Chapter Summary
As we have already read, in a wave motion a physical quantity \(y\) is made to oscillate at one point and these oscillations of \(y\) propagate to other places also.
Therefore, in a wave, several particles oscillate (unlike SHM in which normally a single oscillates).
So, to determine the value of \(y\) (from its mean position between \(+A\) and \(-A\) ) we will have to tell the position of the particle and time. Thus,
\(
y=f(\text { position of particle, time })
\)
In three-dimensional space, the position of the particle can be represented by three variable coordinates. Thus, in general, \(y\) is a function of four variables, three in coordinates and the fourth one is time.
But in physics, we normally keep least number of variables. If the wave is one-dimensional, then position of the particle can be represented by a single variable co-ordinate (say \(x\) ).
Thus, in a one-dimensional wave \(y\) is a function of two variables \(x\) and \(t\). Here, \(x\) is used for the position of the particle and \(t\) for time or
\(
y=f(x, t)
\)
Note: When dealing with a function of multiple variables, such as y, partial differentiation is used to find the derivative with respect to one variable while holding the others constant. Examples include \(\partial y / \partial x, \partial y / \partial t\), and \(\partial^2 y /\) \(\partial x^2\).
For example: If \(y=x^2+2 x t+t^2\), then:
\(\partial y / \partial x=2 x+2 t\) (treating \(t\) as a constant)
\(\partial y / \partial t=2 x+2 t\) (treating \(x\) as a constant)
\(\partial^2 y / \partial x^2=2\) (treating \(t\) as a constant)
Obviously, all functions will not represent a wave function. Only those functions of \(x\) and \(t\) will represent a wave function which satisfies the following three conditions.
Condition 1: The given function must satisfy the following differential equation :
\(
\left(\frac{\partial^2 y}{\partial t^2}\right)=k\left(\frac{\partial^2 y}{\partial x^2}\right) \dots(i)
\)
Here, \(k\) is a constant which is equal to the square of the wave velocity or
\(
k=v^2
\)
where \(v\) is the wave speed
Condition 2: The wave function must be single-valued. For given values of \(x\) and \(t\) there should be only one value of \(y\).
Condition 3: The wave function and its first derivative must be continuous. Therefore, there should not be a sudden change in the value of \(y\) and its first derivative (in some cases it will be called slope).
The general solution of Eq. (i) discussed above is of the form :
\(
y(x, t)=f(a x \pm b t) \dots(ii)
\)
Thus, any function of \(x\) and \(t\) which satisfies Eq. (i) and which can be written as Eq. (ii) represents a wave, provided conditions (2) and (3) are also satisfied.
If \(y(x, t)\) function is of this type (as shown in eq (ii)), then the following two conclusions can be drawn.
Plane Progressive Wave
If oscillations of \(y\) are simple harmonic in nature then the wave is called a plane progressive wave. It is of two types,

General equation of progressive harmonic wave is,
\(
y=A \sin (\omega t \pm k x \pm \phi) \quad \text { or } \quad y=A \cos (\omega t \pm k x \pm \phi)
\)

In these equations,

Important Points:

Phase Difference [latex](\Delta \phi)\)
Energy in Wave Motion
In harmonic wave:
Energy density \(=\frac{\text { energy of oscillation }}{\text { volume }}\)
or \(u=\frac{E}{V}=\frac{\frac{1}{2} m \omega^2 A^2}{V}\)
But, \(\frac{m}{V}=\text { density or } \rho\)
\(\therefore u=\frac{1}{2} \rho \omega^2 A^2\)
Power : \(\mathrm{P}=\) (energy density) (volume/ time)=Energy transferred per unit
\(
P=\left(\frac{1}{2} \rho \omega^2 A^2\right)(S v)
\)
[where \(\mathrm{S}=\) Area of cross-section] \(v\) is velocity (wave speed).
Intensity: Energy transferred per unit cross-sectional area per unit time is called intensity. Thus,
\(
\begin{array}{r}
I=\frac{\text { Energy transferred }}{(\text { time })(\text { cross-sectional area) }}=\frac{\text { Power }}{\text { cross-sectional area }}=\frac{P}{S} \\
=\frac{\frac{1}{2} \rho \omega^2 A^2 S v}{S} \text { or } I=\frac{1}{2} \rho \omega^2 A^2 v
\end{array}
\)
Intensity of wave:
\(
\begin{aligned}
&\text { Due to point source } I \propto \frac{1}{{r}^2}\\
&y(r, t)=\frac{A}{r} \sin (\omega t-\vec{k} \cdot \vec{r}) \\
\end{aligned}
\)
\(
\begin{aligned}
&\text { Due to cylindrical source } I \propto \frac{1}{{r}}\\
&y(r, t)=\frac{{A}}{\sqrt{{r}}} \sin (\omega {t}-\vec{k} \cdot \vec{r}) \\
\end{aligned}
\)
\(
\begin{aligned}
&\text { Due to plane source } I=\text { constant }\\
&y(r, t)=A \sin (\omega t-\vec{k} \cdot \vec{r}) \\
\end{aligned}
\)
Speed of transverse wave on a string (stretched wire):
Speed of the transverse wave on a string is given by
\(
v=\sqrt{\frac{T}{\mu}}
\)
Here, \(\mu=\) mass per unit length of the string \(=\frac{m}{l}=\frac{m A}{l A} \quad(A=\text { area of cross-section of the string })\)
\(
=\left(\frac{m}{V}\right) A \quad(V=\text { volume of string })
\)
\(
=\rho A \quad(\rho=\text { density of string })
\)
Hence, the above expression can also be written as
\(
v=\sqrt{\frac{T}{\rho A}}
\)
Interference of Waves
Resultant Amplitude

