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Mathematical Problems in Engineering

Volume 2013 (2013), Article ID 284720, 10 pages

http://dx.doi.org/10.1155/2013/284720

## Application of Adomian Modified Decomposition Method to Free Vibration Analysis of Rotating Beams

School of Aircraft Engineering, Nanchang HangKong University, 696 South Fenghe Avenue, Nanchang 330063, China

Received 7 January 2013; Revised 23 February 2013; Accepted 23 February 2013

Academic Editor: Safa Bozkurt Coskun

Copyright © 2013 Qibo Mao. 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.

#### Abstract

The Adomian modified decomposition method (AMDM) is employed in this paper for dynamic analysis of a rotating Euler-Bernoulli beam under various boundary conditions. Based on AMDM, the governing differential equation for the rotating beam becomes a recursive algebraic equation. By using the boundary condition equations, the dimensionless natural frequencies and corresponding mode shapes can be easily obtained simultaneously. The computed results for different boundary conditions as well as different offset length and rotational speeds are presented. The accuracy is assured from the convergence and comparison published results. It is shown that the AMDM offers an accurate and effective method of free vibration analysis of rotating beams with arbitrary boundary conditions.

#### 1. Introduction

The rotating Euler-Bernoulli beams have been the subject of numerous investigations because they are widely used in various aeronautical, robotic, and helicopter blade and wind turbine engineering fields. The free vibration analysis of rotating beams has been extensively studied by many researchers [1–10] with great success. Different numerical or analysis methods such as differential transformation method [1, 2], the Frobenius method [3], finite element method [4, 5], and dynamic stiffness method [6] have been used in solving free vibration problems of such structures. References in [4, 5] give an exhaustive literature survey on the free vibration analysis of rotating beams. References in [11–13] discussed dynamic response of rotating beams with piezoceramic actuation and localized damages. No attempt will be made here to present a bibliographical account of previous work in this area. Few selective recent papers [1–10] which provide further references on the subject are quoted.

Until now, most of the vibration analysis of rotating beams has been limited to classical boundary conditions (i.e., which are either clamped, free, simply supported, or sliding). In practice, however, the characteristics of a test structure may be very well depart from these classical boundary conditions. In this paper, a relatively new computed approach called Adomian modified decomposition method (AMDM) [14–21] is used to analyze the free vibration for the rotating Euler-Bernoulli beams under various boundary conditions, rotating speeds, and offset lengths. The AMDM is a useful and powerful method for solving linear and nonlinear differential equations. The goal of the AMDM is to find the solution of linear and nonlinear, ordinary, or partial differential equation without dependence on any small parameter like perturbation method. The main advantages of AMDM are computational simplicity and do not involve any linearization, discretization, perturbation, or unjustified assumptions which may alter the physics of the problems [14]. In AMDM, the solution is considered as a sum of an infinite series and rapid convergence to an accurate solution [15]. Recently, AMDM has been applied to the problem of vibration of structural and mechanical systems, and this method has shown reliable results in providing analytical approximation that converges rapidly [16–21].

Using the AMDM, the governing differential equation for the rotating beam becomes a recursive algebraic equation [14–17]. The boundary conditions become simple algebraic frequency equations which are suitable for symbolic computation. Moreover, after some simple algebraic operations on these frequency equations, we can obtain the natural frequency and corresponding closed-form series solution of mode shape simultaneously. Finally, some numerical examples are studied to demonstrate the accuracy and efficiency of the proposed method.

#### 2. AMDM for the Rotating Beams

Consider the free vibration of a rotating Euler-Bernoulli beam with length , constant thickness , and width , as shown in Figure 1. The partial differential equation describing the free vibration of a rotating beam is as follows [1, 2]: where is Young’s modulus, is the cross-sectional moment of inertia of the beam, is the cross-sectional area, and is the density of the beam. is the axial force due to the centrifugal stiffening and is given by the following: where is the angular rotating speed of the beam and is offset length between beam and rotating hub.

According to modal analysis approach (for harmonic free vibration), the can be separable in space and time: where , and are the structural mode shape and the natural frequency, respectively.

Substituting (3) into (1), then separating variable for time and space , the ordinary differential equation for the rotating beam can be obtained:

Substituting (2) into (4), then rewriting (4) in dimensionless form, where , , , is the dimensionless rotating speed and is the dimensionless natural frequency.

According to the AMDM [11–18], in (5) can be expressed as an infinite series: where the unknown coefficients will be determined recurrently.

Impose a linear operator , then the inverse operator of is therefore a 4-fold integral operator defined by the following:

Applying both sides of (5) with , we get the following:

Substituting (6) and (8) into (9), we get the following:

Finally, the coefficients in (10) can be determined by using the following recurrence relations:

We may approximate the above solution by the -term truncated series, and (6) can be rewritten as follows:

Equation (13) implies that is negligibly small. The number of the series summation limit is determined by convergence requirement in practice.

From the above analysis, it can be found that there are five unknown parameters , and for the free vibration analysis of the rotating beam. These unknown parameters can be determined by using the boundary condition equations of the beam, and then the natural frequencies and corresponding mode shapes for the rotating beams can be obtained.

#### 3. Natural Frequencies and Mode Shapes

The boundary conditions of the rotating beam shown in Figure 1 can be expressed into dimensionless form [1–4], and we get the following: where , , , , and are the stiffness of the translational springs, and and are the stiffness of the rotational springs at and , respectively.

Substituting (11) into (14), we get the following:

Substituting (12) and (16) into (15), then (15) can be expressed as a linear function of and :

From (17) and (18), the *n*th dimensionless frequency parameter can be solved by the following:
where is the greatest power of .

