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The climax of this book comes early. Here we identify the crucial features of a system that supports waves — space translation invariance and local interactions.

5.1: Space Translation Invariance

A finite system of coupled pendulums.

Figure 5.1:A finite system of coupled pendulums.

The typical system of coupled oscillators that supports waves is one like the system of NN identical coupled pendulums shown in Figure 5.1. This system is a generalization of the system of two coupled pendulums that we studied in chapters 3 and 4. Suppose that each pendulum bob has mass mm, each pendulum has length \ell, each spring has spring constant κ\kappa and the equilibrium separation between bobs is aa. Suppose further that there is no friction and that the pendulums are constrained to oscillate only in the direction in which the springs are stretched. We are interested in the free oscillation of this system, with no external force. Such an oscillation, when the motion is parallel to the direction in which the system is stretched in space is called a “longitudinal oscillation”. Call the longitudinal displacement of the jjth bob from equilibrium ψj\psi_{j}. We can organize the displacements into a vector, Ψ\Psi (for reasons that will become clear below, it would be confusing to use XX, so we choose a different letter, the Greek letter psi, which looks like ψ\psi in lower case and Ψ\Psi when capitalized):

Ψ=(ψ1ψ2ψ3ψN).(5.1)\Psi=\left(\begin{array}{c} \psi_{1} \\ \psi_{2} \\ \psi_{3} \\ \vdots \\ \psi_{N} \end{array}\right) . \tag{5.1}

Then the equations of motion (for small longitudinal oscillations) are

d2Ψdt2=M1KΨ(5.2)\frac{d^{2} \Psi}{d t^{2}}=-M^{-1} K \Psi \tag{5.2}

where MM is the diagonal matrix with mm’s along the diagonal,

(m0000m0000m0000m),(5.3)\left(\begin{array}{ccccc} m & 0 & 0 & \cdots & 0 \\ 0 & m & 0 & \cdots & 0 \\ 0 & 0 & m & \cdots & 0 \\ \vdots & \vdots & \vdots & \ddots & \vdots \\ 0 & 0 & 0 & \cdots & m \end{array}\right) , \tag{5.3}

and KK has diagonal elements (mg/+2κ)(m g / \ell+2 \kappa), next-to-diagonal elements κ-\kappa, and zeroes elsewhere,

(mg/+2κκ00κmg/+2κκ00κmg/+2κ0000mg/+2κ).(5.4)\left(\begin{array}{ccccc} m g / \ell+2 \kappa & -\kappa & 0 & \cdots & 0 \\ -\kappa & m g / \ell+2 \kappa & -\kappa & \cdots & 0 \\ 0 & -\kappa & m g / \ell+2 \kappa & \cdots & 0 \\ \vdots & \vdots & \vdots & \ddots & \vdots \\ 0 & 0 & 0 & \cdots & m g / \ell+2 \kappa \end{array}\right) . \tag{5.4}

The κ- \kappa in the next-to-diagonal elements has exactly the same origin as the κ- \kappa in the 2×2 K2 \times 2 \text { } K matrix in 3.78. It describes the coupling of two neighboring blocks by the spring. The (mg/+2κ)(m g / \ell+2 \kappa) on the diagonal is analogous to the (mg/+κ)(m g / \ell+ \kappa) on the diagonal of 3.78. The difference in the factor of 2 in the coefficient of κ\kappa arises because there are two springs, one on each side, that contribute to the restoring force on each block in the system shown in Figure 5.1, while there was only one in the system shown in Figure 3.1. Thus M1KM^{- 1}K has the form

(2BC00C2BC00C2B00002B)(5.5)\left(\begin{array}{ccccc} 2 B & -C & 0 & \cdots & 0 \\ -C & 2 B & -C & \cdots & 0 \\ 0 & -C & 2 B & \cdots & 0 \\ \vdots & \vdots & \vdots & \ddots & \vdots \\ 0 & 0 & 0 & \cdots & 2 B \end{array}\right) \tag{5.5}

where

2B=g/+2κ/m,C=κ/m.(5.6)2 B=g / \ell+2 \kappa / m, \quad C=\kappa / m . \tag{5.6}

It is interesting to compare the matrix, 5.5, with the matrix, 4.43, from the previous chapter. In both cases, the diagonal elements are all equal, because of the symmetry. The same goes for the next-to-diagonal elements. However, in 5.5, all the rest of the elements are zero because the interactions are only between nearest neighbor blocks. We call such interactions “local.” In 4.43, on the other hand, each of the masses interacts with all the others. We will use the local nature of the interactions below.

We could try to find normal modes of this system directly by finding the eigenvectors of M1KM^{- 1}K, but there is a much easier and more generally useful technique. We can divide the physics of the system into two parts, the physics of the coupled pendulums, and the physics of the walls. To do this, we first consider an infinite system with no walls at all.

A piece of an infinite system of coupled pendulums.

Figure 5.2:A piece of an infinite system of coupled pendulums.

Notice that in Figure 5.2, we have not changed the interior of the system shown in Figure 5.1 at all. We have just replaced the walls by a continuation of the interior.

Now we can find all the modes of the infinite system of Figure 5.2 very easily, making use of a symmetry argument. The infinite system of Figure 5.2 looks the same if it is translated, moved to the left or the right by a multiple of the equilibrium separation, aa. It has the property of “space translation invariance.” Space translation invariance is the symmetry of the infinite system under translations by multiples of aa. In this example, because of the discrete blocks and finite length of the springs, the space translation invariance is “discrete.” Only translation by integral multiples of aa give the same physics. Later, we will discuss continuous systems that have continuous space translation invariance. However, we will see that such systems can be analyzed using the same techniques that we introduce in this chapter.

We can use the symmetry of space translation invariance, just as we used the reflection and rotation symmetries discussed in the previous chapter, to find the normal modes of the infinite system. The discrete space translation invariance of the infinite system (the symmetry under translations by multiples of aa) allows us to find the normal modes of the infinite system in a simple way.

