Research Article  Open Access
Wanyou Li, Gang Wang, Jingtao Du, "Vibration Analysis of Conical Shells by the Improved Fourier ExpansionBased Differential Quadrature Method", Shock and Vibration, vol. 2016, Article ID 9617957, 10 pages, 2016. https://doi.org/10.1155/2016/9617957
Vibration Analysis of Conical Shells by the Improved Fourier ExpansionBased Differential Quadrature Method
Abstract
An improved Fourier expansionbased differential quadrature (DQ) algorithm is proposed to study the free vibration behavior of truncated conical shells with different boundary conditions. The original function is expressed as the Fourier cosine series combined with closeform auxiliary functions. Those auxiliary functions are introduced to ensure and accelerate the convergence of series expansion. The grid points are uniformly distributed along the space. The weighting coefficients in the DQ method are easily obtained by the inverse of the coefficient matrix. The derivatives in both the governing equations and the boundaries are discretized by the DQ method. Natural frequencies and modal shapes can be easily obtained by solving the numerical eigenvalue equations. The accuracy and stability of this proposed method are validated against the results in the literature and a very good agreement is observed. The centrosymmetric properties of these newly proposed weighting coefficients are also validated. Studies on the effects of semivertex angle and the ratio of length to radius are reported.
1. Introduction
Conical shells are widely used in various engineering fields, such as aerospace and ship industries. The development of accurate shell theories has been the subject of significant research interest for many years, and a large number of shell theories based on different approximations and assumptions have been proposed. However, more work is focused on the vibration of cylindrical shells compared with the conical shell. Since the conical coordinate system is function of the meridional direction, the equations of motion for conical shells consist of a set of partial differential equations with variable coefficients. Current methods for the free vibration analysis of thin conical shells can be classified as to analytical methods and numerical methods. Saunders et al. [1], Garnet and Kempner [2], Siu [3], and Lim and Liew [4] have studied the free vibration of uniform conical shells by RayleighRitz method. Ueda [5] analyzed the same problems using the finite element method. Irie et al. [6] studied a conical shell with variable thickness by the transfer matrix method. The DQ method was employed to analyze the free vibration of a uniform conical shell [7]. Jin et al. [8] studied the free and forced vibration of conical shell using the improved Fourier series method by considering the general boundary conditions. The kernel particle (kp) functions were employed in hybridized form with harmonic functions to study the vibration of the conical shell based on Ritz method [9].
Besides the studies of the isotropic conical shells, laminated and functional graded conical shells have also been fully studied by various methods [10–16]. The differential quadrature (DQ) method was adopted to solve the differential governing equations of the conical shell in those researches [10–13]. For the vibration of the rotating conical shell, in which the centrifuge force should be taken into consideration, the DQ method was also extensively used to study those problems [10, 17]. The reason that the DQ method is widely adopted to study the vibration behavior of the conical shell is the convenience of transforming the partial differential governing equations approximately into a set of linear algebraic governing equations. Imposing the given boundary conditions, the numerical eigenvalue equations for the free vibration of the (rotating or composite) conical shell are derived and solved.
The differential quadrature method is a numerical technique for solving the differential equations. It was first developed by Bellman et al. [18, 19] and their associates in the early 1970s. The DQ method, akin to the conventional integral quadrature method, approximates the derivative of a function at any location by a linear summation of all the functional values along a mesh line. The key procedure in the DQ method applications lies in the determination of the weighting coefficients. Shu [7, 12, 20, 21] proposed two types of weighting coefficients obtained by the polynomials and the truncated Fourier series, among which the Lagrange interpolation functions are widely used for their simplicity explicitness [7, 21]. Although it is well known that Lagrange interpolation functions are limited by the number of interpolation points and severe oscillation may take place if the order is large, the use of the GaussChebyshev points [7, 21] can accelerate the convergence rate of the DQ method. Some works focusing on improving the accuracy and stability of the DQ method are presented by proposing different ways to generate the weighting coefficients and to determine the distribution of grid points [22–24].
The Fourier series with auxiliary functions was first proposed by Li [25] to study the vibration problems of the beam structure. This method is extensively used to study the 2D and 3D structural vibration and vibroacoustic problems [26–30]. The auxiliary functions are introduced to accelerate the convergence and deal with all the possible discontinuities, at the end points or edges, associated with the original Fourier cosine series. This improved Fourier series method becomes a promising method to study the structural vibration problems.
In this paper, the improved Fourier expansionbased differential quadrature method is proposed to solve the free vibration behavior of the truncated conical shell. The weighting coefficients are obtained based on this improved Fourier series in a much easier way. The centrosymmetric properties of these newly proposed weighting coefficients are also validated. The following sections will illustrate the development of this hybrid method, and numerical results are then presented to validate the effectiveness, accuracy, and stability of this current method on predicting the modal characteristics of the conical shell.
