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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 106
PROCEEDINGS OF THE TWELFTH INTERNATIONAL CONFERENCE ON COMPUTATIONAL STRUCTURES TECHNOLOGY Edited by:
Paper 162
Natural Frequencies of Composite Cross-Ply Spherical Panels using the Dynamic Stiffness Method and the Wittrick-Williams Algorithm F.A. Fazzolari and J.R. Banerjee
School of Engineering and Mathematical Sciences, City University London, United Kingdom F.A. Fazzolari, J.R. Banerjee, "Natural Frequencies of Composite Cross-Ply Spherical Panels using the Dynamic Stiffness Method and the Wittrick-Williams Algorithm", in , (Editors), "Proceedings of the Twelfth International Conference on Computational Structures Technology", Civil-Comp Press, Stirlingshire, UK, Paper 162, 2014. doi:10.4203/ccp.106.162
Keywords: direct stiffness method, free vibration, composites, Wittrick-Williams, spherical shells, symbolic computation..
Summary
An exact free vibration analysis of doubly-curved laminated composite shells has
been carried out by combining the dynamic stiffness method (DSM) and a higher
order shear deformation theory (HSDT) for the first time. In essence, the HSDT has
then been fruitfully exploited to develop first the shell element dynamic stiffness (DS)
matrix and then the global DS matrix of spherical shell structures by assembling the
individual DS elements. As an essential prerequisite, Hamilton's principle is used
to derive the governing differential equations and natural boundary conditions. The
equations are solved symbolically in an exact sense and the DSmatrix is formulated by
imposing the natural boundary conditions in an algebraic form. TheWittrick-Williams
algorithm is used as a solution technique to compute the eigenvalues of the overall DS
matrix. The effect of several parameters such as boundary conditions, orthotropic ratio,
length-to-thickness ratio and length-to-radius ratio on the natural frequencies and
mode shapes is investigated in details. The results are compared with those available
in the literature and also by using commercial software. Finally some concluding
remarks given.
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