Most of the modes that we find using the space translation invariance of the infinite system of Figure 5.2 will have nothing to do with the finite system shown in Figure 5.1. But if we can find linear combinations of the normal modes of the infinite system of Figure 5.2 in which the 0th and NN + 1st blocks stay fixed, then they must be solutions to the equations of motion of the system shown in Figure 5.1. The reason is that the interactions between the blocks are “local” — they occur only between nearest neighbor blocks. Thus block 1 knows what block 0 is doing, but not what block −1 is doing. If block 0 is stationary it might as well be a wall because the blocks on the other side do not affect block 1 (or any of the blocks 1 to NN) in any way. The local nature of the interaction allows us to put in the physics of the walls as a boundary condition after solving the infinite problem. This same trick will also enable us to solve many other problems.

Let us see how it works for the system shown in Figure 5.1. First, we use the symmetry under translations to find the normal modes of the infinite system of Figure 5.2. As in the previous two chapters, we describe the solutions in terms of a vector, AA. But now AA has an infinite number of components, AjA_{j} where the integer jj runs from - \infty to ++ \infty. It is a little inconvenient to write this infinite vector down, but we can represent a piece of it:

A=(A0A1A2A3ANAN+1).(5.7)A=\left(\begin{array}{c} \vdots \\ A_{0} \\ A_{1} \\ A_{2} \\ A_{3} \\ \vdots \\ A_{N} \\ A_{N+1} \\ \vdots \end{array}\right) . \tag{5.7}

Likewise, the M1KM^{- 1}K matrix for the system is an infinite matrix, not easily written down, but any piece of it (along the diagonal) looks like the interior of 5.5:

(2BC00C2BC00C2BC00C2B).(5.8)\left(\begin{array}{cccccc} \ddots & \vdots & \vdots & \vdots & \vdots & \ddots \\ \cdots & 2 B & -C & 0 & 0 & \cdots \\ \cdots & -C & 2 B & -C & 0 & \cdots \\ \cdots & 0 & -C & 2 B & -C & \cdots \\ \cdots & 0 & 0 & -C & 2 B & \cdots \\ \ddots & \vdots & \vdots & \vdots & \vdots & \ddots \end{array}\right) . \tag{5.8}

This system is “space translation invariant” because it looks the same if it is moved to the left a distance aa. This moves block j+1j+1 to where block jj used to be, thus if there is a mode with components AjA_{j}, there must be another mode with the same frequency, represented by a vector, A=SAA^{\prime} = SA, with components

Aj=Aj+1.(5.9)A_{j}^{\prime}=A_{j+1} . \tag{5.9}

The symmetry matrix, SS, is an infinite matrix with 1s along the next-to-diagonal. These are analogous to the 1s along the next-to-diagonal in 4.40. Now, however, the transformation never closes on itself. There is no analog of the 1 in the lower left-hand corner of 4.40, because the infinite matrix has no corner. We want to find the eigenvalues and eigenvectors of the matrix SS, satisfying

A=SA=βA(5.10)A^{\prime}=S A=\beta A \tag{5.10}

or equivalently (from 5.9), the modes in which AjA_{j} and AjA_{j}^{\prime} are proportional:

Aj=βAj=Aj+1(5.11)A_{j}^{\prime}=\beta A_{j}=A_{j+1} \tag{5.11}

where β\beta is some nonzero constant.[1]

Equation 5.11 can be solved as follows: Choose A0=1A_{0} = 1. Then A1=βA_{1} = \beta, A2=β2A_{2} = \beta^{2}, etc., so that Aj=(β)jA_{j} = (\beta)^{j} for all nonnegative jj. We can also rewrite 5.11 as Aj1=β1AjA_{j-1}=\beta^{-1} A_{j}, so that A1=β1A_{-1} = \beta^{-1}, A2=β2A_{-2} = \beta^{-2}, etc. Thus the solution is

Aj=(β)j(5.12)A_{j}=(\beta)^{j} \tag{5.12}

Now that we know the form of the normal modes, it is easy to get the corresponding frequencies by acting on 5.12 with the M1KM^{-1}K matrix, 5.8. This gives

ω2Ajβ=2BAjβCAj+1βCAj1β,(5.13)\omega^{2} A_{j}^{\beta}=2 B A_{j}^{\beta}-C A_{j+1}^{\beta}-C A_{j-1}^{\beta} , \tag{5.13}

or inserting 5.13,

ω2βj=2BβjCβj+1Cβj1=(2BCβCβ1)βj.(5.14)\omega^{2} \beta^{j}=2 B \beta^{j}-C \beta^{j+1}-C \beta^{j-1}=\left(2 B-C \beta-C \beta^{-1}\right) \beta^{j} . \tag{5.14}

This is true for all jj, which shows that 5.13 is indeed an eigenvector (we already knew this from the symmetry argument, 4.22, but it is nice to check when possible), and the eigenvalue is

ω2=2BCβCβ1.(5.15)\omega^{2}=2 B-C \beta-C \beta^{-1} . \tag{5.15}

Notice that for almost every value of ω2\omega^{2}, there are two normal modes, because we can interchange β\beta and β1\beta^{-1} without changing 5.16. The only exceptions are

ω2=2B2C,(5.16)\omega^{2}=2 B \mp 2 C , \tag{5.16}

corresponding to β=±1\beta=\pm 1. The fact that there are at most two normal modes for each value of ω2\omega^{2} will have a dramatic consequence. It means that we only have to deal with two normal modes at a time to implement the physics of the boundary. This is a special feature of the one-dimensional system that is not shared by two- and three-dimensional systems. As we will see, it makes the one-dimensional system very easy to handle.

Boundary Conditions

Figure5-1

We have now solved the problem of the oscillation of the infinite system. Armed with this result, we can put back in the physics of the walls. Any β\beta (except β=±1\beta=\pm 1) gives a pair of normal modes for the infinite system of Figure 5.2. But only special values of β\beta will work for the finite system shown in Figure 5.1. To find the normal modes of the system shown in Figure 5.1, we use (4.56), the fact that any linear combination of the two normal modes with the same angular frequency, ω\omega, is also a normal mode. If we can find a linear combination that vanishes for j=0j = 0 and for j=N+1j = N + 1, it will be a normal mode of the system shown in Figure 5.1. It is the vanishing of the normal mode at j=0j = 0 and j=N+1j = N + 1 that are the “boundary conditions” for this particular finite system.

