It is well known that most important musical instruments, including the violin and the guitar, involve strings whose natural frequencies and mode shapes play a significant role in their performance. The characteristics of many engineering systems, such as guy wires, electric transmission lines, ropes and belts used in machinery, and thread manufacture, can be derived from a study of the dynamics of taut strings. The free and forced transverse vibration of strings is considered in this chapter. As will be seen in subsequent chapters, the equation governing the transverse vibration of strings will have the same form as the equations of motion of longitudinal vibration of bars and torsional vibration of shafts.
Figure 8.1 shows a tightly stretched elastic string or cable of length l subjected to a distributed transverse force per unit length. The string is assumed to be supported at the ends on elastic springs of stiffness and . By assuming the transverse displacement of the string to be small, Newton's second law of motion can be applied for the motion of an element of the string in the z direction as
If is the tension, is the mass per unit length, and is the angle made by the deflected string with the x axis, Eq. (8.1) can be rewritten, for an element of length , as
Noting that
Eq. (8.2) can be expressed as
If the string is uniform and the tension is constant, Eq. (8.6) takes the form
For free vibration, and Eq. (8.7) reduces to
which can be rewritten as
where
Equation (8.9) is called the one‐dimensional wave equation.
Strain Energy There are three sources of strain energy for the taut string shown in Fig. 8.1. The first is due to the deformation of the string over , where the tension tries to restore the deflected string to the equilibrium position; the second is due to the deformation of the spring at ; and the third is due to the deformation of the spring at . The length of a differential element dx in the deformed position, ds, can be expressed as
by assuming the slope of the deflected string, , to be small. The strain energy due to the deformations of the springs at and is given by and , and the strain energy associated with the deformation of the string is given by the work done by the tensile force while moving through the distance :
Thus, the total strain energy, , is given by
Kinetic Energy The kinetic energy of the string is given by
where is the mass of the string per unit length.
Work Done by External Forces The work done by the nonconservative distributed load acting on the string, , can be expressed as
Hamilton's principle gives
or
The variations of the individual terms appearing in Eq. (8.17) can be carried out as follows:
using the interchangeability of the variation and differentiation processes. Equation (8.18) can be evaluated by using integration by parts with respect to time:
Using the fact that at and and assuming to be constant, Eq. (8.19) yields
The second term of Eq. (8.16) can be written as
By using integration by parts with respect to x, Eq. (8.21) can be expressed as
The third term of Eq. (8.16) can be written as
By inserting Eqs. (8.20), (8.22), and (8.23) into Eq. (8.16) and collecting the terms, we obtain
Since the variation over the interval is arbitrary, Eq. (8.24) can be satisfied only when the individual terms of Eq. (8.24) are equal to zero:
Equation (8.25) denotes the equation of motion while Eqs. (8.26) and (8.27) represent the boundary conditions. Equation (8.26) can be satisfied when or when . Since the displacement cannot be zero for all time at , Eq. (8.26) can only be satisfied by setting
Similarly, Eq. (8.27) leads to the condition
Thus, the differential equation of motion of the string is given by Eq. (8.25) and the corresponding boundary conditions by Eqs. (8.28) and (8.29).
The equation of motion, Eq. (8.6), or its special forms Eqs. (8.7) and (8.8) or (8.9), is a partial differential equation of order 2 in x as well as t. Thus, two boundary conditions and two initial conditions are required to find the solution, . If the string is given an initial deflection and an initial velocity , the initial conditions can be stated as
If the string is fixed at , the displacement is zero and hence the boundary conditions will be
If the string is connected to a pin that is free to move in a transverse direction, the end will not be able to support any transverse force, and hence the boundary condition will be
If the axial force is constant and the end is free, Eq. (8.32) becomes
If the end of the string is connected to an elastic spring of stiffness k, the boundary condition will be
Some of the possible boundary conditions of a string are summarized in Table 8.1.
