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Waves

CBSE Class 11 Physics • Chapter 14 • Detailed Notes

Chapter Overview

This chapter covers the detailed physics of Wave Motion, including mechanical waves, equation of progressive waves, reflection, superposition, standing waves, beats, and the Doppler effect.

14.1 Introduction to Waves

Wave Motion: It is a mode of energy transfer from one point to another without the permanent transport of matter. Patterns of disturbance move through the medium.

Mechanism: Particles of the medium oscillate about their mean positions. The disturbance is handed over from one particle to the next due to Elasticity and Inertia of the medium.

Types of Waves based on Medium:

14.2 Transverse and Longitudinal Waves

Comparison based on particle vibration direction relative to wave propagation.

Animation: Transverse vs Longitudinal Waves
Property Transverse Wave Longitudinal Wave
Particle Vibrations Perpendicular ($\perp$) to wave propagation. Parallel ($\parallel$) to wave propagation.
Formation Travels in the form of Crests (Pos. Max) and Troughs (Neg. Max). Travels in the form of Compressions (High Density) and Rarefactions (Low Density).
Medium Required Requires Rigidity (Shear modulus). Solids and Surface of Liquids. Requires Elasticity of Volume (Bulk modulus). Solids, Liquids, and Gases.
Pressure Variation No pressure variation in the medium. Pressure and density vary at every point.
Polarization Can be polarized. Cannot be polarized.

14.3 Progressive Wave (Travelling Wave)

Derivation of the Equation of a Plane Progressive Harmonic Wave:

Goal: To mathematically describe a wave where every particle performs Simple Harmonic Motion (SHM).

Step 1: Motion at the Source ($x=0$)

Assume the particle at the origin ($x=0$) oscillates in SHM starting from mean position:

$$ y(0, t) = A \sin(\omega t) $$

Step 2: Propagation & Time Lag

The disturbance travels with wave velocity $v$. To reach a particle at position $x$, the wave takes time $t_{lag} = \frac{x}{v}$.

Step 3: Motion at Position $x$

The particle at $x$ does exactly what the source particle did earlier at time $(t - t_{lag})$.

$$ y(x, t) = y(0, t - t_{lag}) $$

Substituting the SHM equation:

$$ y(x, t) = A \sin[\omega (t - \frac{x}{v})] $$

$$ y(x, t) = A \sin(\omega t - \frac{\omega}{v}x) $$

Step 4: Defining Wave Constants

We define Propagation Constant (or Angular Wave Number) as $k = \frac{\omega}{v} = \frac{2\pi \nu}{\nu \lambda} = \frac{2\pi}{\lambda}$.

Substituting $k$:

$$ y(x, t) = A \sin(\omega t - kx) $$

Note: Since $\sin(-\theta) = -\sin(\theta)$, and usually we start with $kx$, we often write it as:

$$ y(x, t) = A \sin(kx - \omega t + \phi) $$

This represents a wave traveling in the Positive X direction.

Why $(kx - \omega t)$?

General Sinusoidal Wave Equation:

$$ y(x, t) = A \sin(kx - \omega t + \phi) $$

Detailed Analysis of Terms:

Relation between Phase Diff ($\Delta \phi$), Path Diff ($\Delta x$), and Time Diff ($\Delta t$):

1. Phase difference for two particles separated by distance $\Delta x$:

We know:   $\lambda \longleftrightarrow 2\pi$

This means phase per unit length is:   $\frac{2\pi}{\lambda}$

So if distance is $\Delta x$, phase difference will be:   $\Delta \phi = \frac{2\pi}{\lambda} \times \Delta x$

This gives:

$$ \Delta \phi = \frac{2\pi}{\lambda} \Delta x $$

2. Phase difference for the SAME particle after time interval $\Delta t$:

We know:   $T \longleftrightarrow 2\pi$

This means phase per unit time is:   $\frac{2\pi}{T}$

So if time interval is $\Delta t$, phase difference will be:   $\Delta \phi = \frac{2\pi}{T} \times \Delta t$

This gives:

$$ \Delta \phi = \frac{2\pi}{T} \Delta t $$

Key Definitions: Wavelength, Period & Frequency

Snapshot of wave at t=0 and t=Δt showing wavelength and speed
Practice Problem 1

Q: A wave equation is $y = 0.05 \sin(80x - 3t)$. Find velocity and wavelength. (SI units)

Solution: Compare with standard $y = A \sin(kx - \omega t)$.

