Physics by Lamhi: Not Your Boring Physics

CLASS 12 · CHAPTER 10 · OPTICS

DETAILED NOTES

Wave Optics

The complete chapter, section by section: Huygens' principle and how its secondary wavelets derive the law of reflection and Snell's law of refraction, coherent sources and sustained interference, the resultant intensity of two interfering waves, the full derivation of Young's double-slit fringe width, single-slit diffraction, and polarization, from Malus's law to Brewster's law, explained in plain language with original worked examples.

10.1 Huygens’ Principle

Huygens’ principle treats every point on a wavefront as a source of its own tiny secondary wavelet, spreading outward at the wave’s own speed. The new wavefront, a little later, is just the common tangent surface (the “envelope”) touching all of these secondary wavelets. This simple construction explains reflection and refraction purely from the geometry of wavefronts, without needing to track individual rays (§10.2 carries out both derivations step by step), and it’s the starting point for understanding interference and diffraction: both arise from adding up these secondary wavelets with their correct phases.

10.2 Reflection & Refraction by Huygens’ Construction

Section 10.1 claimed that secondary wavelets alone can explain reflection and refraction. This section makes good on that claim: both laws fall out of nothing more than a pair of right-angled triangles. One fact about angles is needed first. A ray is always perpendicular to its wavefront, and the normal is always perpendicular to the surface, so the angle between the wavefront and the surface is exactly the same as the angle between the ray and the normal: it is the same pair of directions, each simply turned through 90°. That lets us read the angles of incidence, refraction and reflection straight off the wavefronts, without drawing a single ray.

10.2.1 Refraction, and Snell’s law

A flat surface separates medium 1, where light travels at speed v1v_1, from medium 2, where it travels at v2v_2. A plane wavefront AB arrives at an angle of incidence ii, tilted so that its lower end, point A, has just touched the surface, while its upper end, point B, still has a distance BC to travel (along the ray) before it reaches the surface at point C. Call the time B takes to cover that distance τ\tau:

BC=v1τBC = v_1\tau

Point A has not been idle in the meantime. The instant the wavefront touched it, A became the source of a secondary wavelet spreading into medium 2 at that medium’s own speed, v2v_2. So by the time B reaches C, A’s wavelet is a hemisphere (below the surface) of radius:

AE=v2τAE = v_2\tau

Every point of the surface between A and C launches its own wavelet too, as the wavefront sweeps across it; the closer a point is to C, the later it starts, and the smaller its wavelet has grown. The refracted wavefront is the envelope touching all of them: the plane CE drawn from C just tangent to A’s wavelet, touching it at point E. Now compare two right-angled triangles that share the same hypotenuse AC, the strip of surface between A and C.

Triangle ABC has its right angle at B (BC runs along the incident ray, which is perpendicular to the wavefront AB), and its angle at A is the angle between the incident wavefront and the surface, which by the fact above is ii. Triangle AEC has its right angle at E (a tangent always meets the radius AE at 90°), and its angle at C is the angle between the refracted wavefront CE and the surface, which is the angle of refraction rr. Reading off the side opposite each of those angles:

sin⁡i=BCAC=v1τAC,sin⁡r=AEAC=v2τAC\sin i = \dfrac{BC}{AC} = \dfrac{v_1\tau}{AC}, \qquad \sin r = \dfrac{AE}{AC} = \dfrac{v_2\tau}{AC}

Divide the first by the second, and both τ\tau and ACAC cancel:

Ratio of sines from the construction
sin⁡isin⁡r=v1v2\dfrac{\sin i}{\sin r} = \dfrac{v_1}{v_2}

The refractive index of a medium is defined as n=c/vn = c/v, so v1=c/n1v_1 = c/n_1 and v2=c/n2v_2 = c/n_2:

sin⁡isin⁡r=c/n1c/n2=n2n1\dfrac{\sin i}{\sin r} = \dfrac{c/n_1}{c/n_2} = \dfrac{n_2}{n_1}
Snell's law of refraction
n1sin⁡i=n2sin⁡r\textcolor{#e08a1e}{n_1\sin i = n_2\sin r}

Notice what the wave picture predicts along the way. If the ray bends toward the normal (r<ir<i), then sin⁡i/sin⁡r\sin i/\sin r is bigger than 1, so v2v_2 must be smaller than v1v_1: light has to travel more slowly in the denser medium. The older particle (corpuscular) model of light predicted exactly the opposite, and Foucault’s 1850 measurement of the speed of light in water settled the question in favour of waves.

