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Chapter 15 Waves

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Chapter 15 Waves

CHAPTER NO.15 WAVES

 

18.1 INTRODUCTION

In the previcus Chapter, we studied the motion of objects oscillating in isolation. What happens in a system, which is a collection of such objects? A material medium provides such an exampke. Here, clastic forces bind the constituents to each other and, therefore, the motion of one affects that of the other. If you drop a little pebble in a pond of still water,the water surface gets disturbed. The disturbance does not remain confined to one place, but propagates outward along

a circle. If you continue dropping pebbles in the pond, you see circles rapidly moving outward from the point where the water surface is disturbed. It gives a feeling as if the water is

moving cutward from the point of disturbance. If you put some cork pieces on the disturbed surface, it is seen that the cork pieces move up and down but do not move away from the centre of disturbance. This shows that the water

mass does not flow outward with the circles, but rather a moving disturbance is created. Similarly, when we speak,

the sound moves outward from us, without any flow of air from one part of the medium to another. The disturbances

produced in air are much less obvious and only our ears or a microphone can detect them. These patterns, which move

without the actual physical transfer or flow of matter as a whole, are called waves. In this Chapter, we will study such waves.

 

Waves transport enemy and the pattern of disturbance has information that propagate from one point to another. All our communications essentially depend on transmission of sig-nals through waves. Speech means production of sound

waves in air and hearing amounts to their detection. Often,communication involves different kinds of waves. For exam-ple, sound waves may be first converted into an electric cur-rent signal which in tim may generate an electromagnetic wave that may be transmitted by an optical cable or via a

satellite. Detection of the original signal will usu-ally involve these steps in reverse order.

 

Not all waves require a medium for their

propagation. We know that light waves can travel through vacuum. The light emitted by stars, which are hundreds of light years away,Teaches us through inter-stellar space, which is practically a vacuum,

 

The most familiar type of waves such as waves ona string, water waves, sound waves, seismic waves, etc. ia the so-called mechanical waves.These waves require a medium for propagation,

they cannot propagate through vacuum. They involve oscillations of constituent particles and depend on the elastic properties of the medium.The electromagnetic waves that you will learn in Class XII are a different type of wave.Electromagnetic waves do not necessarily require a medium - they can travel through vacuiun.Light,radiowaves, X-rays, are all electromagnetic waves. In vacuum, all electromagnetic waves

have the same speed c, whose value ts :

¢= 299, 792, 458 ms". (15.1)

 

A third kind of wave is the so-called Matter waves. They are associated with constituents of matter: electrons, protons, neutrons, atoms and molecules. They arise in quantum mechanical

description of nature thet you will learn in your ater studies. Though conceptually mare abstract than mechanical or electro-magnetic waves, they have already found applications tn several devices basic to modern technology; matter waves associated with electrons are employed in electron microscopes.

 

In this chapter we will study mechanical

waves, which require a material medium for

their propagation.

 

The aesthetic influence of waves on art and Hterature is seen from very early times; yet the first scientific analysis of wave motion dates back te the seventeenth century. Some of the famous

scientists associated with the physics of wave motion are Christiaan Huygens (1629-1695),Robert Hooke and Isaac Newton. The understanding of physics of waves followed the physics of oscillations of masses tied to springs

and physics of the simple penduhumn. Waves in elastic media are intimately connected with harmonic oscillations. (Stretched strings, cofled springs, air, etc., are examples of elastic media).

 

We shall illustrate this connection throngh simple examples.

 

Consider a collection of springs connected to one another as shown tn Fig. 15.1. Ifthe apring at one end is pulled suddenly and released, the

disturbance travels to the other end. What has A :Pig. 15.1 A collection of springs connected to each other. The end A ts pulled suddenly generating a disturbance, which then propagates fo the other end.happened? The first spring 1s disturbed from its equilfprium length. Since the second spring ts

connected to the first, it is also stretched or compressed, and so on. The disturbance moves from one end to the other; but each spring only executes small oscillations about its equilibrium

posttion. As a practical example of this situation,consider a stationary train at a railway station. Different bogies of the train are coupled to cach

other through a spring coupling. When an

engine is attached at one end, ft gives a push to the bogie next. to it; this push is transmitted from one bogic to another without the entire train

being bodily displaced.

 

Now let us consider the propagation of sound waves in air. As the wave passes through atr, it compresses or expands a small region of air. This causes a change in the density of that region,

say dp, this change induces a change in pressure,dp, in that region. Pressure js force per unit area,so there is a restoring force proportional to

the disturbance, fust like in a spring. In this case, the quantity similar to extension or compression of the spring is the change in density. Ifa region is compressed, the molecules fn that region are packed together, and they tend

to move out to the adjoining region, thereby increasing the density or creating compression in the adjoining region. Consequently, the air in the first region undergoes rarefaction. If a

region is comparatively rarefied the surrounding air will rush in making the rarefaction move to the adjoining region. Thus, the compression or

rarefaction moves from one region to another,making the propagation of a disturbance possible in air.

 

In solids, similar arguments can be made. In a crystalline solid, atoms or group of atoms are arranged in a periodic lattice. In these, each

atom or group of atoms is in equilibrium, due to forces from the surrounding atoms. Displacing

one atom, keeping the othera fixed, leada to restoring forces, exactly as in a spring. So we can think of atoms in a lattice as end points,with springs between pairs of them.

 

In the anbsequent sections of this chapter we are going to discuss various characteristic properties of waves.

 

15.2 TRANSVERSE AND LONGITUDINAL

WAVES

We have seen that motion of mechanical waves involves oscillations of constituents of the medium. If the constituents of the medium oscillate perpendicular to the direction of wave

propagation, we call the wave a transverse wave.If they oscillate along the direction of wave propagation, we call the wave a longitudinal wave.

 

Fig.15.2 shows the propagation of a single pulse along a string, resulting from a single up and down jerk. If the string is very long compared 



to the size of the pulse, the pulse will damp out before it reaches the other end and reflection from that end may be ignored. Fig. 15.3 ahows a similar situation, but this time the external agent gives a continuous periodic sinusoidal 1p

and down jerk to one end of the string. The resulting disturbance on the string ‘s then a sinusoidal wave. In either case the elements of the string oscillate about their equilibrium mean

position as the pulse or wave passes through them. The oscillations are normal to the direction of wave motion along the string, so this is an example of transverse wave.

 

We can look at a wave in two ways. We can fix an instant of tine and picture the wave in space.This will give us the shape of the wave as a whole in space at a given instant. Another way is to fix a location ie. fix our attention on a particular element of string and see its oscillatory motion in time.

 

Fig. 15.4 describes the situation for

longitudinal waves in the most familiar example of the propagation of sound waves. A long pipe filled with air has a piston at one end. A single sudden push forward and pull back of the piston

will generate a pulse of condensations (higher density) and rarefactions {lower density) in the medium (air). Ifthe push-pull of the piston is continuous and periodic (sinusoidal), a sinusoidal wave will be generated propagating

in air along the length of the pipe. This is clearly an example of longitudinal waves.

 

The waves considered above, transverse or longitudinal, are travelling or progressive waves since they travel from one part of the medium to another. The material medium as a whole does not move, as already noted. A stream, for

example, constitutes motion of water as a whole.Ina water wave, it is the distirbance that moves,not water as a whole. Likewise a wind (motion of air as a whole) should not be confused with a sound wave which is a propagation of disturbance (in pressure density) in air, without the motion of air medium as a whole.

 

Mechanical waves are related to the elastic properties of the medium. In transverse waves,the constituents of the medium oacillate perpendicular to wave motion causing change is shape. That is, each element of the medium in subject to shearing stress. Solida and atrings

have shear modulus, that is they sustain

shearing stress. Fluids have no shape of their own - they yield to shearing streaa. This ts why transverse waves are possible in solids and strings (under tension) but not in fluids.However, solids as well as fluida have bulk

modulus, that is, they can sustain compressive strain. Since longitudinal waves involve compressive stress (pressure), they can be propagated through solids and fluids. Thus a

steel bar possessing both bulk and sheer elastic moduli can propagate longitudinal as well as transverse waves. But air can propagate only

longitudinal pressure waves (sound). When a medium such as a steel bar propagates both longitudinal and transverse waves, their apeeda

can be different since they arise from different elastic moduli.