14.4 Speed of a Travelling Wave

$$ v = \frac{\omega}{k} = \frac{2\pi\nu}{2\pi/\lambda} = \nu \lambda $$

Wave velocity depends ONLY on the properties of the medium (Elasticity $E$ and Inertia $\rho$).

$$ v = \sqrt{\frac{E}{\rho}} $$

Case 1: Transverse Wave on Stretched String (Pulse Method)

Goal: To derive $v = \sqrt{T/\mu}$ using the concept of Centripetal Force.

Logic: Imagine moving with the pulse at speed $v$. In this frame, the pulse appears stationary, and the string moves backward with speed $v$.

Transverse Wave Stretched String Pulse

Step 1: Dynamics of Element

Consider a small element of length $dl = R(2\theta)$ (where $\theta$ is small half-angle). Mass $dm = \mu (2R\theta)$.

The element moves on a curved path of radius $R$ with speed $v$. Required Centripetal Force:

$$ F_c = \frac{(dm)v^2}{R} = \frac{(2\mu R \theta)v^2}{R} = 2\mu v^2 \theta $$

Step 2: Restoring Force

The tension $T$ at both ends provides the downward radial force. Vertical component is $2T \sin\theta$.

For small $\theta$, $\sin\theta \approx \theta$. So, $F_{res} \approx 2T\theta$.

Step 3: Equating Forces

$$ 2T\theta = 2\mu v^2 \theta $$

$$ T = \mu v^2 \Rightarrow v = \sqrt{\frac{T}{\mu}} $$

Case 2: Longitudinal Wave (Sound) in Fluids

General Formula: $v = \sqrt{\frac{B}{\rho}}$ where $B$ is Bulk Modulus.

Definition of Bulk Modulus: $B = -V \frac{dP}{dV}$.


1. Newton's Formula (Isothermal):

Assumption: Sound travels slowly, temperature remains constant ($PV = \text{constant}$).

Differentiating: $P dV + V dP = 0 \Rightarrow P dV = -V dP \Rightarrow P = -V \frac{dP}{dV}$.

This implies $B_{iso} = P$. So, $v = \sqrt{\frac{P}{\rho}}$.

(Result: ~280 m/s for air. Incorrect.)


2. Laplace's Correction (Adiabatic):

Assumption: Compressions are rapid, heat cannot escape ($PV^\gamma = \text{constant}$).

Differentiating: $\gamma P V^{\gamma-1} dV + V^\gamma dP = 0$.

Divide by $V^{\gamma-1}$: $\gamma P dV + V dP = 0 \Rightarrow \gamma P = -V \frac{dP}{dV}$.

This implies $B_{adia} = \gamma P$. So, $v = \sqrt{\frac{\gamma P}{\rho}}$.

(Result: ~331 m/s. Correct!)

Factors Affecting Speed of Sound in Gas:

  1. Temperature: $v \propto \sqrt{T}$. Speed increases by 0.61 m/s for every $1^\circ$C rise.
  2. Molecular Weight: $v \propto \frac{1}{\sqrt{M}}$. (Hydrogen transmits sound faster than Oxygen).
  3. Humidity: Moist air is lighter ($\rho$ decreases) than dry air. Hence speed increases with humidity.
  4. Pressure: NO EFFECT (at constant temperature), because $P/\rho$ remains constant.

14.5 Principle of Superposition of Waves

Principle of Superposition: When two or more waves simultaneously pass through a point in a medium, the resultant displacement at that point is the vector sum of the displacements produced by the individual waves.

$$ \vec{y} = \vec{y}_1 + \vec{y}_2 + \dots + \vec{y}_n $$

Analytical Treatment of Interference:

Consider two harmonic waves of the same frequency and amplitude, travelling in the same direction, with a constant phase difference $\phi$:

$$ y_1 = A \sin(kx - \omega t) $$

$$ y_2 = A \sin(kx - \omega t + \phi) $$

By Principle of Superposition, the resultant displacement $y = y_1 + y_2$ is:

$$ y = A [\sin(kx - \omega t) + \sin(kx - \omega t + \phi)] $$

Using the trigonometric identity $\sin C + \sin D = 2 \sin\left(\frac{C+D}{2}\right) \cos\left(\frac{C-D}{2}\right)$:

$$ y = \left[2A \cos\left(\frac{\phi}{2}\right)\right] \sin\left(kx - \omega t + \frac{\phi}{2}\right) $$

The resultant wave is also a harmonic wave with:

Types of Interference:

1. Constructive Interference:

When waves meet in the same phase, their amplitudes add up to give maximum intensity.


