Department of Naval Architecture & Ocean Engineering, Inha University, 253 Yonghyun-dong, Nam-gu, Incheon 402-751, Republic of Korea
Copyright © 2010 K. K. Viswanathan et al. This is an open access article distributed under the
Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Abstract
Free vibration of layered circular cylindrical shells of variable thickness is studied
using spline function approximation by applying a point collocation method. The shell is
made up of uniform layers of isotropic or specially orthotropic materials. The equations
of motions in longitudinal, circumferential and transverse displacement components, are
derived using extension of Love's first approximation theory. The coupled differential
equations are solved using Bickley-type splines of suitable order, which are cubic and
quintic, by applying the point collocation method. This results in the generalized
eigenvalue problem by combining the suitable boundary conditions. The effect of
frequency parameters and the corresponding mode shapes of vibration are studied with
different thickness variation coefficients, and other parameters. The thickness variations
are assumed to be linear, exponential, and sinusoidal along the axial direction. The results
are given graphically and comparisons are made with those results obtained using finite
element method.