 

Example 15.1 Gtven below are some

examples of wave motion. State in each case ifthe wave motion ts transverse, longttudinal or a combination of both:

 

(a) Motionofa kink na longitudinal spring produced by displacing one end of the spring sideways.

 

(b) Waves produced in a cylinder

containing a liquid by moving its piston

back and forth.

 

(c) Waves produced by a motorboat sailing in water.

 

(d) Ultrasonic waves in air produced by a vibrating quartz crystal.

Answer

(a) Transverse and longthudinal

(b) Longitudinal

(c) Transverse and longitudinal

(d) Longitudinal

 

 

18.3 DISPLACEMENT RELATION IN A

PROGRESSIVE WAVE

For mathematical deacription of a travelling ‘wave, we need a function of both position x and time t. Such a function at every instant should

give the shape of the wave at that instant. Also at every given location, it should describe the motion of the constituent of the medium at that

location. If we wish to deacribe a sinusoidal travelling wave (such as the one shown in Fig.15.3) the corresponding function must also be sinusoidal. For convenience, we shall take the

wave to be transverse ao that if the position of the constituents of the medium is denoted by x,the displacement from the equilibrium position

may be denoted by y. A sinusoidal travelling wave is then described by :

y(x,t) = asin(kx — wt + ) (15.2)

The term ¢ in the argument of sine function means equivalently that we are considering a linear combination of sine and cosine functions:y(«.t) = Asin(kx - wt) + Beos(kx -— at) (15.3)From Equations (15.2) and (15.3),

: { B a=VA2+ BP and $= tan (5)

 

To understand why Equation (15.2)

represents a sinusoidal travelling wave, take a fixed instant, say t = ¢,. Then the argument of the sine function in Equation (15.2) is simply kx + constant. Thus the shape of the wave (at any fixed instant) as a function of x is a sine wave. Similarly, take a fixed location, say x= x,.Then the argument of the sine function in Equation (15.2) is constant -wt. The displacement y, at a fixed location, thus varies sinusoidally with time. That is, the constituents

of the medium at different positions execute simple harmonic motion. Finally, as tincreases,xmust increase in the positive direction to keep kx-ot+9 constant. Thus Eq. (15.2) represents

a sinusiodal (harmonic) wave travelling along the positive direction of the x-axis. On the other hand, a function

y(x,t) = asin(kx + wt + 0) (15.4)

represents a wave travelling in the negative direction of x-axis. Fig. (15.5) gives the names of the various physical quantities appearing in Eq.

(15,2) that we now interpret.

 

Fig. 15.6 shows the plots of Eq. (15.2) for different values of time differing by cqual intervals of time. In a wave, the crest is the point of maximum positive displacement, the trough

is the point of maximum negative displacement.To see how a wave travels, we can fix attention ona crest and see how it progresses with time.In the figure, this is shown by a cross (x) on the crest. 



In the aame manner, we can see the motion of a particular constituent of the mediwun at a fixed location, say at the origin of the x-axis. This is shown by a solid dot (*) The plots of Fig. 15.6 show that with time, the solid dot (*) at the origin

moves periodically Le. the particle at the origin oscfilates about its mean position as the wave progresses. This is true for any other location also. We also see that during the time the solid

dot (*) has completed one full oscillation, the crest has moved further by a certain distance.Using the plots of Fig. 15.6, we now define the various quantities of Eq. (15.2).

 

15.3.1 Amplitude and Phase

In Eq. (15.2), since the sine function varies between 1 and -], the displacement y (x.§ varies between aand —a. We can take ato be a positive

constant, without any loss of  generality. Then a represents the maximum displacement of the constituents of the medium from their equilfbrium poattion. Note that the displacement

y may be positive or negative, but a is positive.It is called the amplitade of the wave.

 

The quantity (kx - wt + ¢ appearing as the argument of the sine function in Eq. (15.2) 1s called the phase of the wave. Given the amplitude a, the phase determines the displacement of the wave at any position and at any instant. Clearly ¢ is the phase at x= 0 and

t=0. Hence ¢ is called the initial phase angle.By suttable choice of origin on the x-axis and the intia] time, it 1s possible to have ¢=0. Thus there is no loss of generality in dropping 4, 1.c..

in taking Eq. (15.2) with ¢=0.

 

15.3.2 Wavelength and Angular Wave Number The minimum distance between two points having the same phase is called the wave length of the wave, usually denoted by 4. For simplicity,we can choose points of the same phase to be crests or troughs. The wavelength is then the distance between two consecutive crests or troughs in a wave. Taking ¢ = 0 in Eq. (15.2),the displacement at t= 0 is given by y(x,0) = asin kx (15.5)Since the sine function repeats its value after every 2x change in angle, siniex = sin(lex + 2nz) = sink | xX+ at

That is the displacements at points x and at x + 2nnr k are the same, where n=1,2,3,... The least distance between points with the same displacement (at any given instant of time) is obtained by taking n= 1. ), is then given by

, Qa Qa Azs ka .k A 015.6)k is the angular wave number or propagation

constant; its SI unit is radian per metre or rad m=* 15.3.3 Period, Angular Frequency and Frequency Fig. 15.7 shows again a sinusoidal plot. It describes not the shape of the wave at a certain

instant but the displacement of an element (at any fixed location) of the medium as a function of time. We may for, simplicity, take Eq. (15.2)

with ¢=0 and monitor the motion of the element say at x=(. We then get



‘y(0.t) = asin(-at)‘=-asinot

 Now the period of oscillation of the wave is the time it takes for an element to complete one full oscillation. That is -asinat =-asin a(t +T)‘=-a sin(@t + oT)Since sine function repeats after every 27,. , 2a @T=2n or OF - (15.7)


'@ 1s called the angular frequency of the wave.Its SI untts is rad s“. The frequency v is the number of oscillations per second. Therefore,

y nn 15.9)T 22 (15.8)'y is usually measured in hertz.

 

In the discussion above, reference has always been made to a wave travelling along a string or a transverse wave. In a longitudinal wave, the displacement of an element of the medium is parallel to the direction of propagation of the

wave. In Eq. (15.2), the displacement function for a longitudinal wave is written as.s{x, 9 = asin (loc— owt + ¢) (15.9)where s(x, i) is the displacement of an element of the medium in the direction of propagation of the wave at position xand time ¢. In Eq. (15.9),

ais the displacement amplitude; other

quantities have the same meaning as in case of a transverse wave except that the displacement function y (x, t) is to be replaced by the function s (x, é).

 

Example 15.2 A wave travelling along a

string is described by,yt, t) = 0.005 sin (80.0 x-3.0 4,in which the numerical constants are in SI units (0.005 m, 80.0 rad mm”, and 3.0 rad s°). Calculate (a) the amplitude,(b) the wavelength, and (c) the period and frequency of the wave. Also, calculate the displacement y of the wave at a distance x= 30.0 cm and time f= 208?

Answer On comparing this displacement

equation with Eq. (15.2),y (x. }= asin (kx ot),we find

{a) the amplitude of the wave is 0.005 m = 5 mm.

