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In this chapter, we apply the tools of the previous chapter to analyze some beautiful and interesting phenomena — shock waves and the Kelvin boat wake.

14.1: Boat Wakes

Combining our analysis of the dispersion relation of water and the discussion of section 11.5 and of group velocity in section 10.2.1 will allow us to give a simple interpretation of one of the most beautiful and subtle of all wave phenomena — the Kelvin wake.

Wakes

The general subject of wakes is very complicated. However, in the simplest case of motion with constant velocity, the symmetry of the system makes it possible to do a linear analysis rather simply. This will allow us to understand some of the most obvious features of the wake in a straightforward way, including the angle and the regular waves that appear along the wake, showing up at sunset like pearls on a string, as in Figure 14.2.2 While I do not think that there is much that is original in the treatment here, the approach is a little unusual,

Wakes at sea.<sup>1 </sup>(Public Domain; Christian Eskelund US Navy)

Figure 14.1:Wakes at sea.1(Public Domain; Christian Eskelund US Navy)

A wake at sunset.

Figure 14.2:A wake at sunset.

© Source unknown. All rights reserved. This content is excluded from our Creative Commons license. For more information, see https://ocw.mit.edu/help/faq-fair-use.

like the approach to diffraction in chapter 13), and I think it gives a useful slant not just on the wake, but also on the crucial concept of group velocity.

Linear analysis of the Kelvin wake

Consider an infinite ocean in the xx-yy plane with a boat (duck, whatever) moving with constant velocity v>0v > 0 along the xx axis. The path of the boat divides the surface of the ocean into two regions, related to one another by reflection in the path. We can therefore without loss of generality focus on the half-plane y>0y > 0. We will not try to describe in detail what goes on near the y=0y = 0 line. In many situations, this involves turbulance, and is well beyond the scope of a beginning waves course. But away from y=0y = 0, it is possible to apply a linear analysis, and think of the waves for y>0y > 0 as linear combinations of plane waves with appropriate boundary conditions along the y=0y = 0 line.3 We will assume that whatever happens near y=0y = 0 produces a localized disurbance on the yy axis that moves along with the boat. This is necessarily a wave packet involving a range of frequencies. The integration over all these frequencies gives rise to the wake. That is the plan. We will do this for some simple illustrative boundary conditions, and we will argue that much can be understood about the system that is independent of the details of the boundary condition. The idea is to make use of the fact that the disturbance is a wave packet, and understand the appropriate analog in this two dimensional situation of the group velocity by which wave packets move.

This system is invariant under simultaneous translations in space and time.

tt+τxx+vτ(14.1)t \rightarrow t+\tau \quad x \rightarrow x+v \tau \tag{14.1}

We are looking for a steady-state solution in which the only things going on are the waves induced by the motion of the boat. This solution should depend only on the combination

xvt(14.2)x-v t \tag{14.2}

and be invariant under 14.1. This means that the wake wave is stationary in a frame of reference moving along with the boat.

An equivalent (and perhaps more physical) way to say this is that the solution that describes only the waves produced by the moving boat is a linear combination of plane waves which are moving along with the boat in the xx direction — that is they have kx=ω/vk_{x}=\omega / v.

Either way, the general solution looks like

dωf(ω)ei[ω(tx/v)kyy](14.3)\int d \omega f(\omega) e^{-i\left[\omega(t-x / v)-k_{y} y\right]} \tag{14.3}

The function f(ω)f(\omega) describes the wave packet in frequency, and it is determined by the displacement of the wave packet at y=0y = 0 and t=0t = 0, through the Fourier transform

ψ(x)=dωf(ω)eiωx/vf(ω)=12πdτψ(vτ)eiωτ(14.4)\psi(x)=\int d \omega f(\omega) e^{i \omega x / v} \Rightarrow f(\omega)=\frac{1}{2 \pi} \int d \tau \psi(v \tau) e^{-i \omega \tau} \tag{14.4}

The relation between ω\omega and

k=kx2+ky2(14.5)k=\sqrt{k_{x}^{2}+k_{y}^{2}} \tag{14.5}

is given by the dispersion relation for water waves. It will turn out that it is usually a good approximation to ignore surface tension, so will use a simple approximation in which the dispersion relation depends only on gravity. We will also assume that the water is deep. Then the dispersion relation is simply

