Differential Equations for EngineersXYZ Homework Edition

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5.2 Application of Eigenfunction Series

The eigenfunction series can arise even from higher order equations. Consider an elastic beam (say made of steel). We will study the transversal vibrations of the beam. That is, suppose the beam lies along the xx-axis and let y(x,t)y(x,t) measure the displacement of the point xx on the beam at time tt. See Figure 1\PageIndex{1}.

A beam in the shape of an arc in the xy-plane.
Figure 1\PageIndex{1}: Transversal vibrations of a beam.

The equation that governs this setup is

a 4 4 y x 4 + 2 y t 2 = 0 , a^4 \frac{\partial^4y}{\partial x^4}+\frac{\partial^2y}{\partial t^2}=0, \nonumber

for some constant a>0a>0, let us not worry about the physics1.

Suppose the beam is of length 11 simply supported (hinged) at the ends. The beam is displaced by some function f(x)f(x) at time t=0t=0 and then let go (initial velocity is 00). Then yy satisfies:

a 4 y x x x x + y t t = 0 ( 0 < x < 1 , t > 0 ) , y ( 0 , t ) = y x x ( 0 , t ) = 0 , y ( 1 , t ) = y x x ( 1 , t ) = 0 , y ( x , 0 ) = f ( x ) , y t ( x , 0 ) = 0 . \begin{align} & a^4 y_{xxxx} + y_{tt} = 0 \qquad (0 < x < 1, \enspace t > 0),\nonumber \\ \label{eq:2} & y(0,t) = y_{xx}(0,t) = 0, \\ & y(1,t) = y_{xx}(1,t) = 0, \\ & y(x,0) = f(x), \qquad y_{t}(x,0) = 0.\nonumber \end{align} \nonumber

(5.2.1)

Again we try y(x,t)=X(x)T(t)y(x,t)=X(x)T(t) and plug in to get a4X(4)T+XT=0a^4X^{(4)}T+XT''=0 or

X ( 4 ) X = T a 4 T = λ . \frac{X^{(4)}}{X}=\frac{-T''}{a^4T}=\lambda. \nonumber

The equations are

T+λa4T=0,X(4)λX=0.T'' + \lambda a^4 T = 0, \qquad X^{(4)} - \lambda X = 0. \nonumber

The boundary conditions y(0,t)=yxx(0,t)=0y(0,t) = y_{xx}(0,t) = 0 and y(1,t)=yxx(1,t)=0y(1,t) = y_{xx}(1,t) = 0 imply

X(0)=X(0)=0,andX(1)=X(1)=0.X(0) = X''(0) = 0, \qquad \text{and} \qquad X(1) = X''(1) = 0. \nonumber

The initial homogeneous condition yt(x,0)=0y_t(x,0) = 0 implies

T(0)=0.T'(0) = 0. \nonumber

As usual, we leave the nonhomogeneous y(x,0)=f(x)y(x,0) = f(x) for later.

Considering the equation for TT, that is, T+λa4T=0T'' + \lambda a^4 T = 0, and physical intuition leads us to the fact that if λ\lambda is an eigenvalue then λ>0\lambda > 0: We expect vibration and not exponential growth nor decay in the tt direction (there is no friction in our model for instance). So there are no negative eigenvalues. Similarly λ=0\lambda = 0 is not an eigenvalue.

Write ω4=λ\omega^4=\lambda, so that we do not need to write the fourth root all the time. For XX we get the equation X(4)ω4X=0X^{(4)}- \omega^4X=0. The general solution is

X ( x ) = A e ω x + B e ω x + C sin ( ω x ) + D cos ( ω x ) . X(x)=Ae^{\omega x}+Be^{- \omega x}+C\sin(\omega x)+D\cos(\omega x). \nonumber

Now 0=X(0)A+B+D,0=X(0)=ω2(A+BD)0=X(0)A+B+D, 0=X''(0)=\omega^2(A+B-D). Hence, D=0D=0 and A+B=0A+B=0, or B=AB=-A. So we have

X ( x ) = A e ω x A e ω x + C sin ( ω x ) . X(x)=Ae^{\omega x}-Ae^{- \omega x}+C\sin(\omega x). \nonumber