Let us begin by trying to satisfy the boundary condition at j=0j = 0. For each possible value of ω2\omega^{2}, we have to worry about only two normal modes, the two solutions of 5.16 for β\beta. So long as β±1\beta \neq \pm 1, we can find a combination that vanishes at j=0j = 0; just subtract the two modes AβA^{\beta} and Aβ1A^{\beta^{-1}} to get a vector

A=AβAβ1,(5.17)A=A^{\beta}-A^{\beta^{-1}} , \tag{5.17}

or in components

AjAjβAjβ1=βjβj.(5.18)A_{j} \propto A_{j}^{\beta}-A_{j}^{\beta^{-1}}=\beta^{j}-\beta^{-j} . \tag{5.18}

The first thing to notice about 5.19 is that AjA^{j} cannot vanish for any j0j \neq 0 unless β=1|\beta|=1. Thus if we are to have any chance of satisfying the boundary condition at j=N+1j = N + 1, we must assume that

β=eiθ.(5.19)\beta=e^{i \theta} . \tag{5.19}

Then from 5.19,

Ajsinjθ.(5.20)A_{j} \propto \sin j \theta . \tag{5.20}

Now we can satisfy the boundary condition at j=N+1j = N + 1 by setting AN+1=0A_{N + 1} = 0. This implies sin[(N+1)θ]=0\sin [(N+1) \theta]=0, or

θ=nπ/(N+1), for integer n.(5.21)\theta=n \pi /(N+1), \text { for integer } n . \tag{5.21}

Thus the normal modes of the system shown in Figure 5.1 are

Ajn=sin(jnπN+1), for n=1,2,N.(5.22)A_{j}^{n}=\sin \left(\frac{j n \pi}{N+1}\right), \text { for } n=1,2, \cdots N . \tag{5.22}

Other values of nn do not lead to new modes, they just repeat the NN modes already shown in 5.23. The corresponding frequencies are obtained by putting 5.20-5.21 into 5.16, to get

ω2=2B2Ccosθ=2B2Ccos(nπN+1).(5.23)\omega^{2}=2 B-2 C \cos \theta=2 B-2 C \cos \left(\frac{n \pi}{N+1}\right) . \tag{5.23}

From here on, the analysis of the motion of the system is the same as for any other system of coupled oscillators. As discussed in chapter 3, we can take a general motion apart and express it as a sum of the normal modes. This is illustrated for the system of coupled pendulums in program 5-1 on the program disk. The new thing about this system is the way in which we obtained the normal modes, and their peculiarly simple form, in terms of trigonometric functions. We will get more insight into the meaning of these modes in the next section. Meanwhile, note the way in which the simple modes can be combined into the very complicated motion of the full system.


5.2: k and Dispersion Relations

So far, the equilibrium separation between the blocks, aa, has not appeared in the analysis. Everything we have said so far would be true even if the springs had random lengths, so long as all spring constants were the same. In such a case, the “space translation invariance” that we used to solve the problem would be a purely mathematical device, taking the original system into a different system with the same kind of small oscillations. Usually, however, in physical applications, the space translation invariance is real and all the inter-block distances are the same. Then it is very useful to label the blocks by their equilibrium position. Take x=0x = 0 to be the position of the left wall (or the 0th block). Then the first block is at x=ax = a, the second at x=2ax = 2a, etc., as shown in Figure 5.3. We can describe the displacement of all the blocks by a function ψ(x,t)\psi(x, t), where ψ(ja,t)\psi(ja, t) is the displacement of the jjth block (the one with equilibrium position jaja). Of course, this function is not very well defined because we only care about its values at a discrete set of points. Nevertheless, as we will see below when we discuss the beaded string, it will help us understand what is going on if we draw a smooth curve through these points.

The coupled pendulums with blocks labeled by their equilibrium positions.

Figure 5.3:The coupled pendulums with blocks labeled by their equilibrium positions.

In the same way, we can describe a normal mode of the system shown in Figure 5.1 (or the infinite system of Figure 5.2) as a function A(x)A(x) where

A(ja)=Aj.(5.24)A(j a)=A_{j} . \tag{5.24}

In this language, space translation invariance, 5.11, becomes

A(x+a)=βA(x).(5.25)A(x+a)=\beta A(x) . \tag{5.25}

It is conventional to write the constant β\beta as an exponential

β=eika.(5.26)\beta=e^{i k a} . \tag{5.26}

Any nonzero complex number can be written as a exponential in this way. In fact, we can change kk by a multiple of 2π/a2 \pi / a without changing β\beta, thus we can choose the real part of kk to be between π/a- \pi / a and π/a\pi / a

πa<Rekπa.(5.27)-\frac{\pi}{a}<\operatorname{Re} k \leq \frac{\pi}{a} . \tag{5.27}

If we put 5.13 and 5.27 into 5.25, we get

Aβ(ja)=eikja.(5.28)A^{\beta}(j a)=e^{i k j a} . \tag{5.28}

This suggests that we take the function describing the normal mode corresponding to 5.27 to be

A(x)=eikx.(5.29)A(x)=e^{i k x} . \tag{5.29}

The mode is determined by the number kk satisfying 5.28.

The parameter kk (when it is real) is called the angular wave number of the mode. It measures the waviness of the normal mode, in radians per unit distance. The “wavelength” of the mode is the smallest length, λ\lambda (the Greek letter lambda), such that a change of xx by λ\lambda leaves the mode unchanged,

A(x+λ)=A(x).(5.30)A(x+\lambda)=A(x) . \tag{5.30}

In other words, the wavelength is the length of a complete cycle of the wave, 2π2 \pi radians. Thus the wavelength, λ\lambda, and the angular wave number, kk, are inversely related, with a factor of 2π2 \pi,

λ=2πk . (5.31)\lambda=\frac{2 \pi}{k} \text { . } \tag{5.31}

In this language, the normal modes of the system shown in Figure 5.1 are described by the functions

An(x)=sinkx,(5.32)A^{n}(x)=\sin k x , \tag{5.32}

with

k=nπL,(5.33)k=\frac{n \pi}{L} , \tag{5.33}

where L=(N+1)aL = (N +1)a is the total length of the system. The important thing about 5.33 and 5.34 is that they do not depend on the details of the system. They do not even depend on NN. The normal modes always have the same shape, when the system has length LL. Of course, as NN increases, the number of modes increases. For fixed L, this happens because a=L/(N+1)a = L/(N + 1) decreases as NN increases and thus the allowed range of kk (remember 5.28) increases.

The forms 5.33 for the normal modes of the space translation invariant system are called “standing waves.” We will see in more detail below why the word “wave” is appropriate. The word “standing” refers to the fact that while the waves are changing with time, they do not appear to be moving in the xx direction, unlike the “traveling waves” that we will discuss in chapter 8 and beyond.

