TECHNICAL NOTES
Jul 1, 2006

Vibration of Open Cylindrical Shells with Stepped Thickness Variations

Publication: Journal of Engineering Mechanics
Volume 132, Issue 7

Abstract

This paper presents the first-known exact solutions for vibration of open circular cylindrical shells with multiple stepwise thickness variations based on the Flügge thin shell theory. An open cylindrical shell is assumed to be simply supported along the two straight edges and the remaining two opposite curved edges may have any combination of edge support conditions. The shell is subdivided into segments at the locations of thickness variations. The state-space technique is adopted to derive the homogenous differential equations for a shell segment and the domain decomposition method is employed to impose the equilibrium and compatibility requirements along the interfaces of the shell segments. The correctness of the proposed method is checked against existing results in the open literature and results generated from finite element package ANSYS and excellent agreement is achieved. Several open shells with various combinations of end boundary conditions are studied by the proposed method.

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Acknowledgment

The work described in this paper was fully supported by a research grant from the University of Western Sydney, Sydney, Australia (Grant No. UNSPECIFIED20801-80418).

References

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Information

Published In

Go to Journal of Engineering Mechanics
Journal of Engineering Mechanics
Volume 132Issue 7July 2006
Pages: 780 - 784

History

Received: Sep 14, 2004
Accepted: Nov 9, 2005
Published online: Jul 1, 2006
Published in print: Jul 2006

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Notes

Note. Associate Editor: Bojan B. Guzina

Authors

Affiliations

L. Zhang
Ph.D. Student, School of Engineering and Industrial Design, Univ. of Western Sydney, Locked Bag 1797, Penrith South DC, N.S.W., Australia.
Y. Xiang, M.ASCE [email protected]
Associate Professor, School of Engineering and Industrial Design, Univ. of Western Sydney, Locked Bag 1797, Penrith South DC, N.S.W., Australia (corresponding author). E-mail: [email protected]

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