 

{b) the angular wave number k and angular frequency @ are k=80.0 mand #=3.0s"We then relate the wavelength A to k through Eq. (15.6),A=2n/k

oe 80.0 m™ = 7.85 cm

 

(c) Now we relate Tto w by the relation

T=2n/a om 3.0 s7]=2.09s and frequency, v = 1/T=0.48 Hz The displacement y at x = 30.0 cm and time t = 20 9 is given by

y =(0.005 m) sin (80.0 x 0.3 - 3.0 x 20)

= (0.005 m) sin (-36 + 12a)

= (0.005 m} sin (1.699)

= (0.005 m) sin (979 = 5 mm


16.4 THE 8PEED OF A TRAVELLING WAVE

To determine the speed of propagation of a travelling wave, we can fix our attention on any particular point on the wave (characterized by some value of the phase) and see how that point moves in time. It is convenient to look at the

motion of the crest of the wave. Fig. 15.8 gives the shape of the wave at two instants of time which differ by a small time internal At. The entire wave pattern is seen to shift to the right

(positive direction of x-axis) by a distance Ax In particular the crest shown by a cross () moves



 a distance Ax in time Aft, The speed of the wave

is then Ax/At. We can put the cross (x) on a point with any other phase. It will move with the same speed v {otherwise the wave pattern will not remain fixed). The motion of a fixed phase point

on the wave is given by kx—- ot = constant (15.10)Thus, as time t changes, the position x of the fixed phase point must change so that the phase remains constant. Thus kx- ot = ket AX — aft+Ab

ork Ax- @At=0 Taking Ax, Ait vanishingly small, this gives wk 2, (15.11)dt ik

Relating » to Tand k to A, we get

b= OR ava Om YT (15.12)Eq. (15.12), a general relation for all progressive waves, shows that in the time required for one full oscillation by any

constituent of the medium, the wave pattern travels a distance equal to the wavelength of the wave. It should be noted that the speed of a mechanical wave is determined by the inertial

(linear mass density for strings, mass density in general) and elastic properties (Young's modulus for near media/ shear moduhus, bulk modulus) of the medium. The medium determines the speed; Eq. (15.12) then relates

wavelength to frequency for the given speed. Of course, as remarked earlier, the medium can support both transverse and longitudinal waves,which will have different speeds in the same medium. Later in this chapter, we shall obtain

specific expressions for the speed of mechanical waves in some media.

 

15.4.1 Speed of a Transverse Wave on Stretched String

The speed of a mechanical wave is determined by the restoring force setup in the medium when it is disturbed and the inertial properties (mass density) of the medium. The speed is expected to

be directly related to the former and inversely to the latter. For waves on a string, the restoring force is provided by the tension Tin the string.The inertial property will in this case be Imear mass density jz, Which is mass m of the string divided by its length L. Using Newton's Laws of Motion, an exact formula for the wave speed on a string can be derived, but this derivation is

outside the scope of this book. We shall,therefore, use dimensional analysis. We already know that dimensional analysis alone can never

yield the exact formula. The overall

dimensionless constant is always left

undetermined by dimensional analysis.

 

The dimension of x is [ME"] and that of Tis like force, namely [MLT?]. We need to combine these dimensions to get the dimension of speed v [LT"]. Simple inspection shows that the quantity T/p has the relevant dimension [mur]

bod Lv T?

[ ML! | [ ]Thus if T and p are assumed to be the only relevant physical quantities,v=C fe (15.13)

 

where C is the undetermined constant of

dimensional analysis. In the exact formula, it turms out, C=1. The speed of transverse waves on a stretched string is given by v= iE (15.14)Note the important point that the apeed uv

depends only on the properties of the medium T and y (T ia a property of the stretched string arising due to an external force). It does not depend on wave length or frequency of the wave

ftself. In higher studies, you will come across waves whose speed is not independent of frequency of the wave. Of the two parameters 4 and y the source of disturbance determines the frequency of the wave generated. Given the speed of the wave in the medium and the frequency Eq. (15.12) then fixea the wavelength

Aaa (15.15)Example 15.3 Astee! wire 0.72 m long has amass of 5.0 x10 kg. If the wire is under a tension of 60 N, what is the speed of transverse waves on the wire ?

You can casily sce the motion of a pulsc on a rope. You can also sce ite reflection from a rigid boundary and measure its velocity of travel.You will uced a rope of diameter 1 to 3 cm, two hooks and some weights. You can perform this experiment in your classroom or

laboratory.

 

Take a long rope or thick string of diameter 1 to 3 cm, and tc it to

hooks on opposite walls in a hall or laboratory. Let one and pass on

a hook and hang some weight (about 1 to 5 k@ to itt. The walls may be about 3 to 5 m apart.Take a stick or a rod and strike the rope hard at a point ncar once end. This creates a pulse on the rope which now travels on it. You

can sec it reaching the end and reficcting back from it. You can

check the phase relation between the incident pulec and refiectod Pulse. You can casily watch two or threc  reflections before the pulse dica out. You can take a stopwatch and find the time for the pulsc to travel the diatance between the walls, and thus measure its velocity. Compare it with that obtained from Eq. (15.14).

 

This js also what happens with a thin metallic string of a musical instrument. The major difference is that the velocity on a string fa fairly high because of low mass per unit length, as compared to that on a thick rope. The low velocity on a rope allows us to watch the motion and make mcasurcaments beautifully.

Arsaver Maas per unit length of the wire,_5.0x10 kg #=—O 72m = 6.9 x10° kg m7"Tension, T= 60 N The speed of wave on the wire fs given by = [T = J GON = 5!

. i 6.9x10Skg nv! Ooms

 

16.4.2 Speed of a Longitudinal Wave (Speed of Sound)

In a longitudinal wave the constituents of the medium oscillate forward and backward in the direction of propagation of the wave. We have already seen that the sound waves travel in the form of compressions and rarefactions of small

volume elements ofair. The elastic property that determines the stress under compressional strain is the bulk moduhus of the medium defined

by (see chapter 9), AP B=-F (15.16) Here the change in pressure AP produces a

AV volumetric strain Vv" Bhas the same dimenaton @s pressure and given in SJ units in terms of pascal (Pa). The inertial property relevant for the

propagation of wave in the mass density p, with dimensions [ML*]. Simple inspection reveals that quantity 3/p has the relevant dimension:

[Mu 1? .[mui T"] =[V T?] (15.17)

[ML]Thus if Band p are considered to be the only relevant physical quantities,

v=c & (15.18)p where, as before, C is the undetermined constant from dimensional analysis. The exact derivation shows that C=1. Thus the general formula for Jongitudinal waves in a medium is: v= E (15.19)p

 

Fora linear medium lfke a solid bar, the lateral expansion of the bar is negligible and we may consider it to be only under longitudinal strain.In that case, the relevant modulus of elasticity

in Young's modulus, which has the same

dimension as the Bulk modulus. Dimensional analysis for this case is the same as before and yields a relation like Eq. (15.18), with an undetermined C which the exact derivation shows to be untty. Thus the speed of longitudinal

‘waves in a solid bar ie given by

Y v= je 15.20)& (15.20)


where Y is the Young's modulus of the material

of the bar. Table 15.1 gives the speed of sound in some media.Table 16.1 Speed of Sound in some Media 



Liquids and solids generally have higher speeds of sound than in gases. [Note for solids,

the speed being referred to is the speed of longitudinal waves in the solid]. This happens because they are much more difficult to compress than gases and so have much higher values of bulk modulus. This factor more than compensates for their higher densities than gases.We can estimate the speed of sound in a gas in

the ideal gas approximation. For an ideal gas,the pressure P, volume V and temperature T are related by (see Chapter 11).PV= Nk,T (15.21)where Nis the number of molecules in volume

V, k, is the Boltzmann constant and T the temperature of the gas (in Kelvin). Therefore, for an isothermal change it follows from Eq.(15.21)that VAP + PAV =0

or . AP P AV/V Hence, substituting in Eq. (15.16), we have B=P Therefore, from Eq. (15.19) the speed of a longitudinal wave in an ideal gas is given by,v= & (15.22)This relation was first given by Newton and is known as Newton's formula.

 

Example 15.4 Estimate the speed of

sound in air at standard temperature and

pressure. The mass of 1 mole of air is

29.0 x10 kg.