ω2=gk(14.6)\omega^{2}=g k \tag{14.6}

The magnitude of the phase velocity is thus

vϕ=ωk=gω(14.7)v_{\phi}=\frac{\omega}{k}=\frac{g}{\omega} \tag{14.7}

Note that coefficient of the right hand side in the dispersion depends on the details of the physics, but the overall structure of the relation follows simply from dimensional analysis. The only combination of gg and kk with units of ω2\omega^{2} is gg kk.

For 14.3, we have

k=(kx2+ky2)1/2(14.8)k=\left(k_{x}^{2}+k_{y}^{2}\right)^{1 / 2} \tag{14.8}

with

kx=ω/v(14.9)k_{x}=\omega / v \tag{14.9}

Thus

ω4=g2(ω2/v2+ky2)ky=(ω4/g2ω2/v2)1/2(14.10)\begin{gathered} \omega^{4}=g^{2}\left(\omega^{2} / v^{2}+k_{y}^{2}\right) \\ k_{y}=\left(\omega^{4} / g^{2}-\omega^{2} / v^{2}\right)^{1 / 2} \tag{14.10} \end{gathered}

where the sign of the square-root is determined by the boundary condition at y=+y = +\infty. If kyk_{y} is real, ky/ωk_{y} / \omega is a positive number so that the phase waves in 14.3 propagate out from the y=0y = 0 line. If kyk_{y} is imaginary, it is i times a positive number, so that that the amplitude vanishes as y+y \rightarrow+\infty for y>0y > 0. These signs are opposite for y<0y < 0, but nothing else in the analysis changes, so the solution is symmetrical about y=0y = 0, as it must be.

Thus for y>0y > 0, we have

k=(kx,ky)=(ω/v,(ω4/g2ω2/v2)1/2)(14.11)\vec{k}=\left(k_{x}, k_{y}\right)=\left(\omega / v,\left(\omega^{4} / g^{2}-\omega^{2} / v^{2}\right)^{1 / 2}\right) \tag{14.11}

and

k=(kx,ky)=(ω/v,(ω4/g2ω2/v2)1/2)(14.12)\vec{k}=\left(k_{x}, k_{y}\right)=\left(\omega / v,\left(\omega^{4} / g^{2}-\omega^{2} / v^{2}\right)^{1 / 2}\right) \tag{14.12}

This is the key to the Kelvin wake. The different frequency components of the wave packet at y=0y = 0 travel in different directions as they move away from the boat for y>0y > 0.

A wake constructed numerically from [14.3](#eq-14-3) for f(\omega)=e^{-\omega^{2} v / g}.

Figure 14.3:A wake constructed numerically from 14.3 for f(ω)=eω2v/gf(\omega)=e^{-\omega^{2} v / g}.

Another view of the wake in [Figure 14.3](#fig-14-3).

Figure 14.4:Another view of the wake in Figure 14.3.

We note in passing that the vector quantity k/ω\vec{k} / \omega is a very important one, and it should probably have some important sounding name. It is sometimes called the “slowness vector” in the literature. This is the object that most naturally appears in the description of a plane wave with frequency ω\omega:

eiω(trk/ω)(14.13)e^{-i \omega(t-\vec{r} \cdot \vec{k} / \omega)} \tag{14.13}

“Slowness vector” does not seem to me to capture adequately the relation of this with the phase velocity, so I plan to start a campaign to call k/ω\vec{k} / \omega the “phase segnocity”

sϕ=kω(14.14)\vec{s}_{\phi}=\frac{\vec{k}}{\omega} \tag{14.14}

from the Latin segnis meaning slow, because the segnocity increases in magnitude as the points of constant phase on the wave move more slowly.4 The phase velocity itself can be easily constructed from the phase segnocity, 14.13, but it is really 14.13 that appears naturally in the equations.

