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Journal of Applied Mathematics
Volume 2017, Article ID 2095425, 6 pages
https://doi.org/10.1155/2017/2095425
Research Article

## Nonlinear Waves in Rods and Beams of Power-Law Materials

1Department of Mathematics, School of Science and Technology, Nazarbayev University, Astana 010000, Kazakhstan
2Institute of Applied Physics and Computational Mathematics, P.O. Box 8009, Beijing 100088, China

Correspondence should be addressed to Dongming Wei; zk.ude.un@iew.gnimgnod

Received 16 March 2017; Revised 4 May 2017; Accepted 4 June 2017; Published 13 July 2017

Copyright © 2017 Dongming Wei 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.

#### Abstract

Some novel traveling waves and special solutions to the 1D nonlinear dynamic equations of rod and beam of power-law materials are found in closed forms. The traveling solutions represent waves of high elevation that propagates without change of forms in time. These waves resemble the usual kink waves except that they do not possess bounded elevations. The special solutions satisfying certain boundary and initial conditions are presented to demonstrate the nonlinear behavior of the materials. This note demonstrates the apparent distinctions between linear elastic and nonlinear plastic waves.

#### 1. Introduction

Free vibrations of rods and beams of power-law materials are considered. Analytic traveling wave solutions to the wave equations for power-law materials (see [1, 2]) are obtained which represent kink waves of single elevation that propagates without change of forms in time. It is shown that, unlike the wave equations for linear materials, the nonlinear wave equations do not allow arbitrary traveling wave forms in an infinite rod or beam. The results demonstrate that the traveling fronts of the waves may sharpen or flatten as the wave speeds increase depending upon the power-law index and the bulk modulus. For , the wave fronts sharpen, whereas for , the fronts flatten as the wave speeds increase. The solutions also demonstrate that the speeds of the nonlinear traveling waves depend not only on the material properties but also on the initial energy-level. It is well known that the speeds of waves for the linear elastic materials (, Hooke’s law) depend only on the material properties in contrast to that of the waves in nonlinear materials. As far as we know these solutions are not available in literature, even though there are numerous research papers and books devoted to the discovery and study of traveling waves in elastic and plastic solids (see [37] for details). In the case of rods and beams of finite length, we also present some special solutions satisfying certain boundary and initial conditions. The closed formula solutions are expressed in terms of non-Euclidean sine functions (cf. [8]), which differ from the Euclidean sine functions corresponding to the waves in rods and beams of linear elastic materials.

The note is organized as follows. In Section 2, the power-law constitutive stress-strain equation is introduced. In Section 3, the potential energy and derivations of the wave equations of power-law materials are outlined. In Sections 4 and 5, closed-form solutions are derived. And, finally the results are summarized in Section 6.

#### 2. Hollomon’s Equation

It is well known that, in uniaxial state, the following power-law stress and strain relation is used for certain elastoplastic materials:where is the axial stress, is the axial strain, and and are engineering constants with values depending on the specific material. The materials satisfying (1) sometimes are also referred to as Ludwick or as Hollomon’s materials in literature (cf. [1, 2]). Many heat-treated metals are well-known power-law materials. For a given annealed metal or alloy, and depend on the heat treatment received by the metal or alloy. The values of are typically between and for such metals. For a comprehensive list of experimental values of and of common annealed industrial metals, see, for example, [9]. For some geological materials, such as certain rocks or ice, however, the values of are greater than . In some biological tissues, experiments also indicate that the power-law index satisfies for bones such as tibia and femur, while for cartilages such as common carotid artery and abdominal aorta (see, e.g., [10, 11]). For a given value of , the stress-strain curve defined by (1) can result in a rapid increase in the yield stress for small strains or strain hardening. However, it can be the opposite for values of , for which large strains produce small stress or softening. For these reasons, is called the strain-hardening or strain-softening exponent. Study of the mechanical properties of these heat-treated metals is very important in industries (see, e.g., [12], for stress analysis of beam columns made of Ludwick materials). If we allow , then (1) reduces to Hooke’s law for linear elastic material and the constant , also called the bulk modulus, equals the corresponding Young’s modulus . Power-law materials are a special case of a more general class of materials called Hencky plastics [13]. Physically, the constitutive equation (1) describes the hardening or softening of materials showing an elastic-plastic transition. In the following, bold letters are used to denote vectors or matrices. A vector is considered as a single row matrix. The transpose of a matrix A is denoted by , and the inner product of two vectors u and v by . The time derivative is denoted by . Let denote the displacement vector, the strain components, and , , , , , and the corresponding stress components. The following generalized power law can be derived from the Hencky total deformation theory [13]:where , where , , and are the material constants; see also Wei [14]. Note that (3) is the three-dimensional version of (1). In the following two sections, wave equations of bars and beams made of the power-law elastoplastic materials are derived by (3) and the assumption of the Euler-Bernoulli beam theory. There are similar versions of generalized power-law stress-strain relations for strain-hardening or strain-softening material in the literature and similar wave equations can be derived (see, e.g., [1520]).

#### 3. The Nonlinear Wave Equations

The potential energy for a power-law elastoplastic body occupying a three-dimension body can by defined by where and . The Lagrangian energy functional equals the kinetic energy minus the elastoplastic potential energy plus the work done by external force. It can be written aswhere is the density, the velocity, the body force, and the surface force. See, for example, [21], for a standard definition of . For a uniaxial bar of infinite length with cross-sectional area , subject to axial force and zero surface force, we have , , , , and . For an Euler beam of infinite length, it is assumed that the components of the displacement satisfy , , , , and . Therefore , , and The potential energies for the bar and the beam are given byrespectively, where is the generalized second moment of inertia of the beam. The -axis is taken to be the axial direction of the bar and the beam. For rods and beams of finite length , the corresponding Lagrangian functions are given by replacing and in (6) and (7) by and , respectively. Note that the assumptions made in this section on the elastoplastic bars and the beams are standard assumptions frequently made for elastic bars and beams (see, e.g., [22, 23], for details). The corresponding linear wave equations of elastic bars and beams corresponding to have been studied extensively.

