Three-dimensional free vibration analysis of thick laminated circular plates

Abstract

In this communication, a numerical analysis regarding free vibration of thick laminated circular plates, having free, clamped as well as simply-supported boundary conditions at outer edges of plates is presented. The employment of finite element is made in this communication. The finite element methodology operates on the basis of three-dimensional theory of elasticity and was employed to assess the natural frequencies for laminated circular plates of various thickness-to-outer radius ratios. The first five natural modes of flexural vibrations for different boundary conditions are presented in pictorial forms. Verification of the accuracy of the results was made using the necessary convergence analysis and checked using literature results.

Static, Free Vibration and Buckling Analysis of Composite Panels; A Review

“…The natural frequency comparison of laminated composite beams based on different boundary conditions and different laminated lay-up sequences with variation in the L/ h (length/height) ratio, L/b (length/breadth) ratio and EL/ET ratio was performed in the ANSYS. Sumit Khare et al [92] have done 3D FEA for free vibration of thick laminated composite circular plates with clamped, simply supported and free boundary condition for different fiber orientation. Ganapathi et al [93] investigated the anisotropic composite laminates for the free vibration features simply supported by an analytical approach.…”