We can calculate f(ω)f(\omega) given a boundary condition at t=y=0t = y = 0, and then construct the wake numerically using 14.3. For illustration, consider a Gaussian f(ω)f(\omega),

f(ω)=eω2v/g(14.15)f(\omega)=e^{-\omega^{2} v / g} \tag{14.15}

which corresponds to a gaussian disturbance along y=0y = 0. The resulting wake pattern is shown in Figures 14.3Figures \text { } 14.3 and 14.4. This looks like a wake! Thus we seem to have captured some of the essential physics of the wake in 14.3.

But what we are really interested in are the more general properties that will allow us to understand the key features of the wake without any numerical integration. We will look at how the various plane-wave components propagate. 14.11 implies that the wake waves propagate away from y=0y = 0 only for

ω2>g2/v2(14.16)\omega^{2}>g^{2} / v^{2} \tag{14.16}

We now need to think carefully about the physics of 14.3 and 14.12-14.13. In any small range of ω\omega, the integration over ω\omega will produce some kind of wave packet that moves along with the boat. Different ω\omega ranges are associated with wave packets moving out at different angles from the xx axis. The envelope of a wave packet in a narrow range of frequency centered on ω\omega will move at the effective group velocity, vgv_{g}, constructed as follows

sg=kω=v^gvg=(1v,2ω3/g2ω/v2(ω4/g2ω2/v2)1/2)(14.17)\vec{s}_{g}=\frac{\partial \vec{k}}{\partial \omega}=\frac{\hat{v}_{g}}{\left|\vec{v}_{g}\right|}=\left(\frac{1}{v}, \frac{2 \omega^{3} / g^{2}-\omega / v^{2}}{\left(\omega^{4} / g^{2}-\omega^{2} / v^{2}\right)^{1 / 2}}\right) \tag{14.17}

and this determines the angle of the wave packet as a function of ω\omega. Again, as with 14.13, the object in 14.18 is very important and deserves a fancy name. I am going to call it the “group segnocity,” sg\vec{s}_{g}, because the envelope of the wave group moves more slowly as sg\vec{s}_{g} increases. Suggestions for better names for sϕ\vec{s}_{\phi} and sg\vec{s}_{g} are welcome.

At this point, the reader may (justifiably) wonder why the group velocity is not the conventional group velocity for water waves,

Vg=ωk(14.18)V_{g}=\frac{\partial \omega}{\partial k} \tag{14.18}

where the relation between ω\omega and kk is given by 14.6 so that

Vg=g2ω=vϕ2(14.19)V_{g}=\frac{g}{2 \omega}=\frac{v_{\phi}}{2} \tag{14.19}

This gives a group velocity in the same direction as the phase velocity and just half the magnitude. To understand the difference, we must generalize the the formula for group velocity in section 10.2.1. There we saw that simplest way to understand group velocity is to think about the superposition of two plane waves that are close together in both ω\omega and k\vec{k}

cos(ω1tk1r)+cos(ω2tk2r)=2cos(ω1ω22tk1k22r)cos(ω1+ω22tk1+k22r)(14.20)\begin{gathered} \cos \left(\omega_{1} t-\vec{k}_{1} \cdot \vec{r}\right)+\cos \left(\omega_{2} t-\vec{k}_{2} \cdot \vec{r}\right) \\ =2 \cos \left(\frac{\omega_{1}-\omega_{2}}{2} t-\frac{\vec{k}_{1}-\vec{k}_{2}}{2} \cdot \vec{r}\right) \cos \left(\frac{\omega_{1}+\omega_{2}}{2} t-\frac{\vec{k}_{1}+\vec{k}_{2}}{2} \cdot \vec{r}\right) \tag{14.20} \end{gathered}

If the ωs\omega s and ks\vec{k} s are close together, the first factor is a slowly oscillating envelope, like the envelope of the wave packet, with segnocity vector

s=k1k2ω1ω2(14.21)\vec{s}_{-}=\frac{\vec{k}_{1}-\vec{k}_{2}}{\omega_{1}-\omega_{2}} \tag{14.21}

The second factor describes the more rapidly oscillating carrier wave, with segnocity vector

s+=k1+k2ω1+ω2(14.22)\vec{s}_{+}=\frac{\vec{k}_{1}+\vec{k}_{2}}{\omega_{1}+\omega_{2}} \tag{14.22}