Table 8.1 Boundary conditions of a string.
Support conditions of the string | Boundary conditions to be satisfied |
1. Both ends fixed | |
2. Both ends free | |
3. Both ends attached with masses | |
4. Both ends attached with springs | |
5. Both ends attached with dampers | |
Consider a string of infinite length. The free vibration equation of the string, Eq. (8.9), is solved using three different approaches in this section.
The solution of the wave equation (8.9) can be expressed as
where and are arbitrary functions of and , respectively. The solution given by Eq. (8.35) is known as D'Alembert's solution. The validity of Eq. (8.35) can be established by differentiating Eq. (8.35) as
where a prime indicates a derivative with respect to the respective argument. By substituting Eqs. (8.36) and (8.37) into Eq. (8.9), we find that Eq. (8.9) is satisfied. The functions and denote waves that propagate in the positive and negative directions of the x axis, respectively, with a velocity c. The functions and can be determined from the known initial conditions of the string. Using the initial conditions of Eq. (8.30), Eq. (8.35) yields
where a prime in Eq. (8.39) denotes a derivative with respect to the respective argument at (i.e. with respect to x). By integrating Eq. (8.39) with respect to x, we obtain
where is a constant. Equations (8.38) and (8.40) can be solved to find and as
By replacing x by and , respectively, in Eqs. (8.41) and (8.42), we can express the wave solution of the string, , as
The solution given by Eq. (8.43) can be rewritten as
where represents a wave propagating due to a known initial displacement with zero initial velocity, and indicates a wave moving due to the initial velocity with zero initial displacement. A typical wave traveling due to initial displacement (introduced by pulling the string slightly in the transverse direction with zero velocity) is shown in Fig. 8.2.
To find the free vibration response of an infinite string under the initial conditions of Eq. (8.30), we take the Fourier transform of Eq. (8.9). For this, we multiply Eq. (8.9) by and integrate from to :
Integration of the left‐hand side of Eq. (8.45) by parts results in
Assuming that both and tend to zero as , the first term on the right‐hand side of Eq. (8.46) vanishes. Using Eq. (7.16), the Fourier transform of is defined as
and Eq. (8.45) can be rewritten in the form
Note that the use of the Fourier transform reduced the partial differential equation (8.9) into the ordinary differentiation equation (8.48). The solution of Eq. (8.48) can be expressed as
where the constants and can be evaluated using the initial conditions, Eqs. (8.30). By taking the Fourier transforms of the initial displacement and initial velocity , we obtain
The use of Eqs. (8.50) and (8.51) in Eq. (8.49) leads to
whose solution gives
Thus, Eq. (8.49) can be expressed as
By using the inverse Fourier transform of Eq. (8.47), we obtain
which, in view of Eq. (8.56), becomes
Note that the inverse Fourier transforms of and , Eqs. (8.50) and (8.51), can be obtained as
so that
By integrating Eq. (8.60) with respect to from to , we obtain
When Eqs. (8.61) and (8.62) are substituted into Eq. (8.58), we obtain
which can be seen to be identical to Eq. (8.43).
The Laplace transforms of the terms in the governing equation (8.9) lead to
where
Using Eqs. (8.64) and (8.65) along with the initial conditions of Eq. (8.30), Eq. (8.9) can be expressed as
Now, we take the Fourier transform of Eq. (8.67). For this, we multiply Eq. (8.67) by and integrate with respect to x from to , to obtain
The integral on the left‐hand side of Eq. (8.68) can be evaluated by parts:
Assuming that the deflection, , and the slope, , tend to be zero as , Eq. (8.69) reduces to
and hence Eq. (8.68) can be rewritten as
or
or
where
Now we first take the inverse Fourier transform of to obtain
and next we take the inverse Laplace transform of to obtain
Noting that
and
Eqs. (8.76) and (8.75) yield
where
From Eqs. (8.80) and (8.81), we can write
In addition, the following identities are valid:
Thus, Eq. (8.79) can be rewritten as
which can be seen to be the same as the solution given by Eqs. (8.43) and (8.63). Note that Fourier transforms were used in addition to Laplace transforms in the current approach.
