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Free and forced vibration of simply supported, orthotropic sandwich panel

โœ Scribed by Tat-Seng Lok; Qian-Hua Cheng


Book ID
108391291
Publisher
Elsevier Science
Year
2001
Tongue
English
Weight
198 KB
Volume
79
Category
Article
ISSN
0045-7949

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๐Ÿ“œ SIMILAR VOLUMES


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Sandwich panels are thin-walled structures fabricated from two #at sheets, separated by and attached to a core. An analytical solution for the dynamic response of such structures is not available but equivalency in the form of a homogenous orthotropic thick plate can be formulated. This paper consid

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A closed-form solution for the forced response of an orthotropic thick plate and sandwich panel has been developed and is presented in this paper. The paper outlines the methodology and develops the formulation to enable the solution to be derived. A novel truss-core sandwich panel is introduced and

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In this paper, the free vibrations characteristics of simply supported anisotropic composite laminates are investigated using analytical approach. The formulation is based on the first-order shear deformation theory and the shear correction factors employed are based on energy consideration that dep

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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