Geometrically nonlinear forced vibrations of the symmetric rectangular honeycomb sandwich panels with the four edges simply supported and one surface affected by the water are investigated in this paper using the homotopy analysis method (HAM). The honeycomb core of hexagonal cells is modeled as a thick layer of orthotropic material whose physical and mechanical properties are determined using the Gibson correlations. The effect of water acting on honeycomb panels can be described as added mass, additional damping and additional stiffness coefficients which are obtained by the semi-analytical fluid pressures. The basic formulation of nonlinear forced vibrations has been developed base on the thirdorder shear deformation plate theory and Green Lagrange nonlinear strain-displacement relation. The equilibrium equations have been obtained using the Hamilton's principle. Effects of water velocity, height and height ratio on the nonlinear forced vibration response have been studied for the honeycomb sandwich panels.


๐Ÿ“œ SIMILAR VOLUMES


Geometrically nonlinear forced vibration
โœ Yongqiang Li; Feng Li; Yongliang He ๐Ÿ“‚ Article ๐Ÿ“… 2011 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 580 KB

Geometrically nonlinear forced vibrations of symmetric rectangular honeycomb sandwich panels with clamped supported boundaries at the four edges are investigated using the homotopy analysis method (HAM). The honeycomb core of hexagonal cells is modeled as a thick layer of orthotropic material whose

Geometrically nonlinear free vibrations
โœ Li Yongqiang; Li Feng; Zhu Dawei ๐Ÿ“‚ Article ๐Ÿ“… 2010 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 784 KB

Geometrically nonlinear free vibrations of symmetric rectangular honeycomb sandwich panels with simply supported boundaries at the four edges are investigated using the homotopy analysis method (HAM). The honeycomb core of hexagonal cells is modeled as a thick layer of orthotropic material whose par