The solution of the free vibration equation, Eq. (8.9), can be found using the method of separation of variables. In this method, the solution is written as
where is a function of x only and is a function of t only. By substituting Eq. (8.87) into Eq. (8.9), we obtain
Noting that the left‐hand side of Eq. (8.88) depends only on x while the right‐hand side depends only on t, their common value must be a constant, a, and hence
Equation (8.89) can be written as two separate equations:
The constant a is usually negative1 and hence, by setting , Eqs. (8.90) and (8.91) can be rewritten as
The solution of Eqs. (8.92) and (8.93) can be expressed as
where is the frequency of vibration, the constants A and B can be evaluated from the boundary conditions, and the constants C and D can be determined from the initial conditions of the string.
If the string is fixed at both ends, the boundary conditions are given by
Equations (8.96) and (8.94) yield
The condition of Eq. (8.97) requires that
in Eq. (8.94). Using Eqs. (8.98) and (8.99) in Eq. (8.94), we obtain
For a nontrivial solution, B cannot be zero and hence
Equation (8.101) is called the frequency or characteristic equation, and the values of ω that satisfy Eq. (8.101) are called the eigenvalues (or characteristic values or natural frequencies) of the string. The nth root of Eq. (8.101) is given by
and hence the nth natural frequency of vibration of the string is given by
The transverse displacement of the string, corresponding to , known as the nth mode of vibration or nth harmonic or nth normal mode of the string is given by
In the nth mode, each point of the string vibrates with an amplitude proportional to the value of at that point with a circular frequency . The first four modes of vibration are shown in Fig. 8.3. The mode corresponding to is called the fundamental mode, is called the fundamental frequency, and
is called the fundamental period. The points at which for are called nodes. It can be seen that the fundamental mode has two nodes (at and ), the second mode has three nodes (at , and ), and so on.
The free vibration of the string, which satisfies the boundary conditions of Eqs. (8.97) and (8.98), can be found by superposing all the natural modes as
This equation represents the general solution of Eq. (8.9) and includes all possible vibrations of the string. The particular vibration that occurs is uniquely determined by the initial conditions specified. The initial conditions provide unique values of the constants and in Eq. (8.106). For the initial conditions stated in Eq. (8.30), Eq. (8.106) yields
Noting that Eqs. (8.107) and (8.108) denote Fourier sine series expansions of and in the interval , the values of and can be determined by multiplying Eqs. (8.107) and (8.108) by and integrating with respect to x from 0 to l. This gives the constants and as
Note that the solution given by Eq. (8.106) represents the method of mode superposition since the response is expressed as a superposition of the normal modes. As indicated earlier, the procedure is applicable in finding not only the free vibration response but also the forced vibration response of any continuous system.
Equation (E8.3.17) corresponds to the frequency equation of a wire with both ends fixed.
and Eq. (E8.3.16) yields the modal functions as
It can be observed that this solution corresponds to that of a wire with both ends free.
or
and Eq. (E8.3.16) gives the modal functions as
This solution corresponds to that of a wire which is fixed at and free at .
The equation of motion governing the forced vibration of a uniform string subjected to a distributed load per unit length is given by
Let the string be fixed at both ends so that the boundary conditions become
The solution of the homogeneous equation (with in Eq. [8.111]), which represents free vibration, can be expressed as (see Eq. [8.106])
The solution of the nonhomogeneous equation (with in Eq. [8.111]), which also satisfies the boundary conditions of Eqs. (8.112) and (8.113), can be assumed to be of the form
where denotes the generalized coordinates. By substituting Eq. (8.115) into Eq. (8.111), we obtain
Multiplication of Eq. (8.116) by and integration from 0 to l, along with the use of the orthogonality of the functions , leads to
where
The solution of Eq. (8.117), including the homogeneous solution and the particular integral, can be expressed as
Thus, in view of Eq. (8.115), the forced vibration response of the string is given by
where the constants and are determined from the initial conditions of the string.