Answer We know that 1 mole of any gas

occupies 22.4 litres at STP. Therefore, density of air at STP is :

Pp, = (nass of one mole of air)/ (volume of one mole of air at STP)_ 29.0x10™ kg

22.4x107 m° = 1.29 kg m*

 

According to Newton’s formula for the speed of sound in a medium, we get for the speed of sound in air at STP,

pq | Odo N m™ Pf 1 “| 1.29kg m™* =280ms? (15.25)

 

The result shown in Eq.(15.23) is about 15% smaller as compared to the experimental value of 331 m s* as given in Table 15.1. Where did we go wrong ? If we examine the basic assumption made by Newton that the pressure variations in a medium during propagation of

sound are isothermal, we find that this is not correct. It was pointed out by Laplace that the pressure variations in the propagation of sound wavea are so fast that there is little time for the

heat flow to maintain constant temperature.These variations, therefore, are adiabatic and not isothermal. For adiabatic processes the ideal gas satisfies the relation,PV’ = conatant

Le. A(PV") =0 or PyVt" AV+ VTAP=0

Thus, for an ideal gas the adiabatic bulk modulus is given by,= AP

Baé 077 = yP where yis the ratio of two specific heats,C,/C,, The speed of sound is, therefore, given by,v= [re 15.

3 (15.24)This modification of Newton's formula is referred to as the Laplace correction. For air 7=7/5. Now using Eq. (15.24) to estimate the speed of sound in air at STP, we get a value 331.3 m a", which agrees with the measured speed.

 

16.6 THE PRINCIPLE OF SUPERPOSITION OF

WAVES

What happens when two wave pulses travelling in opposite directions cross each other? It turns out that wave pulses continue to retain their

identities after they have crossed. However,during the time they overlap, the wave pattern is different from either of the pulses. Figure 15.9

shows the situation when two pulaes of equal and oppostie shapes move towards each other.When the pulses overlap, the resultant displacement is the algebraic sum of the displacement due to each pulse. This is known as the principle of superposition of waves.According to this principle, each pulse moves as if others are not present. The constituents of

the medium therefore suffer displacments due to both and since displacements can be poattive and negative, the net displacement is an algebraic sum of the two. Fig. 15.9 gives graphs of the wave shape at different times. Note the dramatic effect in the graph (c); the displacements due to the two pulses have exactly 



cancelled each other and there is zero displacement throughout.To put the principle of superposition

mathematically, let y, (x9 and y, (x,9 be the displacements due to two wave disturbances in the medium. If the waves arrive in a region simultaneously and therefore, overlap, the net displacement. y (x, is given by

yi O= y,&O+ yl. 8 (15.25)If we have two or more waves moving in the medium the resultant waveform is the sum of

wave functions of individual waves. That is, if the wave functions of the moving waves are Y, =fv0,¥, = £008,UY, = J, O08 then the wave function describing the

disturbance in the medium is y= flx— 00+ £(x- v9+ ...+ flx— ud -E Jp Gory (15.26)

 

The principle of superposition is basic to the phenomenon of interference.For simplicity, consider two harmonic

travelling waves on a stretched string, both with the same (angular frequens) and k (wave number), and, therefore, the same wavelength A. Their wave speeds will be identical. Let us further assume that their amplitudes are equal

and they are both travelling in the positive direction of x-axis. The waves only differ in their initial phase. According to Eq. (15.2), the two

waves are described by the functions:

yx = aain (kx- of (15.27)and ylx, = asin (kx- mt + 9} (15.28)The net displacement is then, by the principle of superposition, given by y (& t) = aain (kx- mf + asin (kx- et + 9)(15.29)

nel ai] ee) *#) ot 2 2 (15.30)

 

where we have used the familiar trignometric identity for sin A+ sin B. We then have y(x,t)=2a cos sa(te—ar + Jason Eq. (15.31) is alao a harmonic travelling wave in the positive direction of x-axis, with the same

frequency and wave length. However, ita initial phase angle is a the algnificant thing is that its amplitude is a function of the phase difference ¢ between the constituent two waves:

A(@ = 2acoa 4% (15.32)For » = 0, when the waves are in phase,y(x,t}=2a sin(kr—- ar) (15.33)fe. the resultant wave has amplitude 2a, the largest possible value for A. For ¢=#, the 


waves are completely, out of phase and the reaultant wave has zero diaplacement

everywhere at all times y (&f) =0 (15.34) Eq. (15.33) refers to the so-called constructive interference of the two waves where the amplitudes add up in

the resultant wave. Eq. (15.34)

is the case of destructive intereference where the amplitudes subtract out in the

resultant wave. Fig. 15.10 shows these two caaes of interference of wavea arising from the principle of superposition.

 

15.6 REFLECTION or WAVES

So far we considered waves propagating in an unbounded medium. What happens if a pulse or a wave meets a boundary? If the boundary is rigid, the pulse or wave gets reflected. The phenomenon of echo is an example of reflection by a rigid boundary. If the boundary is not completely rigid or is an interface between two different elastic media, the situation is some what complicated. A part of the inckient wave is reflected and a part is transmitted into the

second medium. Ifa wave is incident obliquely on the boundary between two different media the transmitted wave is called the refracted wave. The incident and refracted waves obey Snell's law of refraction, and the incident and

reflected waves obey the usual laws of

reflection.

 

Fig. 15.11 shows a pulse travelling along a stretched string and being reflected by the boundary. Assuming there is no absorption of energy by the boundary, the reflected wave has

the same shape as the incident pulse but it suffers a phase change of x or 180° on reflection.This is because the boundary is rigid and the disturbance must have zero displacement at all

times at the boundary. By the principle of superposition, this is possible only if the reflected and incident waves differ by a phase of x, so that the resultant displacement is zero. This

reasoning is based on boundary condition on a rigid wall. We can arrive at the same conclusion dynamically also. As the pulse arrives at the wall,it exerts a force on the wall. By Newton's Third

Law, the wall exerts an equal and opposite force on the string generating a reflected pulse that differs by a phase of x.

 


If on the other hend, the boundary point is not rigid but completely free to move (such as in the case of a string tied to a freely moving ring ona rod), the reflected pulse has the same phase

and amplitude (assuming no energy dissipation)as the incident pulse. The net maximum displacement at the boundary is then twice the amplitude of each pulse. An example of non- rigid

boundary is the open end of an organ pipe.

 

To summarize, a travelling wave or pulse

suffers a phase change of r on reflection at a Tigid boundary and no phase change on Teflection at an open boundary. To put this mathematically, let the Incident travelling wave

be y2 (x,t) = asin (kx a)At a rigid boundary, the reflected wave is given

by y,0< 0 = asin (kx- ost + x).=- asin (kx- ot) (15.35)At an open boundary, the reflected wave is given by y,0c 0 = asin (xc— oot + 0).= asin (kx- at) (15.36)

Clearly, at the rigid boundary, y= y, + y, =0 at all times.

 

16.6.1 Standing Waves and Normal Modes

We considered above reflection at one boundary.But there are familiar situations (a string fixed at either end or an air column in a pipe with

either end closed) in which reflection takes place at two or more boundaries. In a string, for example, a wave going to the right will get Teflected at one end, which in turn will travel and get reflected from the other end. This will

go on unt] there is a steady wave pattern set up on the string. Such wave patterns are called standing waves or stationary waves. To see this mathematically, consider a wave travelling along the positive direction of x-axis and a Teflected wave of the same amplitude and wavelength in the negative direction of x-axis.From Fg. (15.2) and (15.4), with ¢= 0, we get:

yx, t) = asin (kx at)y,0< t) = asin (kx + at)

 

The resultant wave on the string is, according to the principle of superposition:yi d= ule 8 tye 8

=a [sin (kx- mt) + sin (kx + at)]

Using the familiar trignometric identity

Sin (A+B) + Sin (A-B) = 2 sin A cosB we get,yl, ft] = 2asin kx cos at (15.37)

Note the tmportant difference in the wave pattern described by Eq. (15.37) from that described by Eq. (15.2) or Eq. (15.4). The terms kx and ot appear separately, not in the combination kx- wt, The amplitude of this wave is 2a sin kx. Thus in this wave pattern, the amplitude varies from potnt to point, but each element of the string oscillates with the same angular frequency or time period. There is no

phase difference between oscillations of different elements of the wave. The string as a whole vibrates in phase with differing amplitudes at different points. The wave pattern is neither

moving to the right nor to the left. Hence they are called standing or stationary waves. The amplitude is fixed at a given location but, as remarked earlier, it is different at different

locations. The points at which the amplitude is zero {l.c., where there is no motion at all) are nodes; the points at which the amplitude fs the largest are called antinedes. Fig. 15.12 shows

a stationary wave pattern resulting from

superposition of two travelling waves in opposite directions.