One more result comes for free. The frequency ν\nu of the light is fixed by the source: every point of the boundary is shaken by the incident wave and simply follows along at its frequency, so ν\nu is the same on both sides. Since v=νλv = \nu\lambda holds in each medium:

λ1λ2=v1/νv2/ν=v1v2\dfrac{\lambda_1}{\lambda_2} = \dfrac{v_1/\nu}{v_2/\nu} = \dfrac{v_1}{v_2}
Wavelength in each medium
λ1λ2=v1v2=n2n1\dfrac{\lambda_1}{\lambda_2} = \dfrac{v_1}{v_2} = \dfrac{n_2}{n_1}

So light entering a denser medium slows down, and its wavelength shrinks by exactly the same factor, while its frequency stays put.

10.2.2 Reflection

Reflection is the same construction with one change: the wavelet from A now spreads back into medium 1, the medium the light came from (above the surface, on the same side as the incoming light), so it travels at the same speed vv as the incident wave itself. By the time B covers BC=vτBC = v\tau to reach the surface at C, A’s wavelet has grown to radius AE=vτAE = v\tau, exactly equal to BC. The reflected wavefront is again the tangent CE drawn from C to this wavelet.

The same two triangles appear: ABC, right-angled at B, with its angle at A equal to the angle of incidence ii; and AEC, right-angled at E, with its angle at C equal to the angle of reflection rr. Reading off the opposite sides once more:

sin⁡i=BCAC=vτAC,sin⁡r=AEAC=vτAC\sin i = \dfrac{BC}{AC} = \dfrac{v\tau}{AC}, \qquad \sin r = \dfrac{AE}{AC} = \dfrac{v\tau}{AC}

The right-hand sides are identical, so sin⁡i=sin⁡r\sin i = \sin r, and since both angles lie between 0° and 90°, the angles themselves must be equal:

Law of reflection
i=r\textcolor{#e08a1e}{i = r}

In the language of geometry, the two triangles share the hypotenuse AC and have one other side equal (BC = AE), so they are congruent by RHS, and their matching angles ii and rr are equal. Refraction differs from reflection only because, there, the wavelet from A grows at a different speed from the incident wave, which is what breaks the symmetry between the two triangles and bends the ray.

Worked example

Building a refracted wavefront, step by step

A plane wavefront in air (speed v1=3.00×108 m/sv_1 = 3.00\times10^8\text{ m/s}) strikes a flat glass surface (n=1.50n = 1.50) at an angle of incidence of 50.0°. At the instant end A touches the glass, end B is still BC = 3.00 cm from the surface. Use Huygens’ construction to find the angle of refraction, then check it against Snell’s law.

Time for B to reach the surface, and the speed of light in the glass:

τ=BCv1=0.03003.00×108=1.00×10−10 s,v2=cn=3.00×1081.50=2.00×108 m/s\tau = \dfrac{BC}{v_1} = \dfrac{0.0300}{3.00\times10^8} = 1.00\times10^{-10}\text{ s}, \qquad v_2 = \dfrac{c}{n} = \dfrac{3.00\times10^8}{1.50} = 2.00\times10^8\text{ m/s}

Radius of A’s wavelet after that time, and the length of the surface strip AC:

AE=v2τ=(2.00×108)(1.00×10−10)=2.00 cm,AC=BCsin⁡i=3.000.7660=3.916 cmAE = v_2\tau = (2.00\times10^8)(1.00\times10^{-10}) = 2.00\text{ cm}, \qquad AC = \dfrac{BC}{\sin i} = \dfrac{3.00}{0.7660} = 3.916\text{ cm}

The angle of refraction, from triangle AEC:

sin⁡r=AEAC=2.003.916=0.5107  ⇒  r=30.7∘\sin r = \dfrac{AE}{AC} = \dfrac{2.00}{3.916} = 0.5107 \;\Rightarrow\; r = \textcolor{#e08a1e}{30.7^\circ}

Snell’s law, applied directly, agrees:

sin⁡r=sin⁡50.0∘1.50=0.76601.50=0.5107  ⇒  r=30.7∘ ✓\sin r = \dfrac{\sin 50.0^\circ}{1.50} = \dfrac{0.7660}{1.50} = 0.5107 \;\Rightarrow\; r = 30.7^\circ \ \checkmark

The wavelet from A only manages 2.00 cm while B covers 3.00 cm, and that shortfall is what tips the refracted wavefront over, swinging the ray from 50.0° down to 30.7°, toward the normal.

