Advances in Acoustics and Vibration

Advances in Acoustics and Vibration / 2010 / Article

Research Article | Open Access

Volume 2010 |Article ID 501902 | https://doi.org/10.1155/2010/501902

S. Bashmal, R. Bhat, S. Rakheja, "Frequency Equations for the In-Plane Vibration of Circular Annular Disks", Advances in Acoustics and Vibration, vol. 2010, Article ID 501902, 8 pages, 2010. https://doi.org/10.1155/2010/501902

Frequency Equations for the In-Plane Vibration of Circular Annular Disks

Academic Editor: Miguel Ayala Botto
Received23 Oct 2009
Revised23 Jun 2010
Accepted25 Jun 2010
Published13 Sep 2010

Abstract

This paper deals with the in-plane vibration of circular annular disks under combinations of different boundary conditions at the inner and outer edges. The in-plane free vibration of an elastic and isotropic disk is studied on the basis of the two-dimensional linear plane stress theory of elasticity. The exact solution of the in-plane equation of equilibrium of annular disk is attainable, in terms of Bessel functions, for uniform boundary conditions. The frequency equations for different modes can be obtained from the general solutions by applying the appropriate boundary conditions at the inner and outer edges. The presented frequency equations provide the frequency parameters for the required number of modes for a wide range of radius ratios and Poisson's ratios of annular disks under clamped, free, or flexible boundary conditions. Simplified forms of frequency equations are presented for solid disks and axisymmetric modes of annular disks. Frequency parameters are computed and compared with those available in literature. The frequency equations can be used as a reference to assess the accuracy of approximate methods.

1. Introduction

The out-of-plane vibration properties of circular disks subjected to a variety of boundary conditions have been extensively investigated (e.g., [14]). The in-plane vibration analyses of circular disk, however, have been gaining increasing attention only in the recent years. Much of the interest could be attributed to important significance of the in-plane vibration in various practical problems such as the vibration of railway wheels, disk brakes, and hard disk drives contributing to noise and structural vibration [57].

The in-plane vibration of circular disks was first attempted by Love [8] who formulated the equations of motion for a thin solid circular disk with free outer edge together with the general solution. The equations of motion were subsequently solved by Onoe [9] to obtain the exact frequency equations corresponding to different modes of a solid disk with free outer edge. Holland [10] evaluated the frequency parameters and the corresponding mode shapes for a wide range of Poisson’s ratios and the vibration response to an in-plane force. The in-plane vibration characteristics of solid disks clamped at the outer edge have been investigated in a few recent studies. Farag and Pan [11] evaluated the frequency parameters and the mode shapes of in-plane vibration of solid disks clamped at the outer edge using assumed deflection modes in terms of trigonometric and Bessel functions. Park [12] studied the exact frequency equation for the solid disk clamped at the outer edge.

The in-plane vibration analyses in the above reported studies were limited to solid disks with either free or clamped outer edge. The in-plane free vibration of annular disks with different boundary conditions has also been addressed in a few studies. The variations in the in-plane vibration frequency parameters of annular disks with free edges were investigated as function of the size of the opening by Ambati et al. [13]. The variation ranged from a solid disk to a thin ring, while the validity of the analytical results was demonstrated using the experimental data. Another study investigated the free vibration and dynamic response characteristics of an annular disk with clamped inner boundary and a concentrated radial force applied at the outer boundary [14]. Irie et al. [15] investigated the modal characteristics of in-plane vibration of annular disks using transfer matrix formulation while considering free and clamped inner and outer edges.

The above reported studies on in-plane vibration of solid and annular disks have employed different methods of analyses. The finite-element technique has also been used to examine the validity of analytical methods (e.g., [11, 14]). The exact frequency equations of in-plane vibration, however, have been limited only to solid disks. Such analyses for the annular disks pose more complexities due to presence of different combinations of boundary conditions at the inner and outer edges. This study aims at generalized formulation for in-plane vibration analyses of circular annular disks under different combinations of clamped, free, or flexible boundary conditions at the inner and outer edges. The equations of motion are solved for the general case of annular disks. The exact frequency equations are presented for different combinations of boundary conditions, including the flexible boundaries, for various radius ratios, while the solid disk is considered as special cases of the generalized formulation.

