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Interference

3.1 Superposition Principle

When two or more waves overlap, the resultant displacement is the sum of the individual displacements. For two coherent waves with amplitudes E1E_1 and E2E_2:

E=E1+E2=E0cos(krωt+ϕ1)+E0cos(krωt+ϕ2)E = E_1 + E_2 = E_0 \cos(\mathbf{k}\cdot\mathbf{r} - \omega t + \phi_1) + E_0 \cos(\mathbf{k}\cdot\mathbf{r} - \omega t + \phi_2)

The time-averaged intensity is:

I=I1+I2+2I1I2cosΔϕI = I_1 + I_2 + 2\sqrt{I_1 I_2}\cos\Delta\phi

Where Δϕ=ϕ2ϕ1\Delta\phi = \phi_2 - \phi_1 is the phase difference.

3.2 Double-Slit Interference (Young”s Experiment)

Two slits separated by distance dd are illuminated by coherent light of wavelength λ\lambda. The Screen is at distance LdL \gg d.

Condition for bright fringes (constructive interference):

dsinθ=mλ,m=0,±1,±2,d\sin\theta = m\lambda, \quad m = 0, \pm 1, \pm 2, \ldots

Condition for dark fringes (destructive interference):

dsinθ=(m+12)λ,m=0,±1,±2,d\sin\theta = \left(m + \frac{1}{2}\right)\lambda, \quad m = 0, \pm 1, \pm 2, \ldots

Derivation. The path difference between the two slits is Δ=dsinθ\Delta = d\sin\theta. Constructive Interference occurs when Δ=mλ\Delta = m\lambda (phase difference 2mπ2m\pi), and destructive when Δ=(m+1/2)λ\Delta = (m + 1/2)\lambda (phase difference (2m+1)π(2m+1)\pi). \blacksquare

The fringe spacing on the screen:

Δy=λLd\Delta y = \frac{\lambda L}{d}

Worked Example: Double-slit fringe calculation

Problem. In a Young”s double-slit experiment, light of wavelength λ=550\lambda = 550 nm passes Through slits separated by d=0.10d = 0.10 mm onto a screen at L=2.0L = 2.0 m. Find (a) the fringe spacing, (b) the angular position of the third bright fringe, and (c) the total number of bright fringes Visible within the central diffraction maximum (slit width a=0.020a = 0.020 mm).

Solution.

(a) Δy=λL/d=(550×109)(2.0)/(0.10×103)=11.0×103\Delta y = \lambda L/d = (550 \times 10^{-9})(2.0)/(0.10 \times 10^{-3}) = 11.0 \times 10^{-3} m =11.0= 11.0 mm.

(b) dsinθ3=3λ    sinθ3=3(550×109)/(0.10×103)=0.0165d\sin\theta_3 = 3\lambda \implies \sin\theta_3 = 3(550 \times 10^{-9})/(0.10 \times 10^{-3}) = 0.0165 θ3=0.945°\theta_3 = 0.945°.

(c) The diffraction envelope has its first minimum at sinθ=λ/a=550/20=27.5×103\sin\theta = \lambda/a = 550/20 = 27.5 \times 10^{-3} Corresponding to interference order m=dsinθ/λ=(d/a)=0.10/0.020=5m = d\sin\theta/\lambda = (d/a) = 0.10/0.020 = 5. Missing orders at m=±5,±10,m = \pm 5, \pm 10, \ldots. Visible bright fringes: m=0,±1,±2,±3,±4m = 0, \pm 1, \pm 2, \pm 3, \pm 4 Giving 9 bright fringes within the central maximum.

3.3 Thin-Film Interference

Light reflecting from a thin film of thickness tt and refractive index nn undergoes interference Between the wave reflected from the top surface and the wave reflected from the bottom surface.

Path difference: 2ntcosθt2nt\cos\theta_t where θt\theta_t is the angle of refraction inside the film.

A phase shift of π\pi occurs upon reflection from a medium of higher refractive index. The condition For constructive interference (bright reflection) is:

2ntcosθt=(m+12)λ(one phase shift)2nt\cos\theta_t = \left(m + \frac{1}{2}\right)\lambda \quad \mathrm{(one\ phase\ shift)}

2ntcosθt=mλ(zero or two phase shifts)2nt\cos\theta_t = m\lambda \quad \mathrm{(zero\ or\ two\ phase\ shifts)}

:::caution Common Pitfall Always count the number of π\pi phase shifts that occur upon reflection. A reflection from Low-to-high refractive index introduces a π\pi shift; high-to-low does not. For a soap film in Air, there is one π\pi shift (at the top surface). For a coating on glass (ncoat<nglassn_{\mathrm{coat} \lt n_{\mathrm{glass}}}), there is also one shift. The conditions for constructive and destructive interference swap depending on whether the total number of shifts is odd or even.