10.3 Coherent Sources & Sustained Interference

Two sources are coherent if they maintain a constant phase difference between them over time. Only coherent sources produce a sustained (unmoving, observable) interference pattern; if the phase relationship drifts randomly, the bright and dark positions shift too fast to see, and the pattern washes out to a uniform average.

This is why two independent light bulbs never show visible fringes: each emits light in random, independent bursts, so there is no fixed phase relationship between them at all. Young’s experiment sidesteps this by splitting a single wavefront into two (via the two slits), so both halves start out perfectly in phase and stay that way.

10.4 Resultant Intensity of Two Interfering Waves

Section 10.3 said when two waves can interfere steadily; this section works out exactly how bright the result is at any point. Suppose two coherent waves of the same frequency arrive at a point P with amplitudes a1a_1 and a2a_2, the second running ahead of the first by a constant phase difference ϕ\phi:

y1=a1cos⁡ωt,y2=a2cos⁡(ωt+ϕ)y_1 = a_1\cos\omega t, \qquad y_2 = a_2\cos(\omega t+\phi)

10.4.1 Adding the two waves

By the superposition principle, the actual displacement at P is simply the sum y=y1+y2y = y_1 + y_2. Expand the second cosine using cos⁡(A+B)=cos⁡Acos⁡B−sin⁡Asin⁡B\cos(A+B) = \cos A\cos B - \sin A\sin B, then group the cos⁡ωt\cos\omega t terms and the sin⁡ωt\sin\omega t terms together:

y=a1cos⁡ωt+a2(cos⁡ωtcos⁡ϕ−sin⁡ωtsin⁡ϕ)=(a1+a2cos⁡ϕ)cos⁡ωt−(a2sin⁡ϕ)sin⁡ωty = a_1\cos\omega t + a_2\left(\cos\omega t\cos\phi - \sin\omega t\sin\phi\right) = (a_1+a_2\cos\phi)\cos\omega t - (a_2\sin\phi)\sin\omega t

The two brackets are just constants; they don’t change with time. Give them names, using a new amplitude AA and a new phase δ\delta:

Acos⁡δ=a1+a2cos⁡ϕ,Asin⁡δ=a2sin⁡ϕA\cos\delta = a_1 + a_2\cos\phi, \qquad A\sin\delta = a_2\sin\phi

so that, running the same cosine identity backwards:

y=A(cos⁡δcos⁡ωt−sin⁡δsin⁡ωt)=Acos⁡(ωt+δ)y = A\left(\cos\delta\cos\omega t - \sin\delta\sin\omega t\right) = A\cos(\omega t+\delta)

The combined disturbance is still a plain oscillation at the same frequency, just with a new amplitude AA. To find it, square the two defining equations and add them; δ\delta disappears from the left because cos⁡2δ+sin⁡2δ=1\cos^2\delta + \sin^2\delta = 1, and the same identity tidies up the right:

A2=(a1+a2cos⁡ϕ)2+(a2sin⁡ϕ)2=a12+2a1a2cos⁡ϕ+a22(cos⁡2ϕ+sin⁡2ϕ)A^2 = (a_1+a_2\cos\phi)^2 + (a_2\sin\phi)^2 = a_1^2 + 2a_1a_2\cos\phi + a_2^2\left(\cos^2\phi+\sin^2\phi\right)
Resultant amplitude
A2=a12+a22+2a1a2cos⁡ϕA^2 = a_1^2 + a_2^2 + 2a_1a_2\cos\phi