 

The most significant feature of stationary ‘waves ie that the boundary conditions constrain the possible wavelengths or frequencies of

vibration of the system. The system cannot oscillate with any arbitrary frequency (contrast this with a harmonic travelling wave), but is characterized by a set of natural frequencies or

normal modes of oscillation. Let ue determine these normal modes for a stretched string fixed at both ends.

First, from Eq. (15.37), the positions of nodes (where the amplitude ts zero) are given by sinkx=0. which implies

kx=nx n=0,1,2,3,...Stoce k =22// , we get nA x= in=0,1,2,3,... (15.38)

Clearly, the distance between any two

successive nodes is < in the same way, the 



positions of antinodes (where the amplitude is the largest) are given by the largest value of sin kx:lsin kxl = 1

which implies kx= (n+) xz;n=0,1,2,3,...

With k = 22/4, we get x=(n+ vy 4 ;n=0,1,2,3,... (15.39)Again the distance between any two consecutive antinodes ts 4. Eq. (15.38) can be applied to

the case of a stretched string of length L fixed at both ends. Taking one end to be at x= 0, the boundary conditions are that x = 0 and x= L are positions of nodes. The x = 0 condition is already satisfied. The x = L node condition

requires that the length L is related to 4 by L=n4; n=1,2,3,.. (15.40)Thus, the possible wavelengths of stationary waves are constrained by the relation

as ze; nH1,2,3,.. (15.41)n with corresponding frequencies ve 2 for n=1,2,3, (15.42)2L We have thus obtained the natural frequencies - the normal modes of oscillation of the system.

The loweat possible natural frequency of a system is called its fandamental mode or the first harmonic. For the stretched string fixed “v at efther end it is given by v= op’ responding to n= 1 of Eq. (15.42). Here v is the speed of

wave determined by the properties of the

medium. The n = 2 frequency is called the second harmonic; n = 3 is the third harmonic and so on. We can label the various harmonics by the symbol v, (n= 1, 2, sods Fig. 15.13 shows the first six harmonics of a stretched string

fixed at either end. A string need not vibrate in one of these modes

only. Generally, the vibration of a string will be a superposition of

different modes; some modes may be more strongly excited and some less. Musical instruments Ife sitar or violin are based on this principle. Where the string is plucked or bowed, determines

which modes are more prominent han others.Let us next consider normal modes

of oscillation of an air column with one end closed and the other open.

A glass tube partially filled with water fllustrates thie system. The

end in contact with water is a node,while the open end is an antinode.

At the node the pressure changes are the largest, while the displacement is minimum (zero). At the open end - the antinode, it is just the other way - least pressure change and maximum

amplitude of displacement. Taking the end in contact with water to be x= 0, the node condition (Eq. 15.38) is

already satisfied. If the other end x

= Lis an antinode, Eq. (15.39) gives

lla L= (n+ >) qforn=0, 1,2,3,...

The possible wavelengths are then restricted by the relation :

A= 4 _, forn=0, 1.2.3... (15.43)

(n + 1/2)The normal modes — the natural frequencies —of the system are

+) nn 801,23 18 vent a)op ine @ Be hay wre ove ( AA)The fundamental frequency corresponds to n=



0, and ia given by —— . The higher frequencies are odd harmonics, i.c., odd multiples of the

fundamental frequency : 3—, 5 ete.

Fig. 15.14 shows the first six odd harmonics of air column with one end closed and the other open. For a pipe open at both ends, each end is an antinode. It is then easily seen that an open air cohimn at both ends generates all harmonics (See Fig, 15.15).

 

The syatems above, strings and air columns,can also undergo forced oscillations (Chapter 14). If the external frequency is close to one of

the natural frequencies, the system shows resonance.

 

Normal modes of a circular membrane rigidly clamped to the circumference as in a tabla are determined by the boundary condition that no point on the circumference of the membrane vibrates. Estimation of the frequencies of normal modes of this system is more complex. This problem involves wave propagation in two dimensions. However, the underlying physics is the same.

 

Example 15.5 A pipe, 30.0 cm long, is

open at both ends. Which harmonic mode

of the pipe resonates a 1.1 kHz source? Will resonance with the same source be

observed if one end of the pipe is closed 7 Take the speed of sound in air as 330ms".

Answer The first harmonic frequency is given by Y= Z=77 (open pipe)where Lis the length of the pipe. The frequency

of its rth harmonic ts:v,= or for n=1, 2, 3, ... (open pipe)First few modes of an open pipe are shown in Fig. 15.14.



For L= 30.0 cm, v=330ms",‘nx 330 (ms™)

%.=  o6m = 550 ns Clearly, a source of frequency 1.1 kHz will resonate at v,, i.e. the second harmonic.

 

Now ifane end of the pipe is closed (Fig. 15.15),it follows from Eq. (14.50) that the fundamental frequency is

v,= Gra (pipe closed at one end)and only the odd numbered harmonics are present ;

“3p 7 v, = ~, v,= Fp + and 80 on.

 

For L = 30 cm and uv = 330 m a", the

fundamental frequency of the pipe closed at one end is 275 Hz and the source frequency corresponds to its fourth harmonic. Since this harmonic is not a posafble mode, no resonance will be observed with the source, the moment

one end is closed.

 

15.7 BEATS

‘Beats’ is an interesting phenomenon arising from interference of waves. When two harmonic sound waves of close (but not equal) frequencies 



are heard at the same time, we hear a sound of similar frequency (the average of two close

frequencies), but we hear something else also.We hear audibly distinct waxing and waning of the intensity of the sound, with a frequency equal] to the difference in the two close frequencies. Artists use this phenomenon often

while tuning their instruments with each other.They go on tuning until their sensitive ears do not detect any beats.

 

To see this mathematically, let us consider two harmonic sound waves of nearly equal angular frequency @, and m, and fix the location to be x = O for convenience. Eq. (15.2) with a suitable choice of phase ($ = */2 for each) and,

assuming equal amplitudes, gives

&, =acosa@t and s,=acos wt (15.45)

 

Here we have replaced the symbol y by s.

since we are referring to longitudinal not tranaverse displacement. Let m, be the (slightly)greater of the two frequencies. The resultant displacement is, by the principle of superposition,

$= 5,+5,=a(cos@,t+cos 9 Using the familiar trignometric identity for

cas A+ cosB, we get =2a cos Ait cos ant (15.46) which may be written as :

s=[2a cos wt] cos mt (15.47)If |e, -—a,1 <<a, w,, w, >>, th where a, = (@-%) and @, = (4+%)2 2 Now if we assume | @, —m,! <<o,, which means Musical Pillars

Temples often have some pillars portraying human figures playing musical instru- ments, but sekiom do these  pillars themse}ves produce music. At the Nellaiappar temple in Tamil Nadu,gentle taps on a cluster of pillars carved out ofa single piece of rock produce the basic notes of Indian classical music, viz. Sa, Re. Ga, Ma, Pa, Dha.Ni, Sa. Vibrations of these pillars depend on

elasticity of the stone used, tts density and shape.

 

Musical pillars are categorised into three types: The first is called the Shrati Pillar,as it can produce the basic notes — the “swaras”, The second type is the Gana Thoongal, which gencrates the basic tuncs that make up the “ragas”. The third variety ja the Laya Thoongal pillars that produce “taal” (beats) when tapped. The pillars at the Nellaiappar temple are a combination of the Shruti and Laya types.

 

Archacologists date the Nelliappar

temple to the 7th century and claim ft was built by successive mulers of the Pandyan dynasty.

 

The musical pillars of Nelliappar and

several other temples tn southern India like those at Hampi (picture), Kanyalommari, and Thinivananthapuram are unique to the country and have no parallel in any other part of the world.

