ArticlePDF Available

Natural frequencies and mode shapes of variable thickness elastic cylindrical shells resting on a Pasternak foundation

SAGE Publications Inc
Journal of Vibration and Control
Authors:
  • South Vally University, Luxor , Qena , Egypt

Abstract and Figures

According to the framework of the Flügge’s shell theory, the Winkler and Pasternak foundations model, the transfer matrix approach and the Romberg integration method, the vibration behavior of an isotropic and orthotropic cylindrical shell with variable thickness is investigated. The governing equations of the shell based on the Pasternak foundation model are formulated and solved. The analysis is formulated to overcome the mathematical difficulties related to mode coupling which comes from the variable curvature and thickness of the shell. The vibration equations of the shell are reduced to eight first order differential equations in the circumferential coordinate. Using the transfer matrix of the shell, these equations can be written in a matrix differential equation. The proposed model is adopted to get the vibration frequencies and the corresponding mode shapes for the symmetrical and antisymmetrical modes of vibration. The sensitivity of the frequency parameters and the bending deformations to the Winkler and Pasternak foundations moduli, the thickness ratio, and the orthotropic parameters are demonstrated.
This content is subject to copyright.
Article
Natural frequencies and mode shapes of
variable thickness elastic cylindrical shells
resting on a Pasternak foundation
Mousa Khalifa Ahmed
Abstract
According to the framework of the Flu¨gge’s shell theory, the Winkler and Pasternak foundations model, the transfer
matrix approach and the Romberg integration method, the vibration behavior of an isotropic and orthotropic cylindrical
shell with variable thickness is investigated. The governing equations of the shell based on the Pasternak foundation
model are formulated and solved. The analysis is formulated to overcome the mathematical difficulties related to mode
coupling which comes from the variable curvature and thickness of the shell. The vibration equations of the shell are
reduced to eight first order differential equations in the circumferential coordinate. Using the transfer matrix of the shell,
these equations can be written in a matrix differential equation. The proposed model is adopted to get the vibration
frequencies and the corresponding mode shapes for the symmetrical and antisymmetrical modes of vibration. The
sensitivity of the frequency parameters and the bending deformations to the Winkler and Pasternak foundations
moduli, the thickness ratio, and the orthotropic parameters are demonstrated.
Keywords
Orthotropic cylindrical shells, symmetric and antisymmetric modes, transfer matrix method, variable thickness, vibration
behavior, Winkler-Pasternak foundation
1. Introduction
Cylindrical shells which have variable thickness in con-
tact with elastic foundations are found in many engin-
eering applications, such as aerospace, mechanical, civil
and marine structures. The frequencies and mode
shapes of vibration essentially depend on some deter-
mining functions such as the radius of the curvature of
the neutral surface, the shell thickness, the shape of the
shell edges, the elastic media, and so on. In simple cases
when these functions are constant, the vibration deflec-
tion displacements occupy the entire shell surface. If the
determining functions vary from point to point of the
neutral surface then localization of the vibration modes
lies near the weakest lines on the shell surface which are
less stiff. In general, for this class of shells, numerical or
approximate techniques are necessary for their analysis.
In some practical applications, these shells are laid on a
soil medium as the foundation, and more attention paid
to the analysis of the shell’s behavior embedded in soil
simulated with two elastic parameters through the
Winkler-Pasternak model. Hereby, there are a few
researchers interested in the study of vibration behavior
of homogeneous, isotropic and orthotropic circular
cylindrical shells of uniform thickness under elastic
foundations (Paliwal and Bhalla, 1993a,b; Paliwal and
Srivastava, 1994; Paliwal et al., 1996; Paliwal and
Pandey, 1998; Gunawan et al., 2004, 2006; Golovko
et al., 2007) and their studies are conducted for the
vibration behavior of isotropic cylindrical shells on
the Winkler and Pastemak-type foundations. Whereas
Department of Mathematics, Faculty of Science at Qena, South Valley
University, Egypt
Corresponding author:
Mousa Khalifa Ahmed, Department of Mathematics, Faculty of Science at
Qena, South Valley University, Egypt.