Dispersion Relation

In terms of the angular wave number kk, the frequency of the mode is (from 5.16 and 5.27)

ω2=2B2Ccoska.(5.34)\omega^{2}=2 B-2 C \cos k a . \tag{5.34}

Such a relation between kk (actually k2k^{2} because coska\cos k a is an even function of kk) and ω2\omega^{2} is called a “dispersion relation” (we will learn later why the name is appropriate). The specific form 5.35 is a characteristic of the particular infinite system of Figure 5.2. It depends on the masses and spring constants and pendulum lengths and separations.

But it does not depend on the boundary conditions. Indeed, we will see below that 5.35 will be useful for boundary conditions very different from those of the system shown in Figure 5.1.

The dispersion relation depends only on the physics of the infinite system.

Indeed, it is only through the dispersion relation that the details of the physics of the infinite system enters the problem. The form of the modes, e±ikxe^{\pm i k x}, is already determined by the general properties of linearity and space translation invariance.

We will call 5.35 the dispersion relation for coupled pendulums. We have given it a special name because we will return to it many times in what follows. The essential physics is that there are two sources of restoring force: gravity, that tends to keep all the masses in equilibrium; and the coupling springs, that tend to keep the separations between the masses fixed, but are unaffected if all the masses are displaced by the same distance. In 5.35, the constants always satisfy BCB \geq C, as you see from 5.6.

The limit B=CB = C is especially interesting. This happens when there is no gravity (or \ell \rightarrow \infty). The dispersion relation is then

ω2=2B(1coska)=4Bsin2ka2.(5.35)\omega^{2}=2 B(1-\cos k a)=4 B \sin ^{2} \frac{k a}{2} . \tag{5.35}

Note that the mode with k=0k = 0 now has zero frequency, because all the masses can be displaced at once with no restoring force.[2]


5.3: Waves

Beaded String

The beaded string in equilibrium.

Figure 5.4:The beaded string in equilibrium.

Another instructive system is the beaded string, undergoing transverse oscillations. The oscillations are called “transverse” if the motion is perpendicular to the direction in which the system is stretched. Consider a massless string with tension TT, to which identical beads of mass mm are attached at regular intervals, aa. A portion of such a system in its equilibrium configuration is depicted in Figure 5.4. The beads cannot oscillate longitudinally, because the string would break.[3] However, for small transverse oscillations, the stretching of the string is negligible, and the tension and the horizontal component of the force from the string are approximately constant. The horizontal component of the force on each block from the string on its right is canceled by the horizontal component from the string on the left. The total horizontal force on each block is zero (this must be, because the blocks do not move horizontally). But the strings produces a transverse restoring force when neighboring beads do not have the same transverse displacement, as illustrated in Figure 5.5. The force of the string on bead 1 is shown, along with the transverse component. The dotted lines complete similar triangles, so that F/T=(ψ2ψ1)/aF / T=\left(\psi_{2}-\psi_{1}\right) / a. You can see from Figure 5.5 that the restoring force, FF in the figure, for small transverse oscillations is linear, and corresponds to a spring constant T/aT / a.

Two neighboring beads on a beaded string.

Figure 5.5:Two neighboring beads on a beaded string.

Thus 5.37 is also the dispersion relation for the small transverse oscillations of the beaded string with

B=Tma,(5.36)B=\frac{T}{m a}, \tag{5.36}

where TT is the string tension, mm is the bead mass and aa is the separation between beads. The dispersion relation for the beaded string can thus be written as

ω2=4Tmasin2ka2(5.37)\omega^{2}=\frac{4 T}{m a} \sin ^{2} \frac{k a}{2} \tag{5.37}

This dispersion relation, 5.39, has the interesting property that ω0\omega \rightarrow 0 as k0k \rightarrow 0. This is discussed from the point of view of symmetry in appendix C, where we discuss the connection of this dispersion relation with what are called “Goldstone bosons.” Here we should discuss the special properties of the k=0k = 0 mode with exactly zero angular frequency, ω=0\omega = 0. This is different from all other angular frequencies because we do not get a different time dependence by complex conjugating the irreducible complex exponential, eiωte^{-i \omega t}. But we need two solutions in order to describe the possible initial conditions of the system, because we can specify both a displacement and a velocity for each bead. The resolution of this dilemma is similar to that discussed for critical damping in chapter 2 (see 2.12). If we approach ω=0\omega = 0 from nonzero ω\omega, we can form two independent solutions as follows:4

limω0eiωt+eiωt2=1,limω0eiωteiωt2iω=t(5.38)\lim _{\omega \rightarrow 0} \frac{e^{-i \omega t}+e^{i \omega t}}{2}=1, \quad \lim _{\omega \rightarrow 0} \frac{e^{-i \omega t}-e^{i \omega t}}{-2 i \omega}=t \tag{5.38}

The first, for k=0k = 0, describes a situation in which all the beads are sitting at some fixed position. The second describes a situation in which all of the beads are moving together at constant velocity in the transverse direction.

Precisely analogous things can be said about the xx dependence of the k=0k = 0 mode. Again, approaching k=0k = 0 from nonzero kk, we can form two modes,

limk0eikx+eikx2=1,limk0eikxeikx2ik=x(5.39)\lim _{k \rightarrow 0} \frac{e^{i k x}+e^{-i k x}}{2}=1, \quad \lim _{k \rightarrow 0} \frac{e^{i k x}-e^{-i k x}}{2 i k}=x \tag{5.39}

The second mode here describes a situation in which each subsequent bead is more displaced. The transverse force on each bead from the string on the left is canceled by the force from the string on the right.

Fixed Ends

Figure5-2

A beaded string with fixed ends.

Figure 5.6:A beaded string with fixed ends.

Now suppose that we look at a finite beaded string with its ends fixed at x=0x = 0 and x=L=(N+1)ax = L = (N + 1)a, as shown in Figure 5.6. The analysis of the normal modes of this system is exactly the same as for the coupled pendulum problem at the beginning of the chapter. Once again, we imagine that the finite system is part of an infinite system with space translation invariance and look for linear combinations of modes such that the beads at x=0x = 0 and x=Lx = L are fixed. Again this leads to 5.33. The only differences are:

  1. the frequencies of the modes are different because the dispersion relation is now given by 5.39;

  2. 5.33 describes the transverse displacements of the beads.