2. Theory

The equations of the in-plane vibration of a circular disk are formulated for an annular disk shown in Figure 1. The disk is considered to be elastic with thickness h, outer radius b and inner radius a. The material is assumed to be isotropic with mass density ρ, Young's modulus and Poisson ratio v. The equations of dynamic equilibrium in terms of in-plane displacements along the radial and circumferential directions can be found in many reported studies (e.g., [11, 16]). These equations of motion in the polar coordinate system can be written as where ur and uθ are the radial and circumferential displacements, respectively, along the r and θ directions, and .

Following Love’s theory [8], the radial and circumferential displacements can be expressed in terms of the Lamé Potentials and [17], as where

Assuming harmonic oscillations corresponding to a natural frequency ω, the potential functions and can be represented by where n is the circumferential wave number or nodal diameter number. Upon substituting for and in terms of , and from (2) to (5), in (1), the equations of motion reduce to the following uncoupled form: where and are nondimensional frequency parameters defined as

Equations (6) and (7) are the parametric Bessel equations and their general solutions are attainable in terms of the Bessel functions as [18] where are the Bessel functions of the first and second kind of order n, respectively, and and are the deflection coefficients.

The radial and circumferential displacements can then be expressed in terms of the Bessel functions by substituting for and in (2) and (3). The resulting expressions for the radial and circumferential displacements can be expressed as: where

2.1. Free and Clamped Boundary Conditions

Equations (11) represent the solutions for distributions of the radial and circumferential displacements for the general case of an annular disk. The evaluations of the natural frequencies and arbitrary deflection coefficients ( and ), however, necessitate the consideration of the in-plane free vibration response under different combinations of boundary conditions at the inner and the outer edges. For the annular disk clamped at the outer edge (), the application of boundary conditions ( and ) must satisfy the following for the general solutions (11):

In a similar manner, the solution must satisfy the following for the clamped inner edge (), where is the radius ratio between inner and outer radii of the disk: The conditions involving at the free edges are satisfied when the radial () and circumferential () in-plane forces at the edge are zero [11], such that A direct substitution of and from (11) in the above equations would result in second derivatives of the Bessel functions. Alternatively, the above equation for the boundary conditions may be expressed in terms of and through direct substitution of and from (2) and (3), respectively. The boundary conditions in terms of Nr can thus be obtained as Rearranging (19) results in The second order derivative term in (20) can be eliminated by adding and subtracting the term , which yields From (6), it can be seen that the terms within the first parenthesis are identically equal to zero. Equation (21) describing the boundary condition associated with can be further simplified upon substitutions for , which yields Similarly, the boundary condition equation associated with (18) can be simplified as Upon substitutions for and from (16) in (26) and (27), the boundary condition equations for the free edges are obtained, which involve only first derivatives of the Bessel functions. For an annular disk with free inner and outer edges, (22) and (23) represent the conditions at both the inner and the outer boundaries ( and ). The equations for the free edge boundary conditions can be expressed in the matrix form in the four deflection coefficients, as The determinant of the above matrix yields the frequency equation for the annular disk with free inner and outer edge conditions.

For the clamped inner and outer edges, the equations for the boundary conditions can be obtained directly from (13) to (16), such that In the above equations, (24) and (25), the top two rows describe the boundary condition at the outer edge, while the bottom two rows are associated with those at the inner edge. The equations for the boundary conditions involving combinations of free and clamped edges can thus be directly obtained from the above two equations. For the free inner edge and clamped outer edge, denoted as “free-clamped” condition, the matrix equation comprises the tip two rows of the matrix in (25) and the lower two rows from (24). For the clamped inner edge and free outer edge, denoted as “Clamped-Free” condition, the matrix equation is formulated in the similar manner using the lower and upper two rows from (25) and (24), respectively.

The in-plane vibration analysis of a solid disk can be shown as a special case of the above generalized formulations. Upon eliminating the coefficients associated with Bessel function of the second kind, Equations (24) and (25) reduce to those reported by Onoe [9] for free solid disk and by Park [12] for the clamped solid disk. The frequency equation corresponding to different values of n for the solid disks involving the two boundary conditions are summarized in Table 1, where is the derivative of the Bessel function evaluated at the outer edge (). For annular disks, simplified frequency equations can be obtained for the axisymmetric modes. These equations where expressed in Table 2 for the four combinations of boundary conditions.