@, >> @,, we can interpret Eq. (15.47) aa follows.The resultant wave is oscillating with the average angular frequency ,; however ita amplitude is not constant in time, unlike a pure harmonic wave. The amplitude is the largest when the term cos @,¢ takes ite limit +1 or —1. In other words, the intensity of the resultant wave waxes

and wanes with a frequency which is 2m, = @, - @,. Since m= 2av, the beat frequency v,_. is given by Voeat = V1 Ve (15.48)Fig. 15.16 illustrates the phenomenon of beats for two harmonic waves of frequencies 11 Hz and 9 Hz. The amplitude of the resultant wave shows beats at a frequency of 2 Hz.

 


Example 15.6 Two sitar strings Aand B

playing the note ‘Dha’ are slightly out of tune and produce beats of frequency 5 Hz. The tension of the string B is slightly increased and the beat frequency is found to decrease to 3 Hz. What is the original frequency of B if the frequency of A 1s 427 Hz?

Answer Increase in the tension of a string increases its frequency. If the original frequency of B (v,) were greater than that of A (v,), further

increase in v, should have resulted in an increase in the heat frequency. But the beat frequency is found to decrease. This shows that v, < v,. Since v,—- v, = 5 Hz, and v, = 427 Hz, weget v, = 422 Hz.

 

 

15.8 DOPPLER EFFECT

It is an everyday experience that the pitch (or frequency) of the whistle of a fast moving train Reflection of sound in an open pipe When ae high pressure pulse of air travelling down an open pipe

reaches the other end, its momentum

drags the air out into the open, where

pressure falls rapidly to the

atmospheric pressure. AS a result the air following after it in the tube is

pushed out. The low pressure at the end of the tube draws air from further up the tube.The air gets drawn towards the open end forcing the low pressure region to move upwards. As a result a pulse of high pressure air travelling down the tube turns into a pulse of fow pressure air travelling up the tube. We say a pressure wave has been reflected at the open end with a change in phase of 180°. Standing waves in an open pipe organ like the fhite is a result of this

phenomenon.Compare this with what happens when a pulse of high pressure air arrives at a closed end: it collides and as a result pushes the air back in the opposite direction. Here,we say that the pressure wave Js reflected,

with no change in phase.decreases as it recedes away. When we approach a stationary source of sound with high

speed, the pitch of the sound heard appears to be higher than that of the source. As the observer recedes away from the source, the observed pitch (or frequency) becomes lower than that of the source. This motion-related

frequency change is called Doppler effect. The Austrian physicist Johann Christian Doppler first proposed the effect in 1842. Buys Ballot in

Holland tested it experimentally in 1845.Doppler effect is a wave phenomenon, it holds not only for sound waves but also for electromagnetic waves. However, here we shall consider only sound waves.We shall analyse changes in frequency under three different situations: (1) observer is

stationary but the source is moving, (2) observer is moving but the source is stationary, and (3)both the observer and the source are moving.The situations (1) and (2) differ from each other

Decause of the absence or presence of relative motion between the observer and the medium.Most waves require a medium for their propagation; however, electromagnetic waves do not require any medium for propagation. If there

is no medium preaent, the Doppler shifts are same irrespective of whether the source moves or the observer moves, since there is no way of distinction between the two situations.

 

16.8.1 Source Moving ; Observer Stationary Let us choose the convention to take the direction from the observer to the source as the positive direction of velocity. Considera source S moving with velocity v, and an observer

who is stationary in a frame in which the medium is also at rest. Let the speed of a wave of angular frequency @ and period T, both measured by an observer at rest with respect to

the medtum, be v. We assume that the observer has a detector that counts every time a wave crest reaches it. As shown in Fig. 15.17, at time t = 0 the source is at point S,located at a distance L from the observer, and

emits a crest. This reaches the observer at 



time t, = L/v. 

At time t = T, the source has moved a distance u,T, and is at point S., located at a distance (L + v,T,) from the observer. At S.,, the

source emits a second crest. This reaches the observer at ty = T, +G+ at)

At time n T,, the source emits fta {n+1)® crest and this reaches the observer at time tor = NT {et nut) net Hence, in a time interval | + (+ net) -4 v v the observer's detector counts n cresta and the observer recorda the period of the wave as T given by T = et + (L+ nv.Ty) -E iin v v pg ele = vs = 1, (: + 2) (15.49)

 

Equation (15.49) may be rewritten in terms of the frequency v, that would be measured if the source and observer were stationary, and the frequency v observed when the source is moving, a5 v, Y'

veX% (: + =) (15.50)If v, is small compared with the wave speed u,taking binomial expansion to terms in first order in v,/v and neglecting higher power, Eq. (15.50)may be approximated, giving vey (: - 2) (15.51)For a source approaching the observer, we replace u, by -v, to get ve vfs *) (15.52)The observer thus measures a lower frequency

when the source recedes from him than he does when it ia at rest. He measures a higher frequency when the source approaches him.

 

18.8.2 Observer Moving; Source Stationary Now to derive the Doppler shift when the observer is moving with velocity v, towards the source and the source is at reat, we have to proceed in a different manner. We work in the

reference frame of the moving observer. In this reference frame the source and medium are approaching at speed uv, and the speed with which the wave approaches ia u, + v. Following a similar procedure as in the previous case, we find that the time interval between the arrival

of the first and the (n+1) th crests is

boa ~ t, Bn Ty ~ nwo Uy tv The observer thus, measures the period of the

wave to be vo yf Y% yel T, jr “ |

giving vy [1+] (15.53)Ls i is small, the Doppler shift is almost same whether it is the observer or the source moving since Eq. (15.53) and the approximate relation Eq. (15.51 ) are the same.


18.8.3 Both Source and Observer Moving

We will now derive a general expression for Doppler shift when both the source and theobserver are moving. As before, let us take the direction from the observer to the source as the positive direction. Let the source and the

observer be moving with velocities v, and uv,reapectively as shown in Fig.15.18. Suppose at time t = 0, the observer is at O, and the source

is at S,, O, being to the left of S,. The source emits a wave of velocity v, of frequency v and period 7, all measured by an observer at rest

with respect to the medium. Let L be the

distance between O, and S, at £ = 0, when the source emits the first crest. Now, since the observer is moving, the velocity of the wave relative to the observer is v+up. Therefore, the

firat creat reaches the observer at time t, = L/{v-+u,). At time t = T,, both the observer and the source have moved to their new poattions O, and S, respectively. The new distance between the observer and the source, O, S,, would be L+(u,— Vg) Tol. At S,, the source emits a second crest.

 


Application of Doppler effect The change in frequency caused by a moving objec due to Doppler effect ia used to measure the velocities in diverse areas such as military medical acience, astrophysica, etc, It is also uses by police te check over-speeding of vehicles.A sound wave or electromagnetic wave o known frequency is sent towards a moving object Some part of the wave is reflected from the objec and ite frequency is detected by the monitorin;

station, This change in frequency is called Dopple: ohift.It 19 used at airports to guide aircraft, and 11 the military to detect enemy aircraft

Astrophysicists use it to measure the velocitie of atara.

 

Doctors use it te study heart beata and bloa:flew in different parts of the body. Here they us:ulltrasonic waves, and in common practice, it 1 called sonography. Ultrasonic waves enter th

body of the person, some of them are reflecte back, and give information about motion of bloo and pulsation of heart valvea, as well as pulsation

of the heart of the foetus. In the case of heart the picture generated is called echocardiogram This reaches the observer at time.= T, + IL+ (¥,-v)T I /e +2)

At time nT, the source emits its {(n+1) th cre and this reaches the observer at time ta = NT, + (b+ nv, —vJT,)] /(v + v0)Hence, in a time interval £,,,, -t, i.e., ewnflt 0 EP a os fee ean VRS YE shen noe FEF shee ¢:the observer counts n crests and the observer records the period ofthe wave as equal to Tgiven by

T= fT, ( p Uso 7B fr exe Us D+ VEU,

(15.54)The frequency v observed by the observer is given by vay, fore “| (15.55)U+D,

 

Consider a passenger sitting in a train moving on a straight track. Suppose she hears a whistle sounded by the driver of the train. What frequency will she measure or hear? Here both the observer and the source are moving with

the same velocity, so there will be no shift in frequency and the passenger will note the natural frequency. But an observer outside who is stationary with respect to the track will note

a higher frequency if the train is approaching hfm and a lower frequency when it recedes from him.