This is a very nice example of the standing wave normal modes, 5.33, because you can see the shapes more easily than for longitudinal oscillations. For four beads (N=4N = 4), the four independent normal modes are illustrated in Figures 5.7-5.10Figures \text { } 5.7 \text {-} 5.10, where we have made the coupling strings invisible for clarity. The fixed imaginary beads that play the role of the walls are shown (dashed) at x=0x = 0 and x=Lx = L. Superimposed on the positions of the beads is the continuous function, sinkx\sin k x, for each kk value, represented by a dotted line. Note that this function does not describe the positions of the coupling strings, which are stretched straight between neighboring beads.

n = 1.

Figure 5.7:n=1n = 1.

Figure

n = 2.

Figure 5.8:n=2n = 2.

n = 3.

Figure 5.9:n=3n = 3.

n = 4.

Figure 5.10:n=4n = 4.

It is pictures like Figures 5.7-5.10Figures \text { } 5.7 \text {-} 5.10 that justify the word “wave” for these standing wave solutions. They are, frankly, wavy, exhibiting the sinusoidal space dependence that is the sine qua non of wave phenomena.

The transverse oscillation of a beaded string with both ends fixed is illustrated in program 5-2, where a general oscillation is shown along with the normal modes out of which it is built. Note the different frequencies of the different normal modes, with the frequency increasing as the modes get more wavy. We will often use the beaded string as an illustrative example because the modes are so easy to visualize.


4You can evaluate the limits easily, using the Taylor series for ex=1+x+e^{x}=1+x+\cdots.

5.4: Free Ends

Let us work out an example of forced oscillation with a different kind of boundary condition. Consider the transverse oscillations of a beaded string. For definiteness, we will take four beads so that this is a system of four coupled oscillators. However, instead of coupling the strings at the ends to fixed walls, we will attach them to massless rings that are free to slide in the transverse direction on frictionless rods. The string then is said to have its ends free (at least for transverse motion). Then the system looks like the diagram in Figure 5.11, where the oscillators move up and down in the plane of the paper: Let us find its normal modes.

A beaded string with free ends.

Figure 5.11:A beaded string with free ends.

Normal Modes for Free Ends

Figure5-3

As before, we imagine that this is part of an infinite system of beads with space translation invariance. This is shown in Figure 5.12. Here, the massless rings sliding on frictionless rods have been replaced by the imaginary (dashed) beads, 0 and 5. The dispersion relation is just the same as for any other infinite beaded string, 5.39. The question is, then, what kind of boundary condition on the infinite system corresponds to the physical boundary condition, that the end beads are free on one side? The answer is that we must have the first imaginary bead on either side move up and down with the last real bead, so that the coupling string from bead 0 is horizontal and exerts no transverse restoring force on bead 1 and the coupling string from bead 5 is horizontal and exerts no transverse restoring force on bead 4:

A0=A1,(5.40)A_{0}=A_{1} , \tag{5.40}
A4=A5;(5.41)A_{4}=A_{5} ; \tag{5.41}
Satisfying the boundary conditions in the finite system.

Figure 5.12:Satisfying the boundary conditions in the finite system.

We will work in the notation in which the beads are labeled by their equilibrium positions. The normal modes of the infinite system are then e±ikxe^{\pm i k x}. But we haven’t yet had to decide where we will put the origin. How do we form a linear combination of the complex exponential modes, e±ikxe^{\pm i k x}, and choose kk to be consistent with this boundary condition? Let us begin with 5.42. We can write the linear combination, whatever it is, in the form

cos(kxθ).(5.42)\cos (k x-\theta) . \tag{5.42}

Any real linear combination of e±ikxe^{\pm i k x} can be written in this way up to an overall multiplicative constant (see 1.96). Now if

cos(kx0θ)=cos(kx1θ),(5.43)\cos \left(k x_{0}-\theta\right)=\cos \left(k x_{1}-\theta\right) , \tag{5.43}

where xjx_{j} is the position of the jjth block, then either

  1. cos(kxθ)\cos (k x-\theta) has a maximum or minimum at x0+x12\frac{x_{0}+x_{1}}{2}, or

  2. kx1kx0k x_{1}-k x_{0} is a multiple of 2π2 \pi.

Let us consider case 1. We will see that case 2 does not give any additional modes. We will x0+x12\frac{x_{0}+x_{1}}{2} choose our coordinates so that the point , midway between x0x_{0} and x1x_{1}, is x=0x = 0. We don’t care about the overall normalization, so if the function has a minimum there, we will multiply it by −1, to make it a maximum. Thus in case 1, the function cos(kxθ)\cos (k x-\theta) has a maximum at x=0x = 0, which implies that we can take θ=0\theta = 0. Thus the function is simply coskx\cos kx. The system with this labeling is shown in Figure 5.13. The displacement of the jjth bead is then

Aj=cos[ka(j1/2)].(5.44)A_{j}=\cos [k a(j-1 / 2)] . \tag{5.44}
The same system of oscillators labeled more cleverly.

Figure 5.13:The same system of oscillators labeled more cleverly.

It should now be clear how to impose the boundary condition, 5.43, on the other end. We want to have a maximum or minimum midway between bead 4 and bead 5, at x=4ax = 4a. We get a maximum or minimum every time the argument of the cosine is an integral multiple of π\pi. The argument of the cosine at x=4ax = 4a is 4ka4ka, where kk is the angular wave number. Thus the boundary condition will be satisfied if the mode has 4ka=nπ4ka = n \pi for integer nn. Then

cos[ka(41/2)]=cos[ka(51/2)]ka=nπ4.(5.45)\cos [k a(4-1 / 2)]=\cos [k a(5-1 / 2)] \Rightarrow k a=\frac{n \pi}{4} . \tag{5.45}

Thus the modes are

Aj=cos[ka(j1/2)] with k=nπ4a for n=0 to 3.(5.46)A_{j}=\cos [k a(j-1 / 2)] \text { with } k=\frac{n \pi}{4 a} \text { for } n=0 \text { to } 3 . \tag{5.46}

For n>3n > 3, the modes just repeat, because kπ/ak \geq \pi / a.