The equation of the two waves reaching at a point can be written as
\(
\begin{aligned}
& y_1=A_1 \sin (k x-\omega t) \\
& y_2=A_2 \sin (k x-\omega t+\phi)
\end{aligned}
\)
The resultant displacement of the point where the waves meet is
\(
\begin{aligned}
y & =y_1+y_2 \\
& =A_1 \sin (k x-\omega t)+A_2 \sin (k x-\omega t+\phi) \\
& =A_1 \sin (k x-\omega t)+A_2 \sin (k x-\omega t) \cos \phi+A_2 \cos (k x-\omega t) \sin \phi \\
& =\left(A_1+A_2 \cos \phi\right) \sin (k x-\omega t)+A_2 \sin \phi \cos (k x-\omega t) \\
& =A \cos \theta \sin (k x-\omega t)+A \sin \theta \cos (k x-\omega t)
\end{aligned}
\)
\(
y=A \sin (k x-\omega t+\theta)
\)
Here, \(\quad A_1+A_2 \cos \phi=A \cos \theta\)
and \(A_2 \sin \phi=A \sin \theta\)
\(
\begin{aligned}
A^2 & =\left(A_1+A_2 \cos \phi\right)^2+\left(A_2 \sin \phi\right)^2 \\
A & =\sqrt{A_1^2+A_2^2+2 A_1 A_2 \cos \phi} \dots(i)\\
\tan \theta & =\frac{A \sin \theta}{A \cos \theta}=\frac{A_2 \sin \phi}{A_1+A_2 \cos \phi} \dots(ii)
\end{aligned}
\)
Resultant Intensity
We have read that intensity of a wave is given by
\(
I=\frac{1}{2} \rho \omega^2 A^2 v \quad \text { or } \quad I \propto A^2
\)
So, if \(\rho, \omega\) and \(v\) are same for the both interfering waves, then Eq. (i) can also be written as
\(
I=I_1+I_2+2 \sqrt{I_1 I_2} \cos \phi
\)
Here, proportionality constant \(\left(I \propto A^2\right)\) cancels out on right hand side and left hand side.
Note: The special case of above two equations is, when the individual amplitudes (or intensities) are equal. or
\(
A_1=A_2=A_0(\text { say }) \Rightarrow I_1=I_2=I_0(\text { say })
\)
In this case, Eqs. (i) and (ii) become
\(
A=2 A_0 \cos \frac{\phi}{2} \dots(iii)
\)
and \(I=4 I_0 \cos ^2 \frac{\phi}{2} \dots(iv)\)
Extra Points to Remember
Sound Waves
Key Points
Transmission of Waves (Reflection and Refraction)

