A finite element analysis for the free vibration behaviour of point supported laminated composite cylindrical shells is presented. Eight-noded curved quadrilateral isoparametric elements are used. The formulation is based on the assumptions of the first order shear deformation theory for thin, shall
Free vibration analysis of simply supported composite laminated panels
β Scribed by M. Ganapathi; Amit Kalyani; Bhaskar Mondal; T. Prakash
- Publisher
- Elsevier Science
- Year
- 2009
- Tongue
- English
- Weight
- 250 KB
- Volume
- 90
- Category
- Article
- ISSN
- 0263-8223
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β¦ Synopsis
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 depends on the layup as well as material properties. The governing equations are obtained using energy method. For this purpose, a displacement model with a combination of sine and cosine functions in the form of double Fourier series is taken. The effectiveness of the integrated formulation is tested for global behaviors considering examples related to multi-layered laminates having various values for curvatures, thickness ratio, and lay-up for which solutions are available.
π SIMILAR VOLUMES
Free vibration analysis of symmetrically laminated composite rectangular plates with all edges elastically restrained against rotation was carried out based on the first order anisotropic shear deformation plate theory. The iterative Kantorovich method and the Rayleigh-Ritz method with three differe
This paper deals with the flexural vibration behavior of bimodular laminated composite cylindrical panels with various boundary conditions. The formulation is based on first order shear deformation theory and Bert's constitutive model. The governing equations are derived using finite element method