Techno Press
Techno Press

Steel and Composite Structures   Volume 20, Number 5, April10 2016, pages 1087-1102
DOI: http://dx.doi.org/10.12989/scs.2016.20.5.1087
 
Free vibration analysis of composite cylindrical shells with non-uniform thickness walls
Saira Javed, K.K. Viswanathan and Z.A. Aziz

 
Abstract     [Full Text]
    The paper proposes to characterize the free vibration behaviour of non-uniform cylindrical shells using spline approximation under first order shear deformation theory. The system of coupled differential equations in terms of displacement and rotational functions are obtained. These functions are approximated by cubic splines. A generalized eigenvalue problem is obtained and solved numerically for an eigenfrequency parameter and an associated eigenvector which are spline coefficients. Four and two layered cylindrical shells consisting of two different lamination materials and plies comprising of same as well as different materials under two different boundary conditions are analyzed. The effect of length parameter, circumferential node number, material properties, ply orientation, number of lay ups, and coefficients of thickness variations on the frequency parameter is investigated.
 
Key Words
    free vibration; anti-symmetric; non-uniform thickness; shear deformation; spline approximation; frequency parameter
 
Address
(1) UTM Centre for Industrial and Applied Mathematics (UTM-CIAM), Ibnu SIna Institiute for Scientific & Industrial Research, Universiti Teknologi Malaysia, 81310 Johor Bahru, Johor, Malaysia;
(2) Department of Mathematical Sciences, Faculty of Science, Universiti Teknologi Malaysia, 81310 Johor Bahru, Johor, Malaysia.
 

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