Notice that (19) is a polynomial of degree evaluated at . By using the functions *sym2poly* and *roots* in MATLAB Symbolic Math Toolbox, (19) can be directly solved. The next step is to determine the *n*th mode shape function corresponding to *n*th dimensionless frequency . Substituting the solved into (17) or (18), can be expressed as the function of :

Substituting (11), (12), and (20) into (13), then the mode shape function can be obtained. By normalizing (13), the normalized mode shape is defined as follows:

It can be found that the mode shape function by using AMDM is a continuous function (closed-form series solution) and not discrete numerical values at knot point by finite element or finite difference methods.

#### 4. Results and Discussion

In order to verify the proposed method to analyze the free vibration of the rotating beam shown in Figure 1, several numerical examples will be discussed in this section.

As mentioned earlier, the closed-form series solutions of mode shape functions in (13) will have to be truncated in numerical calculations. It is important to check how rapidly the dimensionless natural frequencies computed through AMDM converge toward the exact value as the series summation limit is increased. To examine the convergence of the solution, a clamped-free beam with dimensionless rotating speed and dimensionless offset length is considered. In this study, the classical boundary conditions (such as clamped, simply supported, and free) can be considered as the special cases of (14) and (15). For example, the clamped boundary condition is obtained by setting the stiffness of the translational and rotational springs to be extremely large (which is represented by a very large number, , in this paper). Similarly, for simply supported boundary condition, the stiffness of the translational and rotational springs is set to and 0, respectively. For free boundary condition, the stiffness of the translational and rotational springs is set to 0. Figure 2 shows the first five dimensionless natural frequencies as the function of the series summation limit . Clearly, the converges very quickly as the series summation limit is increased. The excellent numerical stability of the solution can also be found in Figure 2.

For brief, the series summation limit in (13) will be simply truncated to in all the subsequent calculations. The dimensionless natural frequencies are kept accurate to the sixth decimal place for comparison purpose. Tables 1, 2, and 3 list the first five dimensionless natural frequencies of the beam under various dimensionless rotating speeds and offset lengths for clamped-free, clamped-clamped, and clamped-simply supported boundary conditions, respectively. Those calculated results are compared with those listed in [1, 3, 4], and excellent agreement is found. Figure 3 shows the first four normalized mode shapes for different boundary conditions when dimensionless rotating speed and offset length .

Figures 4 and 5 show the first five dimensionless natural frequency ratios for the clamped-free beam as the functions of the dimensionless rotating speed and offset length , where is the corresponding dimensionless natural frequencies when (nonrotating beam). From Figures 4 and 5, it can be found that the natural frequencies’ ratios increase when the rotating speed or offset length increases for both beams. However, the variations on the natural frequency ratios of the low order modes are more sensitive to the rotating speed or offset length.

Next, the beams with general boundary conditions are discussed. Because the proposed method based on AMDM technique offers a unified and systematic procedure for vibration analysis, the modification of boundary conditions from one case to another is as simple as changing the values of the stiffness of translational and rotational springs. And it does not involve any changes to the solution procedures or algorithms.

Table 4 lists the first five dimensionless natural frequency for the beam with different dimensionless rotating speeds and different rotational springs and when the translational springs and the dimensionless offset length . From Table 4, it is found that the natural frequencies increase when the offset length or rotating speed increases, as expected. Figure 6 shows the first four normalized mode shapes of the rotating beam listed in Table 4. From Figure 6, it can be found that the discrepancies of the mode shapes under different rotating speeds are very small. However, the natural frequencies are quite different, as shown in Table 4.

Based on the developments achieved and results obtained in this paper, the following remarks can be made.(1)The essential steps of the AMDM application includes transforming the governing differential equation for the rotating beam into algebraic equation; by using the boundary condition equations, any desired dimensionless natural frequencies and corresponding mode shapes can be easily obtained simultaneously.(2)All the steps of the AMDM are very straightforward, and the application of the AMDM to both equations of motion and the boundary conditions seems to be very involved computationally. However, all the algebraic calculations are finished quickly using symbolic computational software (such as MATLAB). Besides all these, the analysis of the convergence of the results shows that AMDM solutions converge fast. The results of the AMDM are found in excellent agreement with available published results.

#### 5. Conclusions

In this paper, free vibrations of the uniform rotating Euler-Bernoulli beams under different boundary conditions are analyzed using Adomian modified decomposition method (AMDM). The advantages of the AMDM are its fast convergence of the solution and its high degree of accuracy. Natural frequencies and corresponding mode shapes with various boundary conditions, dimensionless offset length, and dimensionless rotating speed are presented. Furthermore, the natural frequencies obtained by using AMDM are in excellent agreement with published results.

It should be noted that the proposed method can be used to analyze the vibration of the rotating beams under arbitrary boundary conditions. The vibration analysis for different boundary conditions and/or rotating speed is as simple as changing the value of corresponding parameters and does not involve any changes to the solution procedures or algorithms.

The results in this paper show that the AMDM technique is reliable, powerful, and promising for solving free vibration problems for rotating beams. The author believes that the AMDM can further be applied to the Timoshenko rotating beam problems and also it can be used as an alternative to other solution techniques such as finite element method, differential quadrature method, and Frobenius method.

#### Acknowledgments

This work was partly sponsored by the National Natural Science Foundation of China (no. 51265037), Scientific Research Foundation for the Returned Overseas Chinese Scholars, State Education Ministry (no. 2012-44), and Technology Foundation of Jiangxi Province, China (no. KJLD12075).

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