 

Note that we have defined the direction from the observer to the source as the positive direction. Therefore, if the observer is moving towards the source, vu) has a positive (mumerical)value whereas if O is moving away from 5, vu,

has a negative value. On the other hand, if S is moving away from O, u, has a positive value whereas if it is moving towards O, v, has a negative value. The sound emitted by the source travels in all directions. It is that part of sound

coming towards the observer which the observer recefvea and detects. Therefore, the relative velocity of sound with respect to the observer is

o+u, in all cases.

 

Exampte 15.7 A rocket is moving at a

speed of 200 m s° towards a stationary

target. While moving, it emits a wave of

frequency 1000 Hz. Some of the sound

reaching the target gets reflected back to the rocket as an echo. Calculate (1) the frequency of the sound as detected by the target and (2) the frequency of the echo as detected by the rocket.

Answer (1) The observer is at rest and the source is moving with a speed of 200 m s“'. Since this is comparable with the velocity of sound,330 m s“, we must use Eq. (15.50) and not the approximate Eq. (15.51). Since the source is approaching a stationary target, v, = 0, and v,

must be replaced by -v,. Thus, we have

yl v =»)v= 1000 Hzx [1-200 ms'/330ms'P"

= 2540 Hz

 

{2) The target is now the source (because it is the source of echo) and the rocket’s detector is now the detector or observer (because it detects

echo). Thus, v, = 0 and v, has a posttive value.The frequency of the sound emitted by the source {the target) 1s v, the frequency intercepted by

the target and not v,. Therefore, the frequency as registered by the rocket is

U+0 v= ‘on o ] . v =2540 Hex 200ms” +330m Ss”330 ms = 4080 Hz

 

SUMMARY

1. Mechanical waves can exist in material media and are governed by Newton's Laws.

 

2 Transverse waves are waves in which the particles of the medium oscillate perpendicular to the direction of wave propagation.

 

3. Longitudinal waves are waves in which the particles of the medium oscillate along the direction of wave propagation.

 

4. Progressive wave is a wave that moves from one poimt of medium to another.

 

5. The displacementin a sinusoidal wave propagating in the positive x direction is given.by ylx $a sin(kx— wt + 9}

where a is the amplitude of the wave, kis the angular wave number, is the angular frequency, (kx —- wt + ¢) ts the phase, and ¢ ts the phase constant or phase angle.

 

6. Wavelength J of a progressive wave is the distance between two consecutive points of the same phase at a given time. In a stationary wave, it is twice the distance between two consecutive nodes or antinodes.

 

7.  Pertod T of oscillation of a wave ie defined as the time any element of the medium takes to move through one complete oscillation. It is related to the angular frequency ca through the relation pTalt a

 

8 Frequency v of a wave 1s defined as 1/T and 1s related to angular frequency by ar)v=— 20

 

9. Speed of a progressive wave ia given by y= 2 = * - iy

 

10. The speed of a transverse wave on a stretched string is eet by the properties of the string. The speed on a string with tenaion T and linear mase denaity jis v= f—

 

11. Sound waves are longitudinal mechanical waves that can travel through solids, liquids,or gases. The apeed v of sound wave in a fluid having bulk modulus Band denaity pis . E vcs [—

pf The speed of longitudinal waves in a metallic bar is t= j— Pp For gases, since B = yP, the speed of sound is

?on fe Pe

 

12. When two or more waves traverse the same medium, the displacement of any element of the medium ie the algebraic sum of the displacements due to cach wave. This is known as the principle of superposttion of waves yay Sx - vt)

ial

 

13. Two sinusoidal waves on the same string exhibit interference, adding or cancelling according to the principle of superposition. If the two are travelling in the same direction and have the same amplitude a and frequency but differ in phase by a phase constant ¢, the result is a aingle wave with the same frequency a:= 14] sinfex—ot +20 y lx, § [200s 59| sin( dex wt 59 If $=0 or an integral multiple of 22, the waves are cxactly in phase and the interference is constructive; if ¢= #, they are exactly out of phase and the interference is destructive.

 

14. Atravelling weve, at a rigid boundary or a closed end, is reflected with a phase reversal but the reflection at an open boundary takes place without any phase change.For an incident wave

yx. 0 = aain (hx — ot)the reflected wave at a rigid boundary is y.& § =— aain (lec + wt) For reflection at an open boundary u,bx.t) = @ ain (hoc + anf

 

15. The interference of two identical waves moving in oppoalte directions produces standing waves, For a string with fixed ends, the standing wave is given by y (x. § = Baain kx] cos at

Standing waves are characterised by fixed locations of zero displacement called nodes and fixed locations of maximum displacanents called antinodes. The separation between two consecutive nodes or antinodes is 4/2.Aatretched string of length L fixed at both the ends vibrates with frequencies given by

v-- n=12,3,..2 2L The set of frequencies given by the above relation are called the normal modes of oacillation of the system. The oacillation mode with lowest frequency is called the fundamental mode or the first harmonic. The second harmonic is the oacillation mode

with n= 2 and ao on.A pipe of length L with one end closed and other end open (such as air columns)vibrates with frequencies given by va(n+%) =, n=#0,1,2,3,..The set of frequencies represented by the above relation are the normal modes of oscillation of such a system. The lowest frequency given by v/4L is the fundamental mode or the first harmonic.

 

16. Astring of length L fixed at both ends or an air column closed at one end and open at the other end, vibratea with frequencies called ita normal modes. Each of these frequencies is a resonant frequency of the system.

 

17. Beats arise when two waves having slightly different frequencies, y, and v, and comparable amplitudes, are auperposed. The beat frequency is

Veeat = V; ~ Va

 

18. The Doppler effect ia a change in the obaerved frequency of a wave when the source and the observer O moves relative to the medium. For sound the observed frequency vis given in terms of the source frequency v, by v+ Yo

v=yv, | ——_ v tv,here via the speed of sound through the medium, v, is the velocity of obecrver relative to the medium, and v, ie the source velocity relative to the medium. In using this

formula, velocities in the direction OS should be treated as positive and those opposite to it should be taken to be negative.

 


POINTS TO PONDER

1. A-wave ia not motion of matter as a whole in a medtum. A wind is different from the sound wave in air. The former involves motion of afr from one place to the other. The latter involves compressions and rarefactions of layers of air.

 

2. Ina wave, energy and not the matter is transferred from one paint to the other.

 

3. Energy tranafer takes place becauae of the coupling through clastic forces between neighbouring oscillating parts af the medinm.

 

4 Tranaverse waves can propagate only nm medtum with shear modulus of elastictty,

Longitudinal wavea need bulk modulus of elasticity and are therefore, posaibie in all media, sclids, liquids and gases.

 

5. In a harmonic progressive wave of a given frequency all particles have the same amplitude but different phases at a given instant of time. In a stationary ware, all particles between two nodes have the same phase at a given instant but have different amplitudes.

 

6. Relative to an observer at rest in a medium the speed of a mechanical wave in that medhim (tj depends anly on elastic and other properties (auch aa masa denaity) of the medium. It does not depend on the veloctty af the source.

 

7. For an observer moving with velocity v, relative to the medium, the speed of a wave is obviously different from v and is given by ut v,.

 

EXERCISES

18.1 Astring of mass 2.50 kg is under a tension of 200 N. The length of the stretched string is 20.0 m. If the traneveree jerk is struck at one end of the string, how long does the disturbance take to reach the other end?

 

15.2 Astone dropped from the top of a tower of height 300 m high splashes into the water ofa pond near the base of the tower. When is the splash heard at the top Siven that the speed of sound in air ie 340 m s'7 (g = 9.8 m 84}

 

15.3 A steel wire haa a length of 12.0 m and a mass of 2.10 kg. What should be the tension in the wire so that speed of a transverse wave on the wire equals the speed of sound in dry air at 20°C = 343 ms".[xe

 

15.4 Use the formula t= to explain why the speed of sound in air P

(a) = ia independent of pressure,

(b) increases with temperature,

(c) mereages with humidity.