2. Destructive Interference:

When waves meet in opposite phases, their amplitudes cancel out to give minimum intensity.

Transverse Wave Superposition

Superposition Scenario 1

Superposition Scenario 2

Superposition Scenario 3

14.6 Reflection & Standing Waves

Boundary Conditions:

Reflection at Fixed End (Phase Inversion)

Reflection at Free End (No Phase Change)

Analytical Treatment of Standing Waves

Goal: To show that superposition of two identical counter-propagating waves creates a stationary wave pattern.

1. Wave Equations:

Incident Wave ($+x$): $y_1 = A \sin(kx - \omega t)$

Reflected Wave ($-x$): $y_2 = A \sin(kx + \omega t)$ (Assuming reflection from free end/ open pipe for in-phase reflection).

2. Superposition Principle:

$$ y = y_1 + y_2 = A [\sin(kx - \omega t) + \sin(kx + \omega t)] $$

Using Identity: $\sin(C) + \sin(D) = 2 \sin(\frac{C+D}{2}) \cos(\frac{C-D}{2})$

$$ y(x, t) = [2A \sin(kx)] \cos(\omega t) $$

3. Interpretation:

4. Nodes and Antinodes:

Nodes (Zero Displacement):

$\sin(kx) = 0 \Rightarrow kx = n\pi$

$\frac{2\pi}{\lambda} x = n\pi \Rightarrow x = \frac{n\lambda}{2}$

Positions: $x = 0, \frac{\lambda}{2}, \lambda, \frac{3\lambda}{2} \dots$

Antinodes (Max Displacement $\pm 2A$):

$\sin(kx) = \pm 1 \Rightarrow kx = (2n+1)\frac{\pi}{2}$

Positions: $x = \frac{\lambda}{4}, \frac{3\lambda}{4}, \frac{5\lambda}{4} \dots$

Normal Modes of a Stretched String (Both Ends Fixed)

A string of length $L$ fixed at both ends can only vibrate in modes where the string length is an integer multiple of half-wavelengths: $L = \frac{n\lambda}{2}$.

So, $\lambda_n = \frac{2L}{n}$ and wave speed $v = \sqrt{T/\mu}$. The allowed frequencies are:

$$ \nu_n = \frac{nv}{2L} = n \cdot \nu_1 \quad (n = 1, 2, 3, \ldots) $$

Fundamental / 1st Harmonic

2nd Harmonic

3rd Harmonic

Mode (n) Name Nodes Antinodes Wavelength Frequency
1 Fundamental / 1st Harmonic 2 1 $\lambda_1 = 2L$ $\nu_1 = \frac{v}{2L}$
2 2nd Harmonic / 1st Overtone 3 2 $\lambda_2 = L$ $\nu_2 = \frac{v}{L} = 2\nu_1$
3 3rd Harmonic / 2nd Overtone 4 3 $\lambda_3 = \frac{2L}{3}$ $\nu_3 = \frac{3v}{2L} = 3\nu_1$
$n$ $n$-th Harmonic $n+1$ $n$ $\lambda_n = \frac{2L}{n}$ $\nu_n = n\nu_1$

Key Point: A stretched string (both ends fixed) supports ALL harmonics (both odd and even multiples of $\nu_1$). This is why stringed instruments like the sitar or violin produce a rich musical tone.

Modes of Vibration (Animated)

Fundamental Mode (n=1) Second Harmonic (n=2)
Closed Pipe (Node at Closed End) Open Pipe (Antinodes at Ends) N A Fund. Freq $\nu = v/4L$ A N A Fund. Freq $\nu = v/2L$ Animation: Fundamental Modes of Vibration in Closed and Open Pipes.

Normal Modes of Organ Pipes

A. Closed Organ Pipe (One End Closed)

Closed end → always a Node (N). Open end → always an Antinode (A).