In 5.48, n=0n = 0 is the trivial mode in which all the beads move up and down together. This is possible because there is no restoring force at all when all the beads move together. As discussed above (see 5.40) the beads can all move with a constant velocity because ω=0\omega = 0 for this mode. Note that case 2, above, gives the same mode, and nothing else, because if kx1kx0=2nπk x_{1}-k x_{0}=2 n \pi, then 5.44 has the same value for all xjx_{j}. The remaining modes are shown in Figures 5.14-5.16Figures \text { } 5.14 \text{-} 5.16. This system is illustrated in program 5-3 on the program disk.

n = 1, A_{j}=\cos [(j-1 / 2) \pi / 4].

Figure 5.14:n=1n = 1, Aj=cos[(j1/2)π/4]A_{j}=\cos [(j-1 / 2) \pi / 4].

n = 2, A_{j}=\cos [(j-1 / 2) 2 \pi / 4].

Figure 5.15:n=2n = 2, Aj=cos[(j1/2)2π/4]A_{j}=\cos [(j-1 / 2) 2 \pi / 4].

5.5: Forced Oscillations and Boundary Conditions

Forced oscillations can be analyzed using the methods of chapter 3. This always works, even for a force that acts on each of the parts of the system independently. Very often, however, for a space translation invariant system, we are interested in a different sort of forced oscillation problem, one in which the external force acts only at one end (or both ends). In this case, we can solve the problem in a much simpler way using boundary conditions. An example of this sort is shown in Figure 5.17.

n = 3, A_{j}=\cos [(j-1 / 2) 3 \pi / 4] ..

Figure 5.16:n=3n = 3, Aj=cos[(j1/2)3π/4].A_{j}=\cos [(j-1 / 2) 3 \pi / 4] ..

A forced oscillation problem in a space translation invariant system.

Figure 5.17:A forced oscillation problem in a space translation invariant system.

This is the system of 5.1, except that one wall has been removed and the end of the spring is constrained by some external agency to move back and forth with a displacement

zcosωdt.(5.47)z \cos \omega_{d} t . \tag{5.47}

As usual, in a forced oscillation problem, we first consider the driving term, in this case the fixed displacement of the N+1N + 1st block, 5.49, to be the real part of a complex exponential driving term,

zeiωdt.(5.48)z e^{-i \omega_{d} t} . \tag{5.48}

Then we look for a steady state solution in which the entire system is oscillating with the driving frequency ωd\omega_{d}, with the irreducible time dependence, eiωdte^{-i \omega_{d} t}.

If there is damping from a frictional force, no matter how small, this will be the steady state solution that survives after all the free oscillations have decayed away. We can find such solutions by the same sort of trick that we used to find the modes of free oscillation of the system. We look for modes of the infinite system and put them together to satisfy boundary conditions.

This situation is different from the free oscillation problem. In a typical free oscillation problem, the boundary conditions fix kk. Then we determine ω\omega from the dispersion relation. In this case, the boundary conditions determine ωd\omega_{d} instead. Now we must use the dispersion relation, 5.35, to find the wave number kk.

Solving 5.35 gives

k=1acos12Bωd22C.(5.49)k=\frac{1}{a} \cos ^{-1} \frac{2 B-\omega_{d}^{2}}{2 C} . \tag{5.49}

We must combine the modes of the infinite system, e±ikxe^{\pm i k x}, to satisfy the boundary conditions at x=0x = 0 and x=(N+1)a=Lx = (N + 1)a = L. As for the system 5.1, the condition that the system be stationary at x=0x = 0 leads to a mode of the form

ψ(x,t)=ysinkxeiωdt(5.50)\psi(x, t)=y \sin k x e^{-i \omega_{d} t} \tag{5.50}

for some amplitude yy. But now the condition at x=L=(N+1)ax = L = (N + 1)a determines not the wave number (that is already fixed by the dispersion relation), but the amplitude yy.

ψ(L,t)=ysinkLeiωdt=zeiωdt.(5.51)\psi(L, t)=y \sin k L e^{-i \omega_{d} t}=z e^{-i \omega_{d} t} . \tag{5.51}

Thus

y=zsinkL.(5.52)y=\frac{z}{\sin k L} . \tag{5.52}

Notice that if ωd\omega_{d} is a normal mode frequency of the system 5.1 with no damping, then 5.54 doesn’t make sense because sinkL\sin kL vanishes. That is as it should be. It corresponds to the infinite amplitude produced by a driving force on resonance with a normal frequency of a frictionless system. In the presence of damping, however, as we will discuss in chapter 8, the wave number kk is complex because the dispersion relation is complex. We will see later that if kk is complex, sinkL\sin kL cannot vanish. Even if the damping is very small, of course, we do not get a real infinity in the amplitude as we go to the resonance. Eventually, nonlinear effects take over. Whether it is nonlinearity or the damping that is more important near any given resonance depends on the details of the physical system.[4]

Forced Oscillations with a Free End

Forced oscillation of a mass on a spring.

Figure 5.18:Forced oscillation of a mass on a spring.

As another example, we will now discuss again the forced longitudinal oscillations of the simple system of a mass on a spring, shown in Figure 5.18. The physics here is the same as that of the system in Figure 2.9, except that to begin with, we will ignore damping. The block has mass mm. The spring has spring constant KK and equilibrium length aa. To be specific, imagine that this block sits on a nearly frictionless table, and that you are holding onto the other end of the spring, moving it back and forth along the table, parallel to the direction of the spring, with displacement

d0cosωdt.(5.53)d_{0} \cos \omega_{d} t . \tag{5.53}

The question is, how does the block move? We already know how to solve this problem from chapter 2. Now we will do it in a different way, using space translation invariance, local interactions and boundary conditions. It may seem surprising that we can treat this problem using the techniques we have developed to deal with space translation invariant systems, because there is only one block. Nevertheless, that is what we are going to do. Certainly nothing prevents us from extending this system to an infinite system by repeating the block-spring combination. The infinite system then has the dispersion relation of the beaded string (or of the coupled pendulum for \ell \rightarrow \infty):

ωd2=4Kmsin2ka2.(5.54)\omega_{d}^{2}=\frac{4 K}{m} \sin ^{2} \frac{k a}{2} . \tag{5.54}

The relevant part of the infinite system is shown in Figure 5.19. The point is that we can impose boundary conditions on the infinite system, Figure 5.19, that make it equivalent to Figure 5.18.

Part of the infinite system.