If k1\vec{k}_{1} and k2\vec{k}_{2} arise from a well defined smooth function k(ω)\vec{k}(\omega),

k1=k(ω1) and k2=k(ω2)(14.23)\vec{k}_{1}=\vec{k}\left(\omega_{1}\right) \quad \text { and } \quad \vec{k}_{2}=\vec{k}\left(\omega_{2}\right) \tag{14.23}

then

limω1,ω2ωs=sg and limω1,ω2ωs+=sϕ(14.24)\lim _{\omega_{1}, \omega_{2} \rightarrow \omega} \vec{s}_{-}=\vec{s}_{g} \quad \text { and } \quad \lim _{\omega_{1}, \omega_{2} \rightarrow \omega} \vec{s}_{+}=\vec{s}_{\phi} \tag{14.24}

as expected from 14.18. But this depends on what is being held fixed between k1\vec{k}_{1} and k2\vec{k}_{2} as ω\omega changes. The point is the usual one that in one dimension, the dispersion relation determines k(ω)k(\omega) up to a sign. But in more than one dimension, infinitely many ks\vec{k} s satisfy the dispersion relation for a given ω\omega. We must specify exactly how the function k(ω)k(\omega) is determined before the limit in 14.25 is well defined. Thus 14.18 is the general formula for the group velocity. But what the derivative means (in more than one dimension) depends on the situation. The conventional physics assumes that all the frequency components of the wave are in the same direction. Then the direction of the k\vec{k} vector does not change with ω\omega, and 14.18 reduces to 14.19.5 But for a wave driven by the moving boat, what is held fixed is not the direction of the waves, but rather the xx component of the segnocity vector, kx/ωk_{x} / \omega, because all the components of the wave packet move along with the boat that produces them. Then the condition 14.9 and the dispersion relation 14.6 taken together force the direction of the k\vec{k} vector to change as a function of ω\omega. Thus we must use the general form, 14.18. As we will see, this implies that the effective group velocity not only has a very different magnitude from the conventional 14.20, but also that the effective group velocity and the phase velocity are not even in the same direction.

The red lines in Figure 14.5 show the position of the wave packet corresponding to ω=1.05g/v\omega = 1.05 g / v. The cyan vectors show the group velocities for y>0y > 0 and y<0y < 0. These are perpendicular to the lines of the wave packets. If we take the origin to be the position of the boat (either instantaneously or by going to a moving coordinate system in which the boat is stationary at the origin), The points r\vec{r} on the wave packet satisfy

rv^g=0(14.25)\vec{r} \cdot \hat{v}_{g}=0 \tag{14.25}
Wave packets (red) and phase waves (blue) for \omega \approx 1.05 \mathrm{~g} / \mathrm{v}.

Figure 14.5:Wave packets (red) and phase waves (blue) for ω1.05 g/v\omega \approx 1.05 \mathrm{~g} / \mathrm{v}.

Note also that because of 14.18,

rkω=0(14.26)\vec{r} \cdot \frac{\partial \vec{k}}{\partial \omega}=0 \tag{14.26}

But there is additional structure within the wave packet because of the phase waves. The phase velocities are shown by the green vectors, and are not in the same direction as the group velocity. Thus there are oscillations along the wave packet corresponding to maxima and minima of the phase waves. Assuming that the maximum occurs at the position of the boat (that we are taking to be the origin), the other maxima occur at

rjk=2πj for j=1 to (14.27)\vec{r}_{j} \cdot \vec{k}=-2 \pi j \quad \text { for } j=1 \text { to } \infty \tag{14.27}

These maxima represent the interaction of the plane wave with frequency omegaomega (and moving along with the boat) and the group wave packet, so we indicate them in the figure by blue lines of constant phase perpendicular to k\vec{k}.