Also 0=X(1)=A(eωeω)+Csinω0=X(1)=A(e^{\omega}-e^{- \omega})+C\sin \omega, and 0=X(1)=Aω2(eωeω)Cω2sinω0=X''(1)=A\omega^2(e^{\omega}-e^{- \omega})-C\omega^2\sin \omega. This means that Csinω=0C\sin \omega =0 and A(eωeω)=2Asinhω=0A(e^{\omega}-e^{- \omega})=2A\sinh \omega=0. If ω>0\omega >0, then ω0\omega \neq 0 and so A=0A=0. This means that C0C \neq 0 otherwise λ\lambda is not an eigenvalue. Also ω\omega must be an integer multiple of π\pi. Hence ω=nπ\omega =n\pi and n1n \geq 1 (as ω>0\omega >0). We can take C=1C=1. So the eigenvalues are λn=n4π4\lambda_n=n^4\pi^4 and the eigenfunctions are sin(nπx)\sin(n\pi x).

Now T+n4π4a4T=0T''+n^4\pi^4a^4T=0. The general solution is T(t)=Asin(n2π2a2t)+Bcos(n2π2a2t)T(t)=A\sin(n^2\pi^2a^2t)+B\cos(n^2\pi^2a^2t). But T(0)=0T'(0)=0 and hence we must have A=0A=0 and we can take B=1B=1 to make T(0)=1T(0)=1 for convenience. So our solutions are Tn(t)=cos(n2π2a2t)T_n(t)=\cos(n^2\pi^2a^2t).

As the eigenfunctions are just sines again, we can decompose the function f(x)f(x) on 0<x<10<x<1 using the sine series. We find numbers bnb_n such that for 0<x<10<x<1 we have

f ( x ) = n = 1 b n sin ( n π x ) . f(x)=\sum_{n=1}^{\infty}b_n\sin(n\pi x). \nonumber

Then the solution to (5.2.1) is

y ( x , t ) = n = 1 b n X n ( x ) T n ( t ) = n = 1 b n sin ( n π x ) cos ( n 2 π 2 a 2 t ) . y(x,t)=\sum_{n=1}^{\infty}b_nX_n(x)T_n(t)=\sum_{n=1}^{\infty}b_n\sin(n\pi x)\cos(n^2\pi^2a^2t). \nonumber

The point is that XnTnX_nT_n is a solution that satisfies all the homogeneous conditions (that is, all conditions except the initial position). And since and Tn(0)=1T_n(0)=1, we have

y ( x , 0 ) = n = 1 b n X n ( x ) T n ( 0 ) = n = 1 b n X n ( x ) = n = 1 b n sin ( n π x ) = f ( x ) . y(x,0)=\sum_{n=1}^{\infty}b_nX_n(x)T_n(0)=\sum_{n=1}^{\infty}b_nX_n(x)=\sum_{n=1}^{\infty}b_n\sin(n\pi x)=f(x). \nonumber

So y(x,t)y(x,t) solves (5.2.1).

The natural (circular) frequencies of the system are n2π2a2n^2\pi^2a^2. These frequencies are all integer multiples of the fundamental frequency π2a2\pi^2a^2, so we get a nice musical note. The exact frequencies and their amplitude are what we call the timbre of the note.

The timbre of a beam is different than for a vibrating string where we get “more” of the lower frequencies since we get all integer multiples, 1,2,3,4,5,1,2,3,4,5, \ldots. For a steel beam we get only the square multiples 1,4,9,16,25,1,4,9,16,25, \ldots. That is why when you hit a steel beam you hear a very pure sound. The sound of a xylophone or vibraphone is, therefore, very different from a guitar or piano.

There are other boundary conditions than just hinged ends. There are three basic possibilities: hinged, free, or fixed. Let us consider the end at x=0x=0. For the other end, it is the same idea. If the end is hinged, then

u(0,t)=uxx(0,t)=0.u(0,t) = u_{xx}(0,t) = 0. \nonumber

If the end is free, that is, it is just floating in air, then

uxx(0,t)=uxxx(0,t)=0.u_{xx}(0,t) = u_{xxx}(0,t) = 0. \nonumber

And finally, if the end is clamped or fixed, for example it is welded to a wall, then

u(0,t)=ux(0,t)=0.u(0,t) = u_{x}(0,t) = 0. \nonumber

Footnotes

[1] If you are interested, a4=EIρa^{4}=\frac{EI}{\rho}, where EE is the elastic modulus, II is the second moment of area of the cross section, and ρ\rho is linear density.

Adapted from Differential Equations for Engineers by Jiří Lebl (https://www.jirka.org/diffyqs/), © Jiří Lebl, licensed under CC BY-SA 4.0. Changes were made. License: CC-BY-SA-4.0.

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