Figure 5.19:Part of the infinite system.

We begin by imagining that the displacement is complex, d0eiωdtd_{0} e^{-i \omega_{d} t}, so that at the end, we will take the real part to recover the real result of 5.55. Thus, we take

ψ2(t)=d0eiωdt.(5.55)\psi_{2}(t)=d_{0} e^{-i \omega_{d} t} . \tag{5.55}

Then to ensure that there is no force on block 1 from the imaginary spring on the left, we must take

ψ0(t)=ψ1(t).(5.56)\psi_{0}(t)=\psi_{1}(t) . \tag{5.56}

To satisfy 5.58, we can argue as in Figure 5.13 that

ψ(x,t)=z(t)coskx(5.57)\psi(x, t)=z(t) \cos k x \tag{5.57}
A better definition of the zero of x.

Figure 5.20:A better definition of the zero of xx.

where xx is defined as shown in Figure 5.20.

Now since the equilibrium position of block 2 is 3a/23 a / 2, we substitute

ψ2(t)=z(t)cos3ka2(5.58)\psi_{2}(t)=z(t) \cos \frac{3 k a}{2} \tag{5.58}

into 5.57, to obtain

z(t)=d0cos3ka2eiωdt.(5.59)z(t)=\frac{d_{0}}{\cos \frac{3 k a}{2}} e^{-i \omega_{d} t} . \tag{5.59}

Then the final result is

ψ1(t)=coska2cos3ka2d0eiωdt(5.60)\psi_{1}(t)=\frac{\cos \frac{k a}{2}}{\cos \frac{3 k a}{2}} d_{0} e^{-i \omega_{d} t} \tag{5.60}

or in real form

ψ1(l)=coska2cos3ka2d0cosωdl.(5.61)\psi_{1}(l)=\frac{\cos \frac{k a}{2}}{\cos \frac{3 k a}{2}} d_{0} \cos \omega_{d} l . \tag{5.61}

We can now use the dispersion relation. First use trigonometry,

cos3y=cos3y3cosysin2y=cosy(14sin2y)(5.62)\cos 3 y=\cos ^{3} y-3 \cos y \sin ^{2} y=\cos y\left(1-4 \sin ^{2} y\right) \tag{5.62}

to write

ψ1(t)=114sin2ka2d0cosωdt(5.63)\psi_{1}(t)=\frac{1}{1-4 \sin ^{2} \frac{k a}{2}} d_{0} \cos \omega_{d} t \tag{5.63}

or substituting 5.56,

ψ1(t)=ω02ω02ωd2d0cosωdt,(5.64)\psi_{1}(t)=\frac{\omega_{0}^{2}}{\omega_{0}^{2}-\omega_{d}^{2}} d_{0} \cos \omega_{d} t , \tag{5.64}

where ω0\omega_{0} is the free oscillation frequency of the system,

ω02=Km.(5.65)\omega_{0}^{2}=\frac{K}{m} . \tag{5.65}

This is exactly the same resonance formula that we got in chapter 2.

Generalization

The real advantage of the procedure we used to solve this problem is that it is easy to generalize it. For example, suppose we look at the system shown in Figure 5.21.

A system with two blocks.

Figure 5.21:A system with two blocks.

Here we can go to the same infinite system and argue that the solution is proportional to coskx\cos kx where xx is defined as shown in Figure 5.22. Then the same argument leads to the result for the displacements of blocks 1 and 2:

ψ1(t)=coska2cos5ka2d0cosωdt,ψ2(t)=cos3ka2cos5ka2d0cosωdt.(5.66)\psi_{1}(t)=\frac{\cos \frac{k a}{2}}{\cos \frac{5 k a}{2}} d_{0} \cos \omega_{d} t, \quad \psi_{2}(t)=\frac{\cos \frac{3 k a}{2}}{\cos \frac{5 k a}{2}} d_{0} \cos \omega_{d} t . \tag{5.66}

You should be able to generalize this to arbitrary numbers of blocks.

The infinite system.

Figure 5.22:The infinite system.


5.6: Coupled LC Circuits

We saw in chapter 1 the analogy between the LCLC circuit in Figure 1.10 and a corresponding system of a mass and springs in Figure 1.11. In this section, we discuss what happens when we put LCLC circuits together into a space translation invariant system.

For example, consider an infinite space translation invariant circuit, a piece of which is shown in Figure 5.23. One might guess, on the basis of the discussion in chapter 1, that the circuit in Figure 5.23 is analogous to the combination of springs and masses shown in

A an infinite system of coupled LC circuits.

Figure 5.23:A an infinite system of coupled LCLC circuits.

Figure 5.24, with the correspondence between the two systems being:

mLK1/CxjQj(5.67)\begin{aligned} m & \leftrightarrow \quad L \\ K & \leftrightarrow 1 / C \\ x_{j} & \leftrightarrow \quad Q_{j} \tag{5.67} \end{aligned}

where xjx_{j} is the displacement of the jjth block to the right and QjQ_{j} is the charge that has been “displaced” through the jjth inductor from the equilibrium situation with the capacitors uncharged. In fact, this is right, and we could use 5.69 to write down the dispersion relation for the Figure 5.23. However, with our powerful tools of linearity and space translation invariance, we can solve the problem from scratch without too much effort. The strategy will be to write down what we know the solution has to look like, from space translation invariance, and then work backwards to find the dispersion relation.

A mechanical system analogous to [Figure 5.23](#fig-5-23).

Figure 5.24:A mechanical system analogous to Figure 5.23.

The starting point should be familiar by now. Because the system is linear and space translation invariant, the modes of the infinite system are proportional to e±ikxe^{\pm i k x}. Therefore all physical quantities in a mode, voltages, charges, currents, whatever, must also be proportional to e±ikxe^{\pm i k x}. In this case the variable, xx, is really just a label. The electrical properties of the circuit do not depend very much on the disposition of the elements in space.6The dispersion relation will depend only on kaka, where aa is the separation between the identical parts of the system (see 5.35). However, it is easier to think about the system if it is physically laid out into a space translation invariant configuration, as shown in Figure 5.23.

A labeling for the infinite system of coupled LC circuits.

Figure 5.25:A labeling for the infinite system of coupled LCLC circuits.