2. Theoretical Formulation
For a continuous function defined on with an absolutely integrable derivative, it can be expanded in Fourier cosine series:
The firstorder derivative of can be done termbyterm:
The secondorder derivative of cannot be obtained termbyterm, which is shown as
These formulations basically tell that while a cosine series can always be differentiated termbyterm, this can be done to a sine series only if . To implement the differential quadrature algorithm, the auxiliary functions are added to traditional Fourier cosine series to cover the discontinuity of the function at the end points and to get the derivatives termbyterm. A function can be expanded as [27]wherewhere and represent the unknown Fourier expansion coefficients. The supplementary functions can be represented as arbitrary continuous functions, regardless of the boundaries. It is easy to verify that and all the other 1storder and 3rdorder derivatives are identically equal to zero at both ends. The main purpose of introducing these supplementary functions to standard Fourier series is to get the first four derivatives of the Fourier cosine series termbyterm. As an immediate numerical benefit, the Fourier series in (4) will converge uniformly at an accelerated rate.
To implement the differential quadrature method, points are equally distributed on :
The functional values at those grid points can be determined as
The Fourier series is truncated to . Rewrite (7) into the matrix form
The Fourier series coefficients can be obtained by the inverse of the matrixin which
In this proposed method, the number of truncated Fourier series and the number of grid points follow the relation that to ensure is a square matrix to let the inverse be more accurate. Once the constant matrix is determined, the approximated Fourier series coefficients are obtained. When the DQ method was first developed, polynomials were adopted to follow this procedure to generate weighting coefficients which would lead to highly ill condition when is large. The Fourier series, however, show much more stability to derive the coefficients by the inversion of which will be validated in the results section.
The firstorder derivatives at those grid points are
Rewrite (11) into the matrix form, in which is the firstorder derivative of and is the firstorder weighting coefficient matrix of the DQ method: . It is obvious from the above equation that the weighting coefficients of the second and higherorder derivatives can be completely determined through the same way, which are expressed as in which () is the thorder derivative of and is the thorder weighting coefficient matrix of the DQ method: .
In this paper, only four supplementary functions are added to the Fourier cosine series, which will ensure the firstfourorder derivatives to converge at a high rate and to keep stability of the Fourier series. Consequently firstfourorder weighting coefficient matrixes can be obtained which are sufficiently enough to study the vibration of a conical shell. Adding more supplementary functions to the Fourier cosine series will give the capability to study the corresponding higherorder partial differential equations.
3. Free Vibration Behavior of a Conical Shell
The free vibration behavior of conical shells has been studied by Shu [7] by the DQ method. This model is adopted again to validate the efficiency, accuracy, and stability of this proposed method.
Consider a conical shell structure with semivertex angle and the radius of the large edge is , as shown in Figure 1. The displacement fields of the conical shell in , , and directions are denoted by , , and , respectively. If the couplings between these three displacement components are ignored, the field functions can be expressed asin which and are the circumferential wave number and the frequency in rad/sec, respectively.
The differential governing equations of the conical shell based upon Flügge theory are written asin which and denote the density of the shell and the shell thickness, respectively. The differential operators () can be referred to [7].
Substituting (14) into (15) and applying (13), then where represents the weighting coefficients, .
The boundary conditions for the conical shell are as follows: simplesupported boundary condition (S): clamped boundary condition (C):
The boundary conditions can also be expressed in the differential forms by substituting (13) into them. Simple supported condition at the small edge is chosen as an example:
Other boundary conditions can also be formulated in similar forms. Those four boundary formulations are applied at the grid points of . Rewrite (16a), (16b), (16c), (19a), (19b), (19c), (19d), and boundary conditions into the matrix formwhere , is a matrix with the dimension of , and
It is clear from (20) that the natural frequencies and modal shapes for the conical shell can now be directly obtained by solving the standard matrix eigenvalue problem. The natural frequency parameter is defined as
4. Numerical Results and Discussion
4.1. Convergence Study
To study the convergence of this proposed method, different numbers of grid points or truncated Fourier series () are selected. The geometric and material parameters of the conical shell are Young’s modulus 0 GPa, Poisson’s ratio , kg/m^{3}, , = 45°, and . The effect of the number of grid points that affects the natural frequencies is studied. The results derived by finite element method (FEM) are adopted to compare with those obtained by this method. Figure 2 shows the natural frequency parameters under SS boundary conditions when the circumferential wave number is and axial number is . Figure 3 shows the natural frequency parameter under SC boundary condition when the circumferential wave number is and axial number is . By comparing the results derived by this method and FEM, the fast convergence behavior and high stability of this method are observed. The natural frequency parameters keep stable even with a large number of grid points. In the following calculation, the number of grid points will be chosen as .