Power
At the boundary of two media, energy incident per second \(=\) energy reflected per second + energy transmitted per second.
Power incident \(=\) power reflected + power transmitted
\(
P_i=P_r+P_t
\)
Let us summarise the above discussion in tabular form as below.
\(Beats
When two sound waves of nearly equal (but not exactly equal) frequencies travel in the same direction, at a given point due to their superposition, intensity alternatively increases and decreases periodically. This periodic waxing and waning of sound at a given position is called beats. Beat frequency \(=\) difference of frequencies of two interfering waves
Beat frequency \(=\left|f_1-f_2\right|\)
Stationary Waves or Standing Waves
When two waves of the same frequency and amplitude travel in opposite direction at the same speed, their superstition gives rise to a new type of wave, called stationary waves or standing waves. Formation of the standing wave is possible only in a bounded medium.
Suppose the two identical waves travelling in opposite directions are
\(
\begin{aligned}
& y_1=A \sin (k x-\omega t) \\
& \text { and } y_2=A \sin (k x+\omega t)
\end{aligned}
\)
By the principle of superposition, their sum is
\(
\begin{aligned}
& y=y_1+y_2 \\
& y=A[\sin (k x-\omega t)+\sin (k x+\omega t)]
\end{aligned}
\)
By using the identity,
\(
\sin A+\sin B=2 \sin \left(\frac{A+B}{2}\right) \cos \left(\frac{A-B}{2}\right) \text {, we obtain }
\)
\(
y=2 A \sin k x \cos \omega t \dots(i)
\)
Eq. (i) represents what is known as a standing wave(stationary wave).
Eq. (i) can also be written as
\(
y=A(x) \cos \omega t \dots(ii)
\)
where,
\(
A_x=2 A \sin k x \dots(iii)
\)
This equation of a standing wave [Eq. (ii)] is really an equation of simple harmonic motion, whose amplitude [Eq. (iii)] is a function of \(x\).
\(
A_x=0, \text { where } \sin k x=0
\)
\(k x=0, \pi, 2 \pi, \ldots, n \pi \quad(n=0,1,2, \ldots)\)
Substituting \(k=\frac{2 \pi}{\lambda}\), we have
\(A_x=0 \quad\) where, \(\quad x=0, \frac{\lambda}{2}, \lambda, \ldots, \frac{n \lambda}{2}\)
These are the points which never displace from their mean position. These are known as the nodes (amplitude is minimum) of the standing wave. The distance between two adjacent nodes is \(\frac{\lambda}{2}\).
Further, from Eq. (iii), we can see that maximum value of \(\left|A_x\right|\) is \(2 A\), where
\(
\sin k x= \pm 1
\)
\(
\begin{array}{lr}
k x=\frac{\pi}{2}, \frac{3 \pi}{2}, \ldots,(2 n-1) \frac{\pi}{2} & (n=0,1,2, \ldots) \\
x=\frac{\lambda}{4}, \frac{3 \lambda}{4}, \ldots,(2 n-1) \frac{\lambda}{4} & \left(k=\frac{2 \pi}{\lambda}\right)
\end{array}
\)
These are the points of maximum displacement called antinodes (amplitude is maximum). The distance between two adjacent antinodes is also \(\frac{\lambda}{2}\), while that between a node and antinode is \(\frac{\lambda}{4}\).
Comparison between travelling and stationary waves
| S No. | Travelling waves | Stationary waves |
| 1 | In these waves, all particles of the medium oscillate with same frequency and amplitude | In these waves, all particles except nodes oscillate with same frequency but different amplitudes. Amplitudes is zero at nodes and maximum at antinodes |
| 2 | At any instant phase difference between any two particles can have any value between 0 and \(2 \pi\). | At any instant phase difference between any two particles can be either zero or \(\pi\). |
| 3 | In these waves, at no instant all the particles of the medium pass through their mean positions simultaneously. | In these waves, all particles of the medium pass through their mean positions simultaneously twice in each time period. |
| 4 | These waves transmit energy in the medium. | These waves do not transmit energy in the medium provided \(A_1=A_2\). |
Transverse stationary waves in a stretched string


Sonometer
A sonometer is defined as the device that is used for demonstrating the relationship between the frequency of the sound that is produced by the string when it is plucked and the tension, length, and mass per unit length of the string.
The sound is produced in the transverse standing wave in the string.

Displacement and pressure wave
A sound wave can be described either in terms of the longitudinal displacement suffered by the particles of the medium (called displacement wave) or in terms of the excess pressure generated due to compression and rarefaction (called pressure wave).
Displacement wave
\(
y=A \sin (\omega t-k x)
\)
Pressure wave
\(
{p}={p}_0 \cos (\omega {t}-{kx})
\)
Where \(p_0=A B k=\rho A v \omega\) relates the pressure amplitude \(\left(p_0\right)\) to the displacement amplitude ( \(A\) ), bulk modulus ( \(B\) ), wave number \((k)\), density ( \(\rho\) ), wave speed ( \(v\) ), and angular frequency ( \(\omega\) ).
Note: As sound sensors (e.g., ear or mike) detect pressure changes, the description of sound as pressure wave is preferred over displacement wave.
Important Points:
Vibrations of organ pipes
Stationary longitudinal waves closed end \(\rightarrow\) displacement node, open end \(\rightarrow\) displacement antinode


End correction :
Due to the finite momentum of air molecules in organ pipes, reflection takes place not exactly at open end but some what above it, so antinode is not formed exactly at free end but slightly above it.
In closed organ pipe \(f_1=\frac{v}{4(\ell+e)}\) where \(e=0.6 \mathrm{R} \quad\) ( \(\mathrm{R}=\) radius of pipe)
In open organ pipe \(f_1=\frac{v}{2(\ell+2 e)}\)
Resonance Tube
Wavelength \(\quad \lambda=2\left(\ell_2-\ell_1\right)\)
End correction \(e=\frac{\ell_2-3 \ell_1}{2}\)
Intensity of sound in decibels
Sound level, \(\mathrm{SL}=10 \log _{10}\left(\frac{\mathrm{I}}{\mathrm{I}_0}\right)\)
Where \(\mathrm{I}_0=\) threshold of human ear \(=10^{-12} \mathrm{~W} / \mathrm{m}^2\)
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