Email: mossa@dr.com
Received: 9 December 2013; accepted: 31 January 2014
Journal of Vibration and Control
2016, Vol. 22(1) 37–50
!The Author(s) 2014
Reprints and permissions:
sagepub.co.uk/journalsPermissions.nav
DOI: 10.1177/1077546314528229
jvc.sagepub.com
by guest on December 31, 2015jvc.sagepub.comDownloaded from
... The natural frequency of finite Timoshenko beams on Pasternak foundations has been analyzed with six cases of bounding conditions [1]. M. K. Ahmed has studied the natural frequencies and mode shapes of a variable thickness elastic cylindrical shell, resting on Pasternak foundation using transfer matrix [2]. D. N. Paliwal and R. Pandey studied the free vibration of an orthotropic thin cylindrical shell on a Pasternak foundation [3]. ...
... The springs are assumed to have pure displacement, they are fully independent, with no integration and coupling effect with each other. The simple and normal response of the foundation to load p(x,y) can be written as; 2 ( , ) p x y Kw G w    ...
... Using the Fourier transformation and the Adomian methods, the vibrations of endless Timoshenko beams supported by a cubic elastic base subjected to a moving load has been studied by [31]. The dynamics of the shells on a Pasternak foundation has been studied by [32] using matrix transformation method. Using Galerkin and superposition methods, the bending of composite shells on a Pasternak foundation due to an external pressure and axial compression has been analysed by [33]. ...
... In order to confirm, the fundamental frequencies obtained by applying this method to an FGM beam studied in the literature [49,66] are given in Table 1. Where, the fundamental frequency parameter (32) of the FGM beam is obtained using TBT (FSDBT2 in [66] for Alumina and Aluminium with the following material properties: ...
Article
Full-text available
This study presents a four-parameter linear basis model to analyse and control the dynamic response of an FGM Timoshenko beam exposed to the accelerating / decelerating mass using the finite element method. The dynamic effects of the foundation's mass and damping are taken into account and the foundation is assumed to consist of four parts: mass, spring, viscous damper and shear layer. Considering the actual physical neutral axis, the combined motion equations of the FGM beammass- base-base system are obtained by combining terms of first order shear deformation (FSDT) and mass and base interactions. In view of the resulting high-speed motion and acceleration conditions of the moving mass, some new findings are presented for both the moving load and the moving mass assumptions to highlight the differences that may be useful in the analysis of new high-speed transport applications today. Due to their effects, the frequency change of the FGM Timoshenko beam-base system is emphasized to show the main cause of the changes.
... Recently, scientists employed different methods and theories to study the dynamic behavior of those shells. Ahmed [1] studied the vibration of an elastic oval cylindrical shell with parabolically varying thickness and along of its circumference surrounded by Pasternak foundations based on the framework of the Flügge's shell theory, the transfer matrix approach and the Romberg integration method. Qu et al. used a Domain Decomposition Method (DDM) to evaluate the vibration of stepped circular cylindrical and conical shells [2] and laminated orthotropic conical shells on Pasternak foundation [3]. ...
Article
Full-text available
This research presents a continuous element model for solving vibration problems of stepped composite cylindrical shells surrounded by Pasternak foundations with various boundary conditions. Based on the First Order Shear Deformation Theory (FSDT), the equations of motion of the circular cylindrical shell are introduced and the dynamic stiffness matrix is obtained for each segment of the uniform shell. The interesting assembly procedure of continuous element method (CEM) is adopted to analyze the dynamic behavior of the stepped composite cylindrical shell surrounded by an elastic foundation. Free vibrations and harmonic responses of different configurations of stepped composite cylindrical shells on elastic foundations are examined. Effects of structural parameters, stepped thickness and elastic foundations on the free vibration responses of stepped composite cylindrical shells are also presented. Comparisons with previously published results and finite element (FE) analyses show that the proposed technique saves data storage volume and calculating time, and is accurate and efficient for widening the studied frequency range.
... Численными экспериментами установлено [28], что для указанной конфигурации 25 прямых обеспечивают вычисление собственных частот с подходящей точностью и приемлемой вычислительной эффективностью. Для отображения полученных результатов используются безразмерные параметры частоты Ω, коэффициентов постели , [29] и уровня жидкости : Т а б л и ц а 1. Сравнение собственных частот колебаний (рад/с) свободно опёртой (SS) цилиндрической оболочки, частично заполненной жидкостью: = 4, = 0, = 0.72 / Table 1 Comparison of natural frequencies of vibrations (rad/s) of a simply supported (SS) cylindrical shell partially filled with fluid: = 4, = 0, = 0.72 ...