Condition: $L = (2n-1)\frac{\lambda}{4}$, giving allowed frequencies:

$$ \nu_n = (2n-1)\frac{v}{4L} = (2n-1)\nu_1 \quad (n = 1, 2, 3, \ldots) $$

Fundamental

3rd Harmonic

5th Harmonic

Mode (n) Name Frequency Harmonic Number
1 Fundamental $\nu_1 = \frac{v}{4L}$ 1st harmonic
2 1st Overtone $\nu_2 = \frac{3v}{4L} = 3\nu_1$ 3rd harmonic
3 2nd Overtone $\nu_3 = \frac{5v}{4L} = 5\nu_1$ 5th harmonic
$n$ $(n-1)$th Overtone $\nu_n = (2n-1)\frac{v}{4L}$ $(2n-1)$th harmonic

Key Point: A closed pipe supports only ODD harmonics ($\nu_1, 3\nu_1, 5\nu_1\ldots$). This gives a hollow, nasal sound.

B. Open Organ Pipe (Both Ends Open)

Both open ends → always Antinodes (A) at both ends.

Condition: $L = \frac{n\lambda}{2}$, giving allowed frequencies:

$$ \nu_n = \frac{nv}{2L} = n\nu_1 \quad (n = 1, 2, 3, \ldots) $$

Fundamental

2nd Harmonic

3rd Harmonic

Mode (n) Name Frequency Harmonic Number
1 Fundamental $\nu_1 = \frac{v}{2L}$ 1st harmonic
2 1st Overtone $\nu_2 = \frac{v}{L} = 2\nu_1$ 2nd harmonic
3 2nd Overtone $\nu_3 = \frac{3v}{2L} = 3\nu_1$ 3rd harmonic
$n$ $(n-1)$th Overtone $\nu_n = \frac{nv}{2L}$ $n$th harmonic

Key Point: An open pipe supports ALL harmonics. Its fundamental frequency is twice that of a closed pipe of the same length ($\nu_{open} = 2\nu_{closed}$).

Resonance

Resonance is the phenomenon in which a body vibrates with maximum amplitude when the frequency of an applied periodic force equals the body's own natural frequency.

📷 AI Image Generation Prompt (Resonance Column Experiment): A highly detailed, realistic 3D educational diagram of a resonance column apparatus. It shows a tall cylindrical glass tube filled with water, with a flexible rubber pipe connecting the bottom of the tube to a water reservoir. A vibrating silver tuning fork is held just above the open top end of the glass tube. Inside the tube, sound waves are illustrated bouncing down to the water surface and reflecting back. A ruler scale is firmly attached to the glass tube to measure the air column length $L$. Annotations point to the "Tuning Fork", "Air Column (Node at water, Antinode at open end)", and "Water Level". Clear, professional lighting with a pale neutral background.

End Correction ($e$):

The antinode in an open pipe is not formed exactly at the open end but slightly outside it.

Formula: $e = 0.6r$ (where $r$ is radius of pipe).

Corrected effective lengths:

14.7 Beats

Goal: Deriving the Beat Frequency ($\nu_b = \nu_1 - \nu_2$) from superposition.

Consider two sound waves at $x=0$ with slightly different frequencies $\omega_1$ and $\omega_2$:

$$ y_1 = A \cos(\omega_1 t) \quad , \quad y_2 = A \cos(\omega_2 t) $$

Superposition: $y = y_1 + y_2 = A [\cos(\omega_1 t) + \cos(\omega_2 t)]$

Using $\cos C + \cos D = 2 \cos(\frac{C-D}{2}) \cos(\frac{C+D}{2})$:

Let $\omega_{avg} = \frac{\omega_1 + \omega_2}{2}$ and $\Delta \omega = \frac{\omega_1 - \omega_2}{2}$.

$$ y(t) = [2A \cos(\Delta \omega \cdot t)] \cos(\omega_{avg} \cdot t) $$

Interpretation: This is a wave with frequency $\nu_{avg}$ but its amplitude varies with time.

Amplitude Modulation: $A(t) = 2A \cos(2\pi \frac{\nu_1-\nu_2}{2} t)$.

Maxima (Waxing): Amplitude is max when $\cos(\dots) = \pm 1$.

Arguments: $0, \pi, 2\pi \dots$

Time interval between two maxima: $\Delta t = \frac{1}{|\nu_1 - \nu_2|}$.

Therefore, Frequency of Beats:

$$ \nu_{beat} = |\nu_1 - \nu_2| $$
Formation of Beats (Interference) Traveling Wave Envelope (Beats). Max amplitude = Loud Sound. Animation: Beats formation showing periodic waxing and waning of amplitude.

14.8 Doppler Effect

The apparent change in frequency of wave due to the relative motion between Source (S), Observer (O), and Medium.