 

15.6 You have Icarnt that a travelling wave in one dimension is represented by a function y = f ix, } where x and ¢ must appear in the combination x -— vt or x+v Le.y =f (x + v @. Ie the converse truc? Examine if the following functions for y can possibly represent a travelling wave :

(a) (x—vt}* th) log [fx + v4/x](cc) 1/0e+ 04

 

15.6 A bat emits ultrasonic sound of frequency 1000 kHz in air. If the sound meets a water eurface, what is the wavelength of (a) the reflected aound, (b) the tranamftted sound? Speed of sound in air is 340 m s— and in water 14866 m s*.

 

15.7 Ahospital usea an ultrasonic scanner to locate tumours in a tlasue. What is the wavelength of sound in the tissue in which the speed of sound is 1.7 kam 5"? The operating frequency of the scanner is 4.2 MHz.

 

15.8 A traneveree harmonic wave on a string is described by yx, 0 =3.0 sin (96 t + 0.018 x + 5/4)where x and y are in cm and fin s. The positive direction of x is from left to right.

 

(a) Ie this a travelling wave or a stationary wave ?If it ts travelling, what are the speed and direction of its propagation ?

 

(b) What are ite amplitude and frequency ?

 

(c) ‘What is the initial phase at the origin ?

 

(d) What ie the least distance between two successive crests in the wave 7?

 

15.9 For the wave described in Exercise 15.8, plot the displacement (yj versus (4 graphs for x =0, 2 and 4 cm. What are the ahapea of these graphs? In which aspects does the oscillatory motion in travelling wave differ from one paint to another: amplitude,frequency or phase ?

 

15.10 For the travellmg harmonic wave

ylx, § = 2.0 cos 2x (10t- 0.0080 c+ 0.35)where xand y are in cin and tin s. Calculate the phase difference between oscillatory motion of two pointe separated by a distance of fa) 4m,

fb) 0.5m,(c)  A/2,(aq) ava

 

15.11 ‘The transverse displacement of a string (clamped at its both ends) ts given by ‘(aR yx, § = 0.06 ain (=. con (120 79 where «and y are in m and tin s. The length of the string is 1.5 m and its mass is 3.0 x10%kg,

Answer the following :a) Does the function represent a travelling wave or a stationary wave?


(b) Interpret the wave as a  uperposition of two waves travelling in opposite directions. What is the wavelength, frequency, and speed of each wave ?

 

(c) Determine the tension in the string.

 

16.12 @ For the wave on a string described in Exercise 15.11, do all the pointe on the string oscillate with the same (a) frequency. (b) phase, (c) amplitude? Explain your answers. (i) What is the amplitude of a point 0.375 m away from one end?

 

16,13 Given below are eome functione of x and {to represent the displacement (transverse or longitudinal) of an elastic wave. State which of these represent (i) a travelling wave, Gi) a stationary wave or (il) none at all:

(a) y=2 cos (3% ain (108

(b) y =2fx — vt

(c) y=3S ain (6x— 0.56 + 4 cos (6x — 0.60

d) yecos xsin t+ cos 2xain 2t

 

15.14 Awire stretched between two rigid supports vibrates in ite fundamental mode with a frequency of 45 Hz. The maas of the wire ia 3.5 x 10 kg and ite linear masa density ie 4.0x 107 kg m“. What is (a) the speed of a transverse wave on the string. and

(b) the tension in the string?

 

15.15 Ametre-long tube open at one end, with a movable piston at the other end, shows resonance with a fixed frequency source {a tuning fork of frequency 340 Hz) when the tube length is 25.5 cm or 79.3 cm. Estimate the speed of sound im afr at the temperature of the experiment. The edge effecte may be neglected.

 

15,16 A steel rod 100 cm long is clamped at ite middle. The fundamental frequency of longitudinal vibrations of the rod are given to be 2.53 kHz. What is the speed of sound in steel?

 

13.17 A pipe 20 cm long is closed at one end. Which harmonic mode of the pipe is

reaonantly excited by a 430 Hz source ? Will the same source be in resonance with the pipe if both ends are open? (speed of sound in afr is 340 m s*}.

 

15.18 Two sitar strings A and B playing the note ‘Ge’ are alightly out of tune and produce beats of frequency 6 Hz. The tension in the string A is slightly reduced and the heat frequency is found to reduce to 3 Hz. If the original frequency of A ia 824 Hz,what is the frequency of B?

 

13.19 Explain why (or how):

(a) ma sound wave, a displacement node ia a pressure antinode and vice versa,

 

(b) «= bats can ascertain distances, directions, nature, and aizes of the obstaclea without any “eyes”,

 

(c) a violin note and sitar note may have the same frequency, yet we can

distinguish between the two notes,

 

(d) solide can support both longitudinal] and transverse waves, but only longitudinal wavea can propagate in gasea, and

 

e) = the shape of a pulse gete distorted during propagation in a dispersive medium.

 

18.20 Atrain, standing at the outer signal of a railway station blows a whistle of frequency 400 Hz in etill air. @) What is the frequency of the whistle for a platform observer

when the train {a) approaches the platform with a speed of 10 m s", (b) recedes from the platform with a speed of 10 m 9‘? (i) What ia the speed of sound in cach case ? The speed of sound im atill air can be taken as 340 ms".

 

15.21 A train, standing in a station-yard, blows a whistle of frequency 400 Hz in atill air. The wind starte blowing in the direction from the yard to the station with a speed of 10 m s?. What are the frequency, wavelength, and speed of sound for an observer standing on the station's platform? Is the situation exactly identical to the case when the air is still and the observer runs towarda the yard at a speed of 10 m 8"? The speed of sound in still air can be taken as 340 m s*

 

Additional Exercises

15.22 A travelling harmonic wave on a string is described by yx. § = 7.5 sin (0.0050x +12 + 2/4)

(a)what are the displacement and velocity of oscillation of a point at x= 10cm, and t= 15? Is this velocity equal to the velocity of wave propagation?

 

(b) Locate the points of the string which have the same traneverse displacements and velocity as the x = 1 an point at (= 2 e, 53 and 11s.

 

15.23 A narrow sound pulee ffor example, a short pip by a whistle) is sent acroae a medium. (a) Does the pulse have a definite (i) frequency, i) wavelength, (ii) speed of propagation? (b) If the pulse rate is 1 after every 20 a, (that is the whistle is blown for a split of second after every 20 s}, is the frequency of the note produced by the whistle equal to 1/20 or 0.05 Hz ?

 

15.24 One end of a long string of linear mass denaity 8.0 x 10% kg mis connected to an.electrically driven tuning fork of frequency 256 Hz. The other end pasees over a pulley and is tied to a pan containing a mass of 90 kg. The pulley end absorhe all the incoming energy so that reflected waves at this end have negligible amplitude.At ¢= 0, the left end (fork end) of the string x = 0 has zero transverse displacement (y = 0) and is moving along posttive y-direction. The amplitude of the wave ia 5.0

om. Write down the transverse  displacement y as function of x and tthat deacribea the wave on the string.

 

15.26 ASONAR system fixed in a submarine operates at a frequency 40.0 kHz. An encmy submarine moves towards the SONAR with a speed of 360 km h™. What ia the

frequency of sound reflected by the submarine ? Take the speed of sound in water to be 1450 m a7.

 

15.26 Earthquakes generate sound waves inside the earth. Unlike a gas, the earth can experience both transverse (5) and longitudinal (P) sound waves. Typically the speed of S wave is about 4.0 km 3’, and that of P wave is 6.0 km s'. A selsmograph records Pand S- waves from an earthquake. The first P wave arrives 4 min before the first S wave. Assuming the waves travel in straight line, at what distance does the

earthquake occur ?

 

15.27 A bat is flitting about in a cave, navigating via ultrasonic beeps. Assume that the sound emission frequency of the bat is 40 kHz. During one fast swoop directly toward a flat wall surface, the bat is moving at 0.03 times the speed of sound in air.What frequency does the bat hear reflected off the wall 2?