In particular, let us label the inductors and capacitors as shown in Figure 5.25. Then the charge displaced through the jjth inductor in the mode with angular wave number, kk, is

Qj(t)=qeijkaeiωt(5.68)Q_{j}(t)=q e^{i j k a} e^{-i \omega t} \tag{5.68}

for some constant charge, qq. Note that we could just as well take the time dependence to be cosωt\cos \omega t, sinωt\sin \omega t, or eiωte^{i \omega t}. It does not matter for the argument below. What matters is that when we differentiate Qj(t)Q_{j}(t) twice with respect to time, we get ω2Qj(t)-\omega^{2} Q_{j}(t). The current through the jjth inductor is

Ij=ddtQj(t)=iωqeijkaeiωt.(5.69)I_{j}=\frac{d}{d t} Q_{j}(t)=-i \omega q e^{i j k a} e^{-i \omega t} . \tag{5.69}

The charge on the jjth capacitor, which we will call qjq_{j}, is also proportional to eijkaeiωte^{i j k a} e^{-i \omega t}, but in fact, we can also compute it directly. The charge, qjq_{j}, is just

qj=QjQj+1(5.70)q_{j}=Q_{j}-Q_{j+1} \tag{5.70}

because the charge displaced through the jjth inductor must either flow onto the jjth capacitor or be displaced through the j+1j + 1st inductor, so that Qj=qj+Qj+1Q_{j}=q_{j}+Q_{j+1}. Now we can compute the voltage, VjV_{j}, of each capacitor,

Vj=1C(QjQj+1)=qC(1eika)eijkaeiωt,(5.71)V_{j}=\frac{1}{C}\left(Q_{j}-Q_{j+1}\right)=\frac{q}{C}\left(1-e^{i k a}\right) e^{i j k a} e^{-i \omega t} , \tag{5.71}

and then compute the voltage drop across the inductors,

LdIjdt=Vj1Vj,(5.72)L \frac{d I_{j}}{d t}=V_{j-1}-V_{j} , \tag{5.72}

inserting 5.71 and 5.73 into 5.74, and dividing both sides by the common factor qLeijkaeiωt-q L e^{i j k a} e^{-i \omega t}, we get the dispersion relation,

ω2=1LC(1eika)(eika1)=4LCsin2ka2.(5.73)\omega^{2}=-\frac{1}{L C}\left(1-e^{i k a}\right)\left(e^{-i k a}-1\right)=\frac{4}{L C} \sin ^{2} \frac{k a}{2} . \tag{5.73}

This corresponds to 5.37 with B=1/LCB = 1 / LC. This is just what we expect from 5.69. We will call 5.75 the dispersion relation for coupled LCLC circuits.

Example of Coupled LCLC Circuits

A circuit with three inductors.

Figure 5.26:A circuit with three inductors.

Let us use the results of this section to study a finite example, with boundary conditions. Consider the circuit shown in Figure 5.26. This circuit in Figure 5.26 is analogous to the combination of springs and masses shown in Figure 5.27.

A mechanical system analogous to [Figure 5.26](#fig-5-26).

Figure 5.27:A mechanical system analogous to Figure 5.26.

We already know that this is true for the middle. It remains only to understand the boundary conditions at the ends. If we label the inductors as shown in Figure 5.28, then we can imagine that this system is part of the infinite system shown in Figure 5.23, with the charges constrained to satisfy

Q0=Q4=0.(5.74)Q_{0}=Q_{4}=0 . \tag{5.74}

This must be right. No charge can be displaced through inductors 0 and 4, because in Figure 5.26, they do not exist. This is just what we expect from the analogy to the system in 5.27, where the displacement of the 0 and 4 blocks must vanish, because they are taking the place of the fixed walls.

Now we can immediately write down the solution for the normal modes, in analogy with 5.21 and 5.22,

Qjsinjn4(5.75)Q_{j} \propto \sin \frac{j n}{4} \tag{5.75}
A labeling of the inductors in [Figure 5.26](#fig-5-26).

Figure 5.28:A labeling of the inductors in Figure 5.26.

for nn = 1 to 3.

Forced Oscillation Problem for Coupled LCLC Circuits

A forced oscillation with three inductors.

Figure 5.29:A forced oscillation with three inductors.

One more somewhat more practical example may be instructive. Consider the circuit shown in Figure 5.29. The Figure in Figure 5.29 stands for a source of harmonically varying voltage. We will assume that the voltage at this point in the circuit is fixed by the source, Figure, to be

Vcosωt.(5.76)V \cos \omega t . \tag{5.76}

We would like to find the voltages at the other nodes of the system, as shown in Figure 5.30, with

V3Vcosωt.(5.77)V_{3}-V \cos \omega t . \tag{5.77}

We could solve this problem using the displaced charges, however, it is a little easier to use the fact that all the physical quantities in the infinite system in Figure 5.23 are proportional to eikxe^{i k x} in a mode with angular wave number kk. Because this is a forced oscillation problem (and because, as usual, we are ignoring possible free oscillations of the system and looking for the steady state solution), kk is determined from ω\omega, by the dispersion relation for the infinite system of coupled LCLC circuits, 5.75.

The other thing we need is that

V0=0,(5.78)V_{0}=0 , \tag{5.78}
The voltages in the system of [Figure 5.29](#fig-5-29).

Figure 5.30:The voltages in the system of Figure 5.29.

because the circuit is shorted out at the end. Thus we must combine the two modes of the infinite system, e±ikxe^{\pm i k x}, into sinkx\sin kx, and the solution has the form

Vjsinjka.(5.79)V_{j} \propto \sin j k a . \tag{5.79}

We can satisfy the boundary condition at the other end by taking

Vj=Vsin3kasinjkacosωt.(5.80)V_{j}=\frac{V}{\sin 3 k a} \sin j k a \cos \omega t . \tag{5.80}

This is the solution.


6This is not exactly true, however. Relativity imposes constraints. See chapter 11.

Problems

Footnotes
  1. Zero does not work for β\beta because the eigenvalue equation has no solution.

  2. See appendix CC.

  3. More precisely, the string has a very large and nonlinear force constant for longitudinal stretching. The longitudinal oscillations have a much higher frequency and are much more strongly damped than the transverse oscillations, so we can ignore them in the frequency range of the transverse modes. See the discussion of the “light” massive spring in chapter 7.

  4. Note also that, when sinkL\sin kL is complex, the parts of the system do not all oscillate in phase, even though all oscillate at the same frequency.