Research Article
Dec 1968
Natural Vibrations of Cylindrical Panels
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VIEW THE REPLYPublication: Journal of the Engineering Mechanics Division
Volume 94, Issue 6
Abstract
In terms of Lamé parameters, basic equations and energy expressions are formulated for the moderately thick-walled shells. The general formulations are then specialized for cylindrical panels. The frequency determinants are obtained by the Rayleigh-Ritz procedure. Both straight and curved characteristic beam functions have been utilized to obtain the frequencies of shell panels having different aspect ratios and central angles subtended by the curved edges and results compared. Effects of rotatory inertia, shear deformations as well as a few Poisson-type boundary conditions have also been considered and discussed.
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Published In
Journal of the Engineering Mechanics Division
Volume 94 • Issue 6 • December 1968
Pages: 1425 - 1446
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© 1968 American Society of Civil Engineers.
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Published in print: Dec 1968
Published online: Feb 3, 2021
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Authors
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Edward Y.W. Tsui, F.ASCE
Staff Scientist, Solid Mechanics, Aerospace Sci. Lab., Lockheed Missiles and Space Co., Palo Alto, Calif.
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ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.
Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.