Boundary conditions at ClampedFree

Radial =0
Circumferential =0
( ) ( ) = ( ) ( )
where


Boundary conditionsradialCircumferential
innerouter

ClampedClamped

FreeFree

ClampedFree

FreeClamped

2.2. Flexible Boundary Conditions

In the above analysis, the boundary conditions considered are either clamped or free. However, Flexible boundary conditions may be considered more representative of many practical situations. The proposed formulations can be further employed to study the in-plane vibration of solid as well as annular disks with flexible boundary conditions. Artificial springs may be applied to describe the flexible boundary conditions at the inner or the outer edge of an annular disk. A number of studies on the analysis of out-of-plane vibration characteristics of circular plates and cylindrical shells have employed uniformly distributed artificial springs around the edge to represent a flexible boundary conditions or a flexible joint [1922].

The effects of flexible boundary conditions on the in-plane free vibration of circular disks have been considered in a recent study by the authors [23] using the Rayleigh-Ritz approach. Artificial springs, distributed along the radial and circumferential directions at the free outer and/or inner edges, were considered to simulate for flexible boundary conditions. The exact solution of the frequency equations for the disk with flexible supports can be attained from (11) together with the consideration of the flexible boundary conditions. The conditions involving flexible edge supports at the inner and outer edges are satisfied when the radial () and circumferential () in-plane forces at the edges are equal to the respective radial and circumferential spring forces, such that where and are the radial and circumferential stiffness coefficients, respectively. Introducing the nondimensional stiffness parameters, and , (26) can be written as The application of the above conditions yields the matrix equations for the disk with flexible supports at the inner and outer edges, similar to (24). The frequency parameters are subsequently obtained through solution of the matrix equations. The above boundary equations reduce to those in (22) and (23) for the free edge conditions by letting and . Furthermore, the clamped edge condition can be represented by considering infinite values of and . Equations (27) further show that the flexible edge support conditions involve combinations of the free and clamped edge conditions.

3. Results

The frequency parameters () derived for different combinations of boundary conditions are compared with those reported in different studies to demonstrate the validity of the proposed formulation. For this purpose, the frequency parameters of a solid disk with free and clamped outer edge are initially evaluated and compared with those reported by Holland [10] and Park [12], respectively. The results presented in Tables 3 and 4 for the free and clamped outer edge conditions, respectively, were found to be identical to those reported in [10, 12] for solid disks with clamped edge.


Mode

11.61761.38772.13042.7740
23.52912.51123.45174.4008
34.04744.52085.34926.1396
45.88615.20296.36957.4633
56.91136.75497.61868.5007
67.79808.26399.347010.2350
79.65948.73429.836611.0551


Mode

11.94413.01853.01854.7021
23.11264.01274.01275.8985
34.91045.73985.73987.3648
45.35706.70796.70798.9816
56.77637.64427.64429.5296
68.49389.43569.435611.1087
78.64589.98949.989412.5940

The exact frequency parameters for the annular disks were subsequently obtained under different combinations of boundary conditions at the inner and outer edges. The edge conditions are presented for the inner followed by that of the outer edge. For instance, a “Free-Clamped” condition refers to free inner edge and clamped outer edge. The solutions obtained for conditions involving free and clamped edges (“Free-Free”, “Free-Clamped”, “Clamped-Clamped”, and “Clamped-Free”) are compared with those reported by Irie et al. [15] in Tables 5, 7, 8, 9, respectively. The simulations results were obtained for two different values of the radial ratios ( and 0.4), and . The results show excellent agreements of the values obtained in the present study with those reported in [15], irrespective of the boundary condition and radius ratio considered.