Article
Full-text available
The paper presents the results of studies on natural vibrations of circular vertical cylindrical shells completely or partially filled with a stationary compressible fluid and embedded in a Pasternak two-parameter elastic foundation. In the meridional direction, the elastic medium is both homogeneous and inhomogeneous, and is an alternation of areas, in which this medium is present or absent. The behavior of the elastic structure and compressible fluid is described within the framework of classical shell theory based on the Kirchhoff-Love hypotheses and the Euler equations. The equations of motion of the shell together with the corresponding geometric and physical relations are reduced to a system of ordinary differential equations with respect to new unknowns. The acoustic wave equation is also reduced to a system of ordinary differential equations using the straight line method. The formulated boundary value problem is solved by the Godunov orthogonal sweep method involving the numerical integration of differential equations by the fourth order Runge-Kutta method. The natural frequencies of vibrations are calculated using a combination of stepwise procedure and subsequent refinement by the half-division method. The validity of the results obtained is confirmed by comparing them with the known numerical-analytical solutions. The dependences of minimum vibration frequencies on the level of fluid are analyzed for simply supported, clamped and cantilevered cylindrical shells at the change in the foundation heterogeneity along the structure length and different stiffness. It is demonstrated that with increase in the level of filling of shells with fluid, the influence of the elastic foundation on the frequency spectrum of the structure decreases.
... In recent years, numerous studies have been conducted on the free and steady vibration of cylindrical shell, including Ritz method, 1-4¯n ite element method (FEM), 5 transfer matrix method, 6,7 dynamic sti®ness method. [8][9][10] and di®erential quadrature method (DQM), 11,12 etc. Considering the in°uence of aspect ratio, number of modes and thermal environment, Ebrahimi et al. 13 investigated the thermal buckling and forced vibration behaviors of the cylindrical shell by using Hamilton's principle. ...
Article
Full-text available
In this paper, the experimental and Jacobi–Ritz method (JRM) have been adopted to analyze the forced vibration analysis of uniform and stepped circular cylindrical shells with general boundary conditions. The simply supported cylindrical shell at both ends is taken as an experimental model, and the free, steady and transient vibration characteristics of structures under hammer and fixed exciter are recorded. The results show that the results of JRM are in sensible agreement with those in experiment. In addition, the results for various boundary conditions, structural parameter are also presented. On this basis, the Newmark-β integration method is adopted to realize the time domain solutions for transient vibration response, and the frequency domain results can be obtained by using Fourier transformations from time domain results. Finally, the line spectrum vibration response results of the structure are presented under the random excitation load, and the research can supply technical support for the vibration control of cylindrical shell structure.
... It was demonstrated in Ref. 6 that the presence of an elastic medium (Winkler model) significantly increases the frequencies of radial vibrations of three-layered shells with thick layers of a filling material. Analysis of isotropic and orthotropic shells with thicknesses variable in the circumferential direction is presented in Ref. 7. It follows from the above results that an increase in the ratio of the maximum thickness to the minimum thickness enhances the influence of the elastic foundation. ...
Article
Full-text available
This paper presents the results of studies on natural vibrations of circular cylindrical shells containing liquid and resting on an elastic foundation, which is described by the Pasternak two-parameter model. In the meridional direction, the elastic medium is nonuniform and represents an alternation of sections in which the foundation is present or absent. The behavior of the elastic structure and the compressible fluid is described in the framework of classical shell theory based on the Kirchhoff–Love hypothesis and the Euler equations. The equations of motion of the shell are reduced to a system of ordinary differential equations with respect to new unknowns. The wave equation written for pressure in the fluid also reduces to a system of ordinary differential equations using the straight line method. The solution of the formulated boundary value problem is found by the Godunov orthogonal sweep method. The validity of the results obtained is confirmed by comparison with the known numerical-analytical solutions. The dependences of the minimum vibration frequencies on the characteristics of elastic medium with variable nonuniformity along the length of the structure have been obtained for cylindrical shells with different boundary conditions. It has been found that the violation of smoothness of the derived dependences is caused by a change of the vibration mode with minimum frequency and is determined both by the ratio of the size of the elastic foundation to the entire length of the shell and its stiffness, and also by a combination of boundary conditions set at the edges of the thin-walled structure.