Intensity is proportional to the square of the amplitude, I=kA2I = kA^2, with the same constant kk for every wave here. Each wave on its own therefore gives I1=ka12I_1 = ka_1^2 and I2=ka22I_2 = ka_2^2, and the cross term can be written as k a1a2=(ka12)(ka22)=I1I2k\,a_1a_2 = \sqrt{(ka_1^2)(ka_2^2)} = \sqrt{I_1I_2}. Multiplying the amplitude equation through by kk:

kA2=ka12+ka22+2(ka12)(ka22)cos⁡ϕkA^2 = ka_1^2 + ka_2^2 + 2\sqrt{(ka_1^2)(ka_2^2)}\cos\phi
Resultant intensity of two interfering waves
I=I1+I2+2I1I2cos⁡ϕ\textcolor{#e08a1e}{I} = I_1 + I_2 + 2\sqrt{I_1I_2}\cos\phi

The first two terms are what you would get by just adding the two intensities. The third, 2I1I2cos⁡ϕ2\sqrt{I_1I_2}\cos\phi, is the interference term: positive where the waves arrive roughly in step, negative where they arrive roughly opposed, and the entire reason fringes exist. If the phase difference drifts randomly, as it does for the incoherent sources of §10.3, cos⁡ϕ\cos\phi averages out to zero and only I=I1+I2I = I_1 + I_2 survives: uniform brightness, no fringes, which is exactly the washed-out pattern described there.

10.4.2 Maximum and minimum intensity

cos⁡ϕ\cos\phi can be no larger than +1, which happens when ϕ=0,±2π,±4π,…\phi = 0, \pm2\pi, \pm4\pi, \ldots (the waves arrive exactly in step). The interference term is then as large as it can be, and the three terms form a perfect square:

Constructive interference (φ = 0, ±2π, …)
Imax⁡=I1+I2+2I1I2=(I1+I2)2\textcolor{#e08a1e}{I_{\max}} = I_1 + I_2 + 2\sqrt{I_1I_2} = \left(\sqrt{I_1}+\sqrt{I_2}\right)^2

cos⁡ϕ\cos\phi can be no smaller than −1, which happens when ϕ=±π,±3π,…\phi = \pm\pi, \pm3\pi, \ldots (crest arriving on trough). The interference term is now as negative as it can be:

Destructive interference (φ = ±π, ±3π, …)
Imin⁡=I1+I2−2I1I2=(I1−I2)2\textcolor{#e08a1e}{I_{\min}} = I_1 + I_2 - 2\sqrt{I_1I_2} = \left(\sqrt{I_1}-\sqrt{I_2}\right)^2

To connect these phase conditions to path differences: a path difference of one whole wavelength puts the second wave exactly one full cycle, a phase of 2π2\pi, behind the first. A path difference Δ\Delta is the fraction Δ/λ\Delta/\lambda of a wavelength, so it produces the same fraction of 2π2\pi:

Phase difference from path difference
ϕ=2πλ Δ\phi = \dfrac{2\pi}{\lambda}\,\Delta

So ϕ=2nπ\phi = 2n\pi is the same statement as Δ=nλ\Delta = n\lambda, and ϕ=(2n+1)π\phi = (2n+1)\pi is the same as Δ=(n+12)λ\Delta = \left(n+\tfrac12\right)\lambda: precisely the bright and dark fringe conditions used for Young’s experiment in §10.5. Notice too that unless I1=I2I_1 = I_2, the minimum is not zero: two unequal waves can never cancel completely, so their dark fringes are only dim, never truly black.

10.4.3 Equal intensities: the 4I₀cos²(φ/2) pattern

In the most common case, two identical slits, both waves have the same intensity, I1=I2=I0I_1 = I_2 = I_0, and the general result tidies up considerably:

I=I0+I0+2I0⋅I0 cos⁡ϕ=2I0(1+cos⁡ϕ)I = I_0 + I_0 + 2\sqrt{I_0\cdot I_0}\,\cos\phi = 2I_0\left(1+\cos\phi\right)

Using the half-angle identity 1+cos⁡ϕ=2cos⁡2(ϕ/2)1+\cos\phi = 2\cos^2(\phi/2):

Two equal-intensity waves
I=4I0cos⁡2 ⁣(ϕ2)\textcolor{#e08a1e}{I} = 4I_0\cos^2\!\left(\dfrac{\phi}{2}\right)