Radius ratio (β)
Reference [15]present studyReference [15]Present studyReference [15]Present studyReference [15]Present study

0.21.6521.6511.1101.1102.0712.0712.7672.766
3.8423.8422.4032.4023.4013.4004.3894.388

0.41.6831.6820.7210.7211.6181.6192.4822.482
4.0444.0442.4512.4503.3463.3464.2274.226


Radius ratio ( )
Reference [15]Present studyReference [15]Present studyReference [15]Present studyReference [15]Present study

0.22.1042.1032.5532.5533.6883.6884.7124.711
3.3033.3023.9483.9484.8594.8585.8945.893

0.42.5172.5172.7212.7213.2143.2143.9553.956
3.5083.5084.1474.1474.9984.9985.8745.873


Radius ratio (β)
Reference [15]present studyReference [15]present studyReference [15]present studyReference [15]present study

0.22.7832.7833.3783.3784.0664.0654.8024.800
4.0604.0604.3604.3595.1045.1036.0036.001

0.43.4293.4294.0234.0224.7074.7075.2875.286
5.3065.3065.3115.3115.6195.6196.2896.288


Radius ratio (β)
Reference [15]present studyReference [15]present studyReference [15]present studyReference [15]present study

0.20.9190.9191.5421.5412.1572.1572.7782.777
2.1212.1212.6052.6043.4733.4724.4084.406

0.41.2811.2811.9651.9642.4452.4452.9112.911
2.6912.6912.9082.9073.6043.6034.4924.491


Boundary conditions
Reference [19]present studyReference [19]present studyReference [19]present studyReference [19]present study

Elastic-Free0.7710.7711.4081.4082.1212.1212.7722.772
1.9061.9062.5242.5243.4443.4444.3974.397

Elastic-Clamped2.5902.5903.1173.1163.9283.9264.7594.760
3.6253.6254.1344.1365.0005.0015.9575.957

Elastic-Elastic1.4941.4921.8151.8132.4742.4723.1233.120
2.6032.6013.2093.2074.0044.0024.8594.857

Free-Elastic1.0401.0461.5051.5042.4142.4163.1143.116
2.4322.4323.0183.0183.8953.8964.8334.834

Clamped-Elastic1.6861.6861.9601.9592.5142.5123.1293.127
2.7642.7653.3193.3174.0614.0604.8794.877

The exact frequency parameters of the annular disk are further investigated for boundary conditions involving different combinations of free, clamped, and elastic edges. The solutions corresponding to selected modes are obtained for (“Elastic-Free”, “Elastic-Clamped”, “Elastic-Elastic”, “Free-Elastic”, and “Clamped-Elastic”) conditions are presented in Table 9. The results were attained for and . The nondimensional radial and circumferential stiffness parameters were chosen as and . The results are also compared with those obtained using the Raleigh-Ritz methods, as reported in [23]. The comparisons reveal very good agreements between the analytical and the reported results irrespective of the boundary condition considered. The results suggest that the proposed frequency equations could serve as the reference for approximate methods on in-plane vibration characteristics of the annular disks with different combinations of edge conditions.

4. Conclusions

The characteristics of in-plane vibration for circular disks are investigated under different combinations of boundary conditions. The governing equations are solved to obtain the exact frequency equation of solid and annular disks. Frequency equations are presented for different combinations of boundary conditions, including flexible boundaries, at the inner and outer edges. The nondimensional frequency parameters obtained by the present approach compare very well with those available in literature, irrespective of the boundary condition and radius ratio considered. The exact frequency parameters can serve as a reference to assess the accuracy of approximate methods. The presented frequency equations can be numerically evaluated to obtain the in-plane modal characteristics of circular disk for a wide range of constraints conditions and geometric parameters.

Nomenclature

Deflection coefficients of the exact solution
Inner radius of the annular disk
Outer radius of the annular disk
Young’s modulus of disk
Thickness of the annular disk
Bessel function of the first kind of order n
Radial and circumferential stiffness coefficients
Nondimensional radial and circumferential stiffness parameters
Nodal diameter number
Radial and circumferential in-plane forces
Radial coordinate
Radial, circumferential, and normal displacements of the disk
Bessel function of the second kind of order n
Normal coordinate
Radius ratio
Circumferential coordinate
Nondimensional frequency parameters
Poisson’s ratio
Nondimensional radial coordinate of the disk
Mass density of the disk
Lamé Potentials
Radial variations of Lamé Potentials
Radian natural frequency.

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Copyright © 2010 S. Bashmal 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.


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