Now we can build up a picture of the wake by putting these together for the range of important ω\omega. As ω\omega changes, the direction of the red wave packet lines and the blue phase waves will change according to 14.27 and 14.12. For ωg/v\omega \approx g / v, the wave packets are nearly horizontal and the phase waves are moving nearly horizontally. This is shown in Figure 14.6 for ω=1.001 g/v\omega=1.001 \mathrm{~g} / \mathrm{v}: As ω\omega increases, the angle of the wave packets increases for a while, giving a situation like that shown in Figure 14.5. But the interesting thing is that there is a critical value of ω\omega that gives the maximum angle for the group velocity.

It is particularly simple to analyze 14.18 because kx/ω\partial k_{x} / \partial \omega is constant. The ω\omega dependence of ky/ω\partial k_{y} / \partial \omega is shown in Figure 14.7 Because it goes to infinity as ωg/v\omega \rightarrow g / v and as ω\omega \rightarrow \infty, in these two limits the group velocity goes to zero, and its direction goes to y^\hat{y}. The minimum of ky/ω\partial k_{y} / \partial \omega corresponds to the maximum of vg\left|\vec{v}_{g}\right|, and also to the maximum angle of the wake wave propagation from the yy direction. This maximum angle is particularly important for two reasons. Not only does the maximum angle correspond to the edge of the

Wave packets (red) and phase waves (blue) for \omega \approx 1.001 \mathrm{~g} / \mathrm{v} ..

Figure 14.6:Wave packets (red) and phase waves (blue) for ω1.001 g/v.\omega \approx 1.001 \mathrm{~g} / \mathrm{v} ..

disturbance produced by the boat, but more importantly, at all smaller angles, the energy is spread over neighboring angles. At the maximum, because the angle is stationary with respect \omega, neighboring \omega contribute constructively and the wave at the edge is generically much more intense …

Figure 14.7:disturbance produced by the boat, but more importantly, at all smaller angles, the energy is spread over neighboring angles. At the maximum, because the angle is stationary with respect ω\omega, neighboring ω\omega contribute constructively and the wave at the edge is generically much more intense than for smaller angles.6

To determine the maximum angle explicitly, we differentiate ky/ω\partial k_{y} / \partial \omega again, which gives

2kyω2=(ω2/g2)(2ω4/g23ω2/v2)(ω4/g2ω2/v2)3/2(14.28)\frac{\partial^{2} k_{y}}{\partial \omega^{2}}=\frac{\left(\omega^{2} / g^{2}\right)\left(2 \omega^{4} / g^{2}-3 \omega^{2} / v^{2}\right)}{\left(\omega^{4} / g^{2}-\omega^{2} / v^{2}\right)^{3 / 2}} \tag{14.28}

so the minimum occurs at

ω2=3g22v2(14.29)\omega^{2}=\frac{3 g^{2}}{2 v^{2}} \tag{14.29}

corresponding to wave number

k=3g2v2(14.30)k=\frac{3 g}{2 v^{2}} \tag{14.30}

and magnitude of phase velocity

vϕ=23v(14.31)v_{\phi}=\sqrt{\frac{2}{3}} v \tag{14.31}

The direction of the phase velocity is is

v^ϕ=(23,13)(14.32)\hat{v}_{\phi}=\left(\sqrt{\frac{2}{3}}, \sqrt{\frac{1}{3}}\right) \tag{14.32}

at an angle from the xx axis of

θmax=arcsin(1/3)=35.26(14.33)\theta_{\max }=\arcsin (1 / \sqrt{3})=35.26^{\circ} \tag{14.33}

The wavelength is

λ=4πv23g(14.34)\lambda=\frac{4 \pi v^{2}}{3 g} \tag{14.34}

Even at low speeds like a meter per second (about 2 knots), this wavelength is large compared to the scale (a few centimeters) at which surface tension becomes important in the dispersion relation, so 14.6 is usually a good approximation.

Wave packets (red) and phase waves (blue) for the critical value \omega \approx \sqrt{3 / 2} g / v.

Figure 14.8:Wave packets (red) and phase waves (blue) for the critical value ω3/2g/v\omega \approx \sqrt{3 / 2} g / v.

At the critical angle, our wave packets and phase waves are shown in Figure 14.8. Often, as in the wakes in Figure 14.1, the phase waves along the maximum angle are all you see.