Now Imax⁡=4I0I_{\max} = 4I_0 (at ϕ=0\phi = 0) and Imin⁡=0I_{\min} = 0 (at ϕ=π\phi = \pi), which the general formulas above confirm: (I0+I0)2=4I0(\sqrt{I_0}+\sqrt{I_0})^2 = 4I_0 and (I0−I0)2=0(\sqrt{I_0}-\sqrt{I_0})^2 = 0. The bright fringes are four times as bright as either wave alone (not twice, because it is the amplitudes that add, and the sum then gets squared), and the dark fringes are genuinely black. No energy has been created at the bright fringes, only moved there from the dark ones: cos⁡2\cos^2 averages to 12\tfrac12 across a fringe, so the average intensity is 4I0×12=2I04I_0\times\tfrac12 = 2I_0, exactly the total the two waves bring with them.

Worked example

Fringes from two unequal beams

Two coherent beams of the same wavelength, with intensities I1=9.00 W/m2I_1 = 9.00\text{ W/m}^2 and I2=4.00 W/m2I_2 = 4.00\text{ W/m}^2, overlap on a screen. Find (a) the maximum and minimum intensities in the pattern, and (b) the intensity at a point where the path difference between the beams is λ/8\lambda/8.

(a) With I1=3.00\sqrt{I_1} = 3.00 and I2=2.00\sqrt{I_2} = 2.00 (in units of W/m2\sqrt{\text{W/m}^2}):

Imax⁡=(3.00+2.00)2=25.0 W/m2,Imin⁡=(3.00−2.00)2=1.00 W/m2I_{\max} = (3.00+2.00)^2 = \textcolor{#e08a1e}{25.0\text{ W/m}^2}, \qquad I_{\min} = (3.00-2.00)^2 = \textcolor{#e08a1e}{1.00\text{ W/m}^2}

(b) Convert the path difference to a phase difference first:

ϕ=2πλ⋅λ8=π4\phi = \dfrac{2\pi}{\lambda}\cdot\dfrac{\lambda}{8} = \dfrac{\pi}{4}I=9.00+4.00+2(9.00)(4.00)cos⁡π4=13.0+12.0(0.7071)=21.5 W/m2I = 9.00 + 4.00 + 2\sqrt{(9.00)(4.00)}\cos\dfrac{\pi}{4} = 13.0 + 12.0(0.7071) = \textcolor{#e08a1e}{21.5\text{ W/m}^2}

The brightest fringe (25.0 W/m²) is well above the 13.0 W/m² that simply adding the two intensities would give, and 25 times brighter than the darkest fringe, even though the darkest fringe never quite reaches zero because the beams are unequal.

10.5 Young’s Double-Slit Experiment

Two narrow slits S1S_1 and S2S_2, separated by a distance dd, are illuminated by the same coherent wavefront. A screen is placed a distance DD away, with D≫dD \gg d. Consider a point P on the screen, a height yy above the central point (the point directly opposite the midpoint of the two slits).

The path difference between the two waves arriving at P is:

Path difference
Δ=S2P−S1P=dsin⁡θ\Delta = S_2P - S_1P = d\sin\theta

where θ\theta is the angle P makes with the central axis. Since D≫d,yD \gg d, y in any real setup, the angle is small, and sin⁡θ≈tan⁡θ=y/D\sin\theta \approx \tan\theta = y/D, giving:

Path difference (small-angle form)
Δ≈dyD\Delta \approx \dfrac{dy}{D}

Bright fringes (constructive interference) form wherever the path difference is a whole number of wavelengths:

Bright fringe condition
Δ=nλ(n=0,±1,±2,…)\Delta = n\lambda \quad (n=0,\pm1,\pm2,\ldots)

Dark fringes (destructive interference) form at odd multiples of a half-wavelength:

Dark fringe condition
Δ=(n+12)λ\Delta = \left(n+\tfrac12\right)\lambda

Substituting the small-angle path difference into the bright fringe condition and solving for yy gives the position of the nn-th bright fringe:

Bright fringe position
yn=nλDdy_n = \dfrac{n\lambda D}{d}

The spacing between any two consecutive bright fringes, yn+1−yny_{n+1}-y_n, is the same everywhere, this constant spacing is the fringe width:

Fringe width
β=λDd\beta = \dfrac{\lambda D}{d}

Note the direction of this dependence carefully: β\beta is inversely proportional to dd. Bringing the slits closer together (smaller dd) makes the fringes wider and easier to see; spreading the slits further apart (larger dd) packs the fringes tighter, eventually too tight to resolve at all. See the interactive double-slit simulation for the live version of this.