For completeness, the derivation of the wave equations of the power-law materials given in [14] is outlined here. It is well known that Hamilton’s principle seeks an equilibrium state in time dependent mechanical systems (see, e.g., [21]).

Specifically, Hamilton’s principle requires that we seek a displacement so that, for any time interval , and , and for all displacement of the form , where is any real number, the first variation of the energy functional satisfiesfor all satisfying and The combination is referred to as an admissible displacement for the mechanical system since it is required to satisfy some boundary conditions. It can be shown that if the displacement satisfies (8) of Hamilton’s principle, then it must also satisfy a differential wave equation under certain conditions. In particular, suppose that the cross-sectional area, denoted by , is a nonzero constant, and then for the rod, we haveand for the corresponding Euler beamWhen , (9) reduces to the standard wave equation for the elastic barand (10) to the standard wave equation for the elastic Euler beamThe quantity reduces to the second moment of inertia, reduces to when in the elastic beam theory, and the material constant becomes Young’s modulus for linear elastic materials. In deriving the wave equations (9) and (10), we have made the assumption that the solutions and are continuously differentiable and their appropriate lower order derivatives are bounded or vanishing when . By (8), we getUsing integration by parts and interchange of the order of integration, with , and assuming that is bounded by a constant independent of and uniformly in , we get the following:from (13). Since , , and are arbitrary and , we then get (9) from (14). The corresponding beam equation (10) can be derived similarly which was reported in [14].

#### 4. Traveling Waves in Rods and Beams of Arbitrary Length

In the following we will derive some traveling wave solutions to (9) and (10) for and . As far as we know, these solutions are not available in literature, even though there are numerous research papers and books devoted to the discovery and study of traveling waves in elastic and plastic solids. For the study of traveling waves in nonlinear beam equations based on Hooke’s law () for elastic materials, see, for example, [35]. Also, see [6, 7, 24, 25], for more results of traveling waves in solids. Assuming that in (9) and (10), we havefor the bar andfor the beam, where and , respectively. We look for traveling wave solutions of the form for both (15) and (16), where denotes a constant and is a function to be determined. Let , where is the index in power-law (3). The inverse of is sinceFirst, let and substitute into (15), so After integration we get , where is an arbitrary constant. Suppose that . Since and , we have . Looking for nontrivial solutions for and assuming that , we get and which gives the following traveling wave solutions:for the bar equation (15). Note that solution (18) includes some physically meaningful solutions. For example, let us consider a semi-infinite bar with initial displacementand initial velocityand boundary condition . A particular solution satisfying these conditions is given bywhich is obtained from (18). The physical interpretation of the initial condition (19) is that half of the bar is initially subject to a constant stress and the other half is free of stress and fixed in position, and the second initial condition (20) means that the bar is initially moving at a constant speed and half of it is instantaneously stopped. Solution (21) explains that if a prestressed semi-infinite axial power-law rod subject to initial conditions and and boundary conditions for and lower order derivatives are bounded or vanishing when , then the displacement in the interval will be zero at time and the restoration of the deformed bar in interval to its undeformed configuration has a moving boundary which is expanding like a kink wave at a velocity .

In the more general situation, for any value of , the equation has at least one solution since it is continuous, and . Let , and then satisfies . We have the following similar solutions:satisfying the initial and boundary conditionsfor and .

For the linear elastic bar, , , and if , the equation is satisfied for any and also makes . This shows that the linear elastic bar equation allows arbitrary traveling wave forms in , and however the wave can travel only at a fixed velocity . If , then equation gives and the corresponding solution is (22), which is similar to the solutions for .

The above shows that the difference between the nonlinear solution and the linear case is that all the nonlinear traveling waves have the same shape and the traveling velocity depends not only on the material property but also on the initial stress-level while the linear traveling waves can take any form while keeping a fixed traveling velocity that depends only on the material property.

Similarly, by substituting into the beam equation (16), we get After integration twice, we get , which gives by setting . Let ; we get and . From the last equation, we get which gives , where is the integration constant.

We assume and . So, the traveling wave solutions for the corresponding elastoplastic Euler beam are given implicitlywhich results in the following formula in terms of generalized trigonometric function defined in [26]

where . Notice that for we obtain the well-known Euclidean sine traveling wave solution for the elastic Euler beam equation. We observe that the amplitude of the wave is determined by the initial condition . The traveling waves for elastoplastic beams can be applied to study piezoelectric robots; see [27].

#### 5. Special Waves in Rods and Beams of Finite Length

Let us consider some special waves in rods and beams of finite length with fixed ends. Equations (15) and (16) are solved for and with homogeneous Dirichlet boundary conditions and special initial conditions. We present some special solutions by using the generalized trigonometric functions developed by Drábek and Manásevich [26]. By using the separation of variables in (15) and using boundary conditions , we haveFrom the first equation and the boundary conditions, we getBy Thm in [26], a sequence of solutions to the nonlinear eigenvalue problem (28) are given by , where and . Let us consider the initial conditions and . In this case we have and we can solve the second equation in (27). A special solution of this initial value problem is given byThe time evolution of the special solutions for , , , and is presented in Figure 1, respectively.