Article
In recent years, magneto-electro-elastic (MEE) cylindrical shells with stepwise thicknesses have shown significant potential in the field of vibration energy harvesting. To aid the design of such energy harvesting devices, an accurate free vibration analysis of embedded MEE cylindrical shells with step-wise thicknesses is performed within the framework of symplectic mechanics. By using the Legendre transformation, a new known vector is defined to transform the higher-order partial differential governing equations into a set of lower-order ordinary differential equations. Therefore, the original vibration analysis is regarded as an eigen problem in the symplectic space, and analytical solutions can be represented by the symplectic series. In numerical examples, the new analytical solutions are compared with the existing results, and good agreement is observed. Furthermore, the effects of critical design parameters on free vibration characteristics are thoroughly investigated. All numerical results can serve as benchmarks for the development of other approximate or numerical methods.
Article
Full-text available
For launching devices and equipment (payload) into orbit they are usually placed in a foam package made of various polymeric materials. One of the functions of the foam package is to prevent low-frequency vibrations of the payload. In this connection, the problem of determining the natural frequencies of vibrations of the “payload – foam package” system is relevant. These frequencies depend on the physical-mechanical properties and the size of the foam package, the mass and size of the payload. The paper presents the results of an experimental determination of the stiffness characteristics of the foam package materials and a computational analysis of the natural frequencies of the “payload – foam package” system.
Article
Full-text available
In this paper an analytical procedure is given to study the free vibration characteristics of laminated non-homogeneous orthotropic thin circular cylindrical shells resting on elastic foundation, accounting for Karman type geometric non-linearity. At first, the basic relations and modified Donnell type stability equations, considering finite deformations, have been obtained for laminated thin orthotropic circular cylindrical shells, the Young's moduli of which varies piecewise continuously in the thickness direction. Applying Galerkin method to the latter equations, a non-linear time dependent differential equation is obtained for the displacement amplitude. The frequency is obtained from this equation as a function of the shell displacement amplitude. Finally, the effect of elastic foundation, non-linearity, non-homogeneity, the number and ordering of layers on the frequency is found for different mode numbers. These results are given in the form of tables and figures. The present analysis is validated by comparing results with those in the literature.
Article
Full-text available
A new vibration behavior is presented for an elastic oval cylindrical shell having circumferentially variable thickness with complex radius of curvature of an isotropic and orthotropic material. Based on the framework of the Flügge’s shell theory, the transfer matrix approach and the Romberg integration method, the governing equations of motion that have variable coefficients are formulated and solved. The analysis is formulated to overcome the mathematical difficulties related to mode coupling which comes from variable curvature and thickness of shell. The vibration equations of the shell are reduced to eight first-order differential equations in the circumferential coordinate, and by using the transfer matrix of the shell, these equations can be written in a matrix differential equation. The proposed model is adopted to get the vibration frequencies and the corresponding mode shapes for symmetric and anti-symmetric modes of vibration. The sensitivity of the frequency parameters and the bending deformations to the shell geometry, ovality parameter, thickness ratio, and orthotropic parameters corresponding to different types of vibration modes of shells is investigated.
Article
The present paper contains a critical study of a number of foundation models as well as a further development of some of the ideas involved. Among others it is shown that the Pasternak foundation is a mechanical model for the so-called “generalized” foundation. It is also demonstrated that the kernel for the Pasternak foundation in plane stress or plane strain is identical with Wieghardt’s exponential kernel, and that for the three-dimensional case the kernel is a modified Bessel function. It is also shown that the “non solvability” of the problem of a finite beam or plate resting on a continuous foundation as posed by Wieghardt and further elaborated by Pflanz is not correct, and that problems of this type are solvable for any load distribution permissible in classical plate theory. Throughout the paper, emphasis is placed on the proper mathematical formulation of the physical problems in question.
Article
Free vibrations of a thin circular-cylindrical shell in contact with an elastic medium are investigated, employing membrane theory. Response of the elastic medium is represented by Winkler/Pasternak models. Dynamic characteristics involving nondimensional frequency parameters and axial wave parameters are drawn. It is found that the value of the foundation modulus (K), considerably affects radial vibrational mode frequency, while the other two vibrational mode frequencies, i.e. torsional and longitudinal, remain almost unaffected. It is found also that the influence of the nondimensional shear modulus parameter (Ḡ), is more pronounced in radial vibrational mode frequencies, to a lesser extent on torsional mode frequencies and least on longitudinal mode frequencies.