Worked example

Fringe width from the standard formula

Slits separated by 0.3 mm are illuminated by light of wavelength 600 nm, with a screen 2 m away. Find the fringe width.

β=λDd=(600×10−9)(2)0.3×10−3=1.2×10−63×10−4=4×10−3 m=4 mm\beta = \dfrac{\lambda D}{d} = \dfrac{(600\times10^{-9})(2)}{0.3\times10^{-3}} = \dfrac{1.2\times10^{-6}}{3\times10^{-4}} = \textcolor{#e08a1e}{4\times10^{-3}\text{ m} = 4\text{ mm}}

Worked example

Finding the slit separation from the fringe width

In a double-slit setup with D = 1 m and λ = 500 nm, bright fringes are observed to be 1 mm apart. Find the slit separation d.

Rearranging β = λD/d for d:

d=λDβ=(500×10−9)(1)1×10−3=5×10−4 m=0.5 mmd = \dfrac{\lambda D}{\beta} = \dfrac{(500\times10^{-9})(1)}{1\times10^{-3}} = \textcolor{#e08a1e}{5\times10^{-4}\text{ m} = 0.5\text{ mm}}

Worked example

Same slits, two wavelengths

The same double slit (d = 0.4 mm, D = 1.2 m) is illuminated first with red light (λ = 640 nm), then with violet light (λ = 400 nm). Find the fringe width in each case, and state which is wider.

βred=(640×10−9)(1.2)0.4×10−3=1.92×10−3 m=1.92 mm\beta_{red} = \dfrac{(640\times10^{-9})(1.2)}{0.4\times10^{-3}} = \textcolor{#e08a1e}{1.92\times10^{-3}\text{ m} = 1.92\text{ mm}}βviolet=(400×10−9)(1.2)0.4×10−3=1.2×10−3 m=1.2 mm\beta_{violet} = \dfrac{(400\times10^{-9})(1.2)}{0.4\times10^{-3}} = \textcolor{#e08a1e}{1.2\times10^{-3}\text{ m} = 1.2\text{ mm}}

Red fringes (1.92 mm) are wider than violet fringes (1.2 mm), since β ∝ λ and red light has the longer wavelength.

10.6 Diffraction at a Single Slit

A single slit of width aa also produces a pattern on a distant screen, but of a different character: a broad central maximum flanked by much weaker secondary maxima. Treating the slit as a continuum of Huygens wavelets, the first minimum (the edge of the bright central band) occurs at:

First diffraction minimum
asin⁡θ=λa\sin\theta = \lambda

Subsequent minima occur at asin⁡θ=nλa\sin\theta = n\lambda for n=1,2,3,…n=1,2,3,\ldots. A key qualitative feature worth remembering: the central maximum is twice as wide (in angular terms) as each of the secondary maxima on either side, since it’s bounded by the first minima on both sides at ±λ/a\pm\lambda/a, while each secondary maximum sits between consecutive minima just one such interval apart.

10.7 Polarization & Brewster's Law

Light is a transverse wave; ordinary (unpolarized) light has its electric field vibrating in all directions perpendicular to the direction of travel. A polarizer passes only the component of the field along one particular axis. When polarized light of intensity I0I_0 passes through a second polarizer (an “analyser”) whose axis is at an angle θ\theta to the first, the transmitted intensity follows Malus’s law:

Malus's law
I=I0cos⁡2θI = I_0\cos^2\theta

At θ=0\theta = 0, all the light passes (I=I0I=I_0); at θ=90°\theta = 90°, none does (I=0I=0), the two polarizers are “crossed.”