Derivation using Wave Crest Counting Logic:

Let Source ($S$) emit frequency $\nu_0$ and move with velocity $v_s$. Observer ($O$) moves with $v_o$. Speed of sound is $v$.

1. Effect of Source Motion (Change in Wavelength):

In time $t=1$ sec, Source emits $\nu_0$ waves. These waves occupy distance $(v - v_s)$ if Source moves towards observer.

New Wavelength $\lambda' = \frac{\text{Distance}}{\text{Number}} = \frac{v - v_s}{\nu_0}$.

2. Effect of Observer Motion (Change in Relative Velocity):

Observer moves towards incoming waves. Relative velocity of wave w.r.t Observer is $v_{rel} = v + v_o$.

3. Apparent Frequency:

$$ \nu' = \frac{\text{Relative Speed}}{\text{Effective Wavelength}} = \frac{v + v_o}{\lambda'} $$

Substituting $\lambda'$:

$$ \nu' = (v + v_o) \cdot \frac{\nu_0}{v - v_s} $$

$$ \nu' = \nu_0 \left( \frac{v \pm v_o}{v \mp v_s} \right) $$

Sign Convention (Top Signs): Use Top signs ($+v_o, -v_s$) when approaching each other. Use Bottom signs when receding.

Special Cases of Doppler Effect

Situation Condition Formula Effect on $\nu'$
Source moves towards stationary observer $v_o = 0$, $v_s > 0$ (towards O) $\nu' = \nu_0 \left(\frac{v}{v - v_s}\right)$ Increases (Higher pitch)
Source moves away from stationary observer $v_o = 0$, $v_s > 0$ (away from O) $\nu' = \nu_0 \left(\frac{v}{v + v_s}\right)$ Decreases (Lower pitch)
Observer moves towards stationary source $v_s = 0$, $v_o > 0$ (towards S) $\nu' = \nu_0 \left(\frac{v + v_o}{v}\right)$ Increases (Higher pitch)
Observer moves away from stationary source $v_s = 0$, $v_o > 0$ (away from S) $\nu' = \nu_0 \left(\frac{v - v_o}{v}\right)$ Decreases (Lower pitch)
Both S and O at rest $v_s = 0$, $v_o = 0$ $\nu' = \nu_0$ No change

Important note: The Doppler formula applies only when the speeds of source and observer are less than the speed of sound. When a source moves at the speed of sound ($v_s = v$), a shock wave (sonic boom) is produced. The ratio $v_s/v$ is called the Mach Number.

A common daily-life example: The whistle of an approaching train sounds shriller (higher pitch) and that of a receding train sounds graver (lower pitch) — Doppler Effect!

Observer Animation: Source moving Right, bunching waves in front.

📋 Quick Formula Reference

Quantity Formula Symbols
Progressive Wave $y(x,t) = A\sin(kx - \omega t + \phi)$ $A$=amplitude, $k$=wave number, $\omega$=ang. freq., $\phi$=phase const.
Wave Number $k = \frac{2\pi}{\lambda}$ $\lambda$=wavelength
Angular Frequency $\omega = \frac{2\pi}{T} = 2\pi\nu$ $T$=period, $\nu$=frequency
Wave Speed $v = \nu\lambda = \frac{\omega}{k}$
Speed on String $v = \sqrt{\frac{T}{\mu}}$ $T$=Tension, $\mu$=linear mass density
Speed of Sound (Laplace) $v = \sqrt{\frac{\gamma P}{\rho}}$ $\gamma$=$C_p/C_v$, $P$=pressure, $\rho$=density
Standing Wave $y(x,t) = [2A\sin(kx)]\cos(\omega t)$ Nodes at $x=n\lambda/2$, Antinodes at $x=(2n+1)\lambda/4$
String Harmonics (both ends fixed) $\nu_n = \frac{nv}{2L}$ $n=1,2,3\ldots$ (all harmonics)
Closed Pipe Harmonics $\nu_n = \frac{(2n-1)v}{4L}$ $n=1,2,3\ldots$ (odd harmonics only)
Open Pipe Harmonics $\nu_n = \frac{nv}{2L}$ $n=1,2,3\ldots$ (all harmonics)
Beat Frequency $\nu_{beat} = |\nu_1 - \nu_2|$ Valid when $|\nu_1-\nu_2|$ is small
Doppler Effect $\nu' = \nu_0\left(\frac{v \pm v_o}{v \mp v_s}\right)$ +/− for approaching; −/+ for receding