Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped Edges

It is fundamental to obtain the natural frequencies and the corresponding mode shapes for cylindrical shells in order to determine their response to different dynamic loading. In this paper an analytical investigation to the free vibration response of moderately-thick shear flexible isotropic cylind...

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Main Authors: Zafer I. Sakka, Jamal A. Abdalla, H.R.H. Kabir
Format: Article
Language:English
Published: Hindawi Limited 2006-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2006/861807
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spelling doaj-cb148efedd654458b385b6b79e382b002020-11-25T01:06:40ZengHindawi LimitedShock and Vibration1070-96221875-92032006-01-0113210311610.1155/2006/861807Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped EdgesZafer I. Sakka0Jamal A. Abdalla1H.R.H. Kabir2University of New South Wales, AustraliaDepartment of Civil Engineering, American University of Sharjah, UAEDepartment of Civil Engineering, Kuwait University, KuwaitIt is fundamental to obtain the natural frequencies and the corresponding mode shapes for cylindrical shells in order to determine their response to different dynamic loading. In this paper an analytical investigation to the free vibration response of moderately-thick shear flexible isotropic cylindrical shells with all edges clamped is presented. The Sander’s kinematic relations for moderately thick cylindrical shell panels are utilized to develop the governing partial differential equations in conjunction with the boundary conditions. A recently developed generalized Navier’s approach, based on a boundary continuous double Fourier series expansion, is used as a solution methodology. A parametric study is presented with respect to various thicknesses, length and radius of curvature of the shell panel. The convergence of the solution method is established numerically for various parametric properties. The present results are compared with the results obtained from finite element method using a four-node isoparametric shell element. The results thus presented should serve as bench-mark solutions for future comparisons with numerical and approximate methods for calculation of free vibration parameters of moderately-thick isotropic cylindrical shells.http://dx.doi.org/10.1155/2006/861807
collection DOAJ
language English
format Article
sources DOAJ
author Zafer I. Sakka
Jamal A. Abdalla
H.R.H. Kabir
spellingShingle Zafer I. Sakka
Jamal A. Abdalla
H.R.H. Kabir
Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped Edges
Shock and Vibration
author_facet Zafer I. Sakka
Jamal A. Abdalla
H.R.H. Kabir
author_sort Zafer I. Sakka
title Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped Edges
title_short Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped Edges
title_full Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped Edges
title_fullStr Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped Edges
title_full_unstemmed Dynamic Response of Shear-Flexible Cylindrical Isotropic Shells with Clamped Edges
title_sort dynamic response of shear-flexible cylindrical isotropic shells with clamped edges
publisher Hindawi Limited
series Shock and Vibration
issn 1070-9622
1875-9203
publishDate 2006-01-01
description It is fundamental to obtain the natural frequencies and the corresponding mode shapes for cylindrical shells in order to determine their response to different dynamic loading. In this paper an analytical investigation to the free vibration response of moderately-thick shear flexible isotropic cylindrical shells with all edges clamped is presented. The Sander’s kinematic relations for moderately thick cylindrical shell panels are utilized to develop the governing partial differential equations in conjunction with the boundary conditions. A recently developed generalized Navier’s approach, based on a boundary continuous double Fourier series expansion, is used as a solution methodology. A parametric study is presented with respect to various thicknesses, length and radius of curvature of the shell panel. The convergence of the solution method is established numerically for various parametric properties. The present results are compared with the results obtained from finite element method using a four-node isoparametric shell element. The results thus presented should serve as bench-mark solutions for future comparisons with numerical and approximate methods for calculation of free vibration parameters of moderately-thick isotropic cylindrical shells.
url http://dx.doi.org/10.1155/2006/861807
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AT jamalaabdalla dynamicresponseofshearflexiblecylindricalisotropicshellswithclampededges
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