10.7.1 Brewster's law: polarization by reflection

(The current NCERT text stops at Malus’s law; this result is added here because it is a standard, frequently tested extension of the same polarization ideas.) Ordinary reflection also polarizes light, partially at most angles, but completely at one special angle of incidence, the Brewster angle θB\theta_B. At this angle, the reflected and refracted rays turn out to be exactly perpendicular to each other, θB+r=90°\theta_B + r = 90°, where rr is the angle of refraction. Substituting r=90°−θBr = 90°-\theta_B into Snell’s law for a ray going from air into a medium of index nn:

sin⁡θB=nsin⁡(90°−θB)=ncos⁡θB\sin\theta_B = n\sin(90°-\theta_B) = n\cos\theta_B
Brewster's law
tan⁡θB=n\textcolor{#e08a1e}{\tan\theta_B} = n

At this one angle, the reflected light is purely polarized, vibrating only perpendicular to the plane of incidence (the component that would vibrate within that plane cannot be reflected at all once the reflected and refracted rays are perpendicular, since a dipole cannot radiate along its own axis of oscillation). This is why polarized sunglasses, oriented to block exactly this component, cut glare from water and glass so effectively: most glare is reflected light sitting near its own Brewster angle.

Worked example

Brewster angle for a glass window

Find the Brewster angle for light reflecting off ordinary glass (n=1.5n=1.5), and the angle of refraction at that incidence.

θB=tan⁡−1(1.5)≈56.3°\theta_B = \tan^{-1}(1.5) \approx \textcolor{#e08a1e}{56.3°}

and since θB+r=90°\theta_B + r = 90°:

r=90°−56.3°=33.7°r = 90° - 56.3° = \textcolor{#e08a1e}{33.7°}

As a check, Snell’s law directly: sin⁡(56.3°)=0.832\sin(56.3°) = 0.832 and 1.5sin⁡(33.7°)=1.5×0.555=0.8321.5\sin(33.7°) = 1.5\times0.555 = 0.832, matching exactly.

— From the NCERT exercises

Two of the chapter’s own exercise questions, with original worked solutions, exercising the frequency-invariance result of §10.2.1 and the resultant-intensity formula of §10.4.

NCERT Exercise 10.1

Monochromatic light of wavelength 589 nm is incident from air on a water surface. What are the wavelength, frequency and speed of (a) reflected, and (b) refracted light? Refractive index of water is 1.33.

Solution

(a) Reflection keeps the light in the same medium (air), so nothing about it changes at all:

λ=589 nm,f=cλ=3.00×108589×10−9≈5.09×1014 Hz,v=3.00×108 m/s\lambda = \textcolor{#e08a1e}{589\text{ nm}}, \qquad f = \dfrac{c}{\lambda} = \dfrac{3.00\times10^8}{589\times10^{-9}} \approx \textcolor{#e08a1e}{5.09\times10^{14}\text{ Hz}}, \qquad v = \textcolor{#e08a1e}{3.00\times10^8\text{ m/s}}

(b) By §10.2.1, frequency is fixed by the source and never changes on refraction, only speed and wavelength do:

v=cn=3.00×1081.33≈2.26×108 m/s,λ=vf≈444 nmv = \dfrac{c}{n} = \dfrac{3.00\times10^8}{1.33} \approx \textcolor{#e08a1e}{2.26\times10^8\text{ m/s}}, \qquad \lambda = \dfrac{v}{f} \approx \textcolor{#e08a1e}{444\text{ nm}}

NCERT Exercise 10.5

In Young's double-slit experiment using monochromatic light of wavelength λ, the intensity of light at a point on the screen where path difference is λ, is K units. What is the intensity of light at a point where path difference is λ/3?

Solution

For two equal-intensity slits, §10.4.3 gives I=4I0cos⁡2(ϕ/2)I=4I_0\cos^2(\phi/2), with ϕ=(2π/λ)Δ\phi = (2\pi/\lambda)\Delta. At Δ=λ\Delta=\lambda, ϕ=2π\phi=2\pi, so I=4I0cos⁡2(π)=4I0=KI = 4I_0\cos^2(\pi) = 4I_0 = K, which pins down I0=K/4I_0 = K/4. At Δ=λ/3\Delta=\lambda/3:

ϕ=2πλ⋅λ3=2π3\phi = \dfrac{2\pi}{\lambda}\cdot\dfrac{\lambda}{3} = \dfrac{2\pi}{3}I=4I0cos⁡2(π3)=4I0(0.5)2=I0=K4I = 4I_0\cos^2\left(\dfrac{\pi}{3}\right) = 4I_0(0.5)^2 = I_0 = \textcolor{#e08a1e}{\dfrac{K}{4}}
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