The D'Alembert's solution of Eq. (8.8), as given by Eq. (8.35), is obtained by assuming that the increase in tension due to stretching is negligible. If this assumption is not made, Eq. (8.9) becomes
where
with denoting the density of the string. Here denotes the speed of compressional longitudinal wave through the string. An approximate solution of Eq. (8.121) was presented by Bolwell [4]. The dynamics of cables, chains, taut inclined cables, and hanging cables was considered by Triantafyllou [5,6]. In particular, the problem of linear transverse vibration of an elastic string hanging freely under its own weight presents a paradox, in that a solution can be obtained only when the lower end is free. An explanation of the paradox was given by Triantafyllou [6], who also showed that the paradox can be removed by including bending stiffness using singular perturbations.
A mathematical model of the excitation of a vibrating system by a plucking action was studied by Griffel [7]. The mechanism is of the type used in musical instruments [8]. The effectiveness of the mechanism is computed over a range of the relevant parameters. In Ref. [9], Simpson derived the equations of in‐plane motion of an elastic catenary translating uniformly between its end supports in a Eulerian frame of reference. The approximate analytical solution of these equations is given for a shallow catenary in which the tension is dominated by the cable section modulus. Although the mathematical description of a vibrating string is given by the wave equation, a quantum model of information theory was used by Barrett to obtain a one‐degree‐of‐freedom mechanical system governed by a second‐order differential equation [10].
The vibration of a sectionally uniform string from an initial state was considered by Beddoe [11]. The problem was formulated in terms of reflections and transmissions of progressive waves and solved using the Laplace transform method without incorporating the orthogonality relationships. The exact equations of motion of a string were formulated by Narasimha [12], and a systematic procedure was described for obtaining approximations to the equations to any order, making only the assumption that the strain in the material of the string is small. It was shown that the lowest‐order equations in the scheme, which were nonlinear, were used to describe the response of the string near resonance.
Electrodischarge machining (EDM) is a noncontact process of electrically removing (cutting) material from conductive workpieces. In this process, a high potential difference is generated between a wire and a workpiece by charging them positively and negatively, respectively. The potential difference causes sparks between the wires and the workpiece. By moving the wire forward and sideways, the contour desired can be cut on the workpiece. In Ref. [13], Shahruz developed a mathematical model for the transverse vibration of the moving wire used in the EDM process in the form of a nonlinear partial differential equation. The equation was solved, and it was shown that the transverse vibration of the wire is stable and decays to zero for wire axial speeds below a critical value.
A comprehensive view of cable structures was presented by Irvine [14]. The natural frequencies and mode shapes of cables with attached masses have been determined by Sergev and Iwan [15]. The linear theory of free vibrations of a suspended cable has been outlined by Irvine and Caughey [16]. Yu presented explicit vibration solutions of a cable under complicated loads [17]. A theoretical and experimental analysis of free and forced vibration of sagged cable/mass suspension has been presented by Cheng and Perkins [18]. The linear dynamics of a translating string on an elastic foundation was considered by Perkins [19].
Equation (a) indicates that the sign of a will be same as the sign of the integral on the left‐hand side. The left‐hand side of Eq. (a) can be integrated by parts to obtain
The first term on the right‐hand side of Eq. (b) can be seen to be zero or negative for a string with any combination of fixed end , free end , or elastically supported end , where k is the spring constant of the elastic support. Thus, the integral on the left‐hand side of Eq. (a), and hence the sign of a is negative.
and initial velocity .
Find the response of the string.
The boundary and initial conditions of the string are given by
Find the displacement of the string, .
with the initial conditions and by using Laplace transforms with respect to t and Fourier transforms with respect to x.
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