4.2. Validation of This Proposed Method
To validate the accuracy of the present method, an example reported by Irie et al. [6] and Shu [7] is adopted again. Shu [7] studied the free vibration behavior of this problem by the DQ method, in which Lagrange interpolation functions and GaussChebyshev points are employed. The geometric parameters are , , and . Table 1 shows the comparison between current natural frequency parameters and results studied by Irie et al. [6] and Shu [7] for the conical shells with CC, SS, FC, and FS boundary conditions. The small discrepancies show a good agreement. Figures 4 and 5 show some selected modal shapes of the conical shell with different parameters.

(a) ,
(b) ,
(c) ,
(a) ,
(b) ,
(c) ,
4.3. Effects of the Auxiliary Functions
To study the advantage of introducing the auxiliary functions, the weighting coefficients obtained without auxiliary functions are adopted to study the eigenvalue problems. The constant matrix without the auxiliary functions can be rewritten as
The weighting coefficient matrix is then derived in the same way as (13):in which is the thorder weighting coefficient matrix and is the thorder derivative of . By using this type of weighting coefficients, natural frequency parameters are derived again to compare with the results obtained before. Table 2 shows the frequency comparison between the results derived by these two types of weighting coefficients. The number of grid points is chosen as . It is clear that the introduction of auxiliary functions will improve the accuracy of this method.

4.4. Relation between the Numbers of Truncated Fourier Series and Grid Points
For the study above, the numbers of truncated Fourier series and grid points follow the relation that to ensure that is a square matrix. It is well known that pseudoinverse of could also be adopted to derive weighting coefficients even when . Figure 6 shows the natural frequency parameters when is set to and . It is clear that only if , that is, , the accurate results could be obtained. To implement this method, the relation between the numbers of truncated Fourier series and grid points should be strictly set to .
(a) CC
(b) FS
4.5. The Centrosymmetric Properties of the Weighting Coefficients
When DQ method was developed, the centrosymmetric and skew centrosymmetric properties were observed shown as [21]
Equation (25) shows that the DQ weighting coefficient matrix is skew centrosymmetric for odd derivatives ( is odd) and centrosymmetric for even order derivatives ( is even) when the grid distribution is symmetric with respect to the center point. This conclusion is true for both uniform and nonuniform grids.
In this proposed method, the centrosymmetric properties are also validated. Two types of weighting coefficients calculated in different ways are employed to study the eigenvalue problems; those are
To implement (27), is first derived based on (26). Table 3 shows the natural frequency parameters obtained by these two types of weighting coefficients. The small discrepancies between these two results show a good agreement. It is concluded that the weighting coefficient matrix derived by this proposed method also obeys the centrosymmetric property.
4.6. Effects of Geometric Parameters
The geometric parameters play an important role in affecting the natural frequencies of a conical shell. In this part, two parameters are studied to study their effects on the free vibration behavior of the conical shells. Figure 7 shows the natural frequency parameters changing with variable ratio of length to radius of the conical shell under CC and FC boundary conditions. The geometric parameters are chosen as , , and variable . The frequency parameters nearly keep constant when as increasing the ratio of length to radius. The frequency parameters decrease when , except for the case of for FC boundary conditions. Next, the effect of semivertex angle is studied with the geometric parameters , , and variable semivertex angle = 30°–90°. Figure 8 shows the natural frequency parameters of different circumferential wave numbers. As semivertex angle increasing to 90°, the frequencies converge to one value. This phenomenon can be explained by the fact that the conical shell degenerates to a circular plate when semivertex angle is 90°.
(a)
(b)
(a)
(b)
5. Conclusions
In this paper, a new method is proposed to generate the weighting coefficients of the DQ method. The functions in the DQ method are expressed as the Fourier cosine series combined with closeform auxiliary functions. The weighting coefficients are directly derived by the inverse of the constant matrix which presents a much easier way. The boundary conditions and differential governing equations are discretized to form the numerical eigenvalue equations. The results obtained by this method are compared with those available in the literature and a good agreement is observed. The centrosymmetric properties of these newly proposed weighting coefficients are also validated. By increasing the number of grid points, the efficiency and high stability are presented in this method. The effect of those parameters which may affect the dynamic characteristics of the shell is also studied.
This method gives a much easier way to generate weighting coefficients in DQ algorithm. It can also be extended to study higherorder partial differential equations just by adding more corresponding supplementary functions to the Fourier cosine series.
Conflict of Interests
The authors declare that there is no conflict of interests regarding the publication of this paper.
Acknowledgments
The research work is supported by the National Natural Science Foundation of China (Grant no. 51375104) and Heilongjiang Province Funds for Distinguished Young Scientists (Grant no. JC 201405).
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Copyright © 2016 Wanyou Li et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.