For ω\omega larger than 3/2g/v\sqrt{3 / 2} g / v, the wave packet angles starts to decrease again but the phase waves continue to get closer together, as shown in Figure 14.9 for ω=2g/v\omega=2 g / v.

We can now put these together for a range of ω\omega from g/vg / v up past the critical value. The result is shown in Figure 14.10. It may be easier to see what is happening if we do not draw the wave packets, but just the phase waves. These, after all, show the places where the oscillation is a maximum. The result is shown in Figure 14.11. This gives nearly the same

Wave packets (red) and phase waves (blue) for \omega \approx 2 g / v .

Figure 14.9:Wave packets (red) and phase waves (blue) for ω2g/v.\omega \approx 2 g / v .

Combined wave packets and phase waves for a range of frequencies.

Figure 14.10:Combined wave packets and phase waves for a range of frequencies.

picture as a parametric plot of the points on the waves packets where the phase waves have there maxima, which is shown in Figure 14.12. You should be able to recognize the basic features of Figure 14.11 both in our numerical construction, Figure 14.3 and in the beautiful picture of a real wake from Wikipedia shown in Figure 14.13 on page 436. We can make this even more obvious by rotating Figure 14.12 in three dimensions, as shown in Figure 14.14. In the wake in Figure 14.13, the phase waves are clearly visible both for small ω\omega (the forwardmoving waves in the center) and for large ω\omega (the outward-moving and closely spaced waves just inside the maximum angle). From Figure 14.11 and 14.13 you should be able to see why the phase waves are sometimes called “featherlet waves.” The phase waves for ω>3/2g/v\omega>\sqrt{3 / 2} g / v look like delicate feathers on the wing of the wake.

It is worth making one more comment about Figure 14.11. You have probably already noticed that the phase waves fit together into continuous curves. This is not an accident. Physically, of course, the position at which the oscillation is maximum must certainly vary

Combined phase waves for a range of frequencies.

Figure 14.11:Combined phase waves for a range of frequencies.

Parametric plot of the phase maxima.

Figure 14.12:Parametric plot of the phase maxima.

continuously as a function of ω\omega. But also, we can see that the tangent to the curve that describes the maxima is perpendicular to k\vec{k}, and thus our phase waves in the figures are just these tangents. To see this, note that from 14.27 and 14.28, rj\vec{r}_{j} satisfies

rjk=2πj and rjkω(14.35)\vec{r}_{j} \cdot \vec{k}=-2 \pi j \quad \text { and } \quad \vec{r}_{j} \cdot \frac{\partial \vec{k}}{\partial \omega} \tag{14.35}

Differentiating the first with respect to ω\omega and using the second gives

rjωk=0(14.36)\frac{\partial \vec{r}_{j}}{\partial \omega} \cdot \vec{k}=0 \tag{14.36}
Compare Figures \text { } 14.3 \text {, } 14.11 \text {, } 14.12 and 14.14 with a real wake.

Figure 14.13:Compare Figures 14.314.1114.12Figures \text { } 14.3 \text {, } 14.11 \text {, } 14.12 and 14.14 with a real wake.

© Source unknown. All rights reserved. This content is excluded from our Creative Commons license. For more information, see https://ocw.mit.edu/help/faq-fair-use.

3D Parametric plot of the phase maxima.

Figure 14.14:3D Parametric plot of the phase maxima.

which says that the tangent to the curve described parametrically by rj(ω)\vec{r}_{j}(\omega) is perpendicular to k\vec{k} and thus parallel to the phase waves.7

2 This is one of many beautiful photographs by Ian Alexander - http://easyweb.easynet.co.uk/ iany/patterns/wake.htm.

3 One could, if necessary, look only at y > a > 0 for some fixed a. This would not change the analysis in any essential way.

4 The inspiration for this comes from paleontologists, who have fossil evidence for the segnosaurus - “slow lizard” and also the velocisaurus - “fast lizard.”

5 It looks different because in 14.18 we are looking at the group segnocity rather than the group velocity, but it is an elementary exercise in calculus to get from one to the other.

6 This pile-up at a stationary point is the same phenomenon that picks out the angle at which we see the rainbow.

Problems