Worked Example: Anti-reflection coating design

Problem. Magnesium fluoride (n=1.38n = 1.38) is used as an anti-reflection coating on a glass lens (nglass=1.52n_{\mathrm{glass} = 1.52}). Find the minimum coating thickness for destructive interference in Reflected light at λ=550\lambda = 550 nm (normal incidence).

Solution. At the air-coating interface (low to high nn): π\pi phase shift. At the coating-glass interface (low to high nn): π\pi phase shift. Total: two phase shifts \equiv zero net phase shift from reflections.

For destructive interference (dark reflection) with zero net phase shift: 2nt=(m+1/2)λ2nt = (m + 1/2)\lambda.

Minimum thickness (m=0m = 0): t=λ/(4n)=550/(4×1.38)=99.6t = \lambda/(4n) = 550/(4 \times 1.38) = 99.6 nm.

This is the standard quarter-wave anti-reflection coating design.

Worked Example: Soap film colours

Problem. A soap film (n=1.33n = 1.33) of thickness t=300t = 300 nm is illuminated by white light at Normal incidence. Which visible wavelengths are strongly reflected?

Solution. Air-soap (low to high): one π\pi phase shift. Soap-air (high to low): no shift. Total: one phase shift. Constructive: 2nt=(m+1/2)λ2nt = (m + 1/2)\lambda.

λ=2nt/(m+1/2)=2(1.33)(300)/(m+1/2)=798/(m+1/2)\lambda = 2nt/(m + 1/2) = 2(1.33)(300)/(m + 1/2) = 798/(m + 1/2) nm.

m=0m = 0: λ=1596\lambda = 1596 nm (infrared, not visible). m=1m = 1: λ=798/1.5=532\lambda = 798/1.5 = 532 nm (green, visible). m=2m = 2: λ=798/2.5=319\lambda = 798/2.5 = 319 nm (ultraviolet, not visible).

The film appears green in reflected light.

3.4 Michelson Interferometer

A beam splitter divides light into two beams that travel perpendicular paths and recombine. The path Difference Δ=2(d1d2)\Delta = 2(d_1 - d_2) determines the interference pattern.

Moving mirror M1M_1 by distance Δd\Delta d shifts the pattern by m=2Δd/λm = 2\Delta d / \lambda fringes.

The Michelson interferometer is used for precise length measurements, the determination of Refractive indices, and was historically crucial in establishing the invariance of the speed of Light (Michelson-Morley experiment).

Worked Example: Michelson interferometer mirror displacement

Problem. A Michelson interferometer uses a HeNe laser (λ=632.8\lambda = 632.8 nm). When one mirror Is displaced, 2000 fringes cross a reference point. How far was the mirror moved?

Solution. Each fringe corresponds to a path difference change of λ\lambda. Moving the mirror by Δd\Delta d changes the path difference by 2Δd2\Delta d:

m=2Δd/λ    Δd=mλ/2=2000×632.8×109/2=6.328×104m = 2\Delta d/\lambda \implies \Delta d = m\lambda/2 = 2000 \times 632.8 \times 10^{-9}/2 = 6.328 \times 10^{-4} m =0.633= 0.633 mm.

3.5 Coherence Length and Fringe Visibility

The fringe visibility (or contrast) quantifies the sharpness of interference fringes:

V=ImaxIminImax+Imin\mathcal{V} = \frac{I_{\max} - I_{\min}}{I_{\max} + I_{\min}}

For two-beam interference with intensities I1I_1, I2I_2 and degree of temporal coherence γ|\gamma|:

V=2I1I2I1+I2γ(τ)\mathcal{V} = \frac{2\sqrt{I_1 I_2}}{I_1 + I_2}\,|\gamma(\tau)|

For equal intensities (I1=I2I_1 = I_2): V=γ(τ)\mathcal{V} = |\gamma(\tau)|.

The coherence function decays with path difference. For a Gaussian spectral profile of width Δλ\Delta\lambda:

γ(τ)=exp ⁣[π(ΔλΔxλ2)2]|\gamma(\tau)| = \exp\!\left[-\pi\left(\frac{\Delta\lambda \cdot \Delta x}{\lambda^2}\right)^2\right]

Where Δx=cτ\Delta x = c\tau is the path difference. Fringes become unresolvable when Δxλ2/Δλ=Lc\Delta x \approx \lambda^2/\Delta\lambda = L_cThe coherence length.

Implication for interferometry. To observe interference fringes, the path difference between The two arms must satisfy ΔxLc\Delta x \ll L_c. A sodium lamp (Δλ0.6\Delta\lambda \approx 0.6 nm at λ=589\lambda = 589 nm) gives Lc0.58L_c \approx 0.58 mm. A HeNe laser (Δλ106\Delta\lambda \approx 10^{-6} nm) Gives Lc350L_c \approx 350 m — fringes are visible over enormous path differences.

3.6 Multiple-Beam Interference: The Fabry-Perot Etalon

A Fabry-Perot etalon consists of two parallel, partially reflecting surfaces separated by Distance dd. Multiple reflections create many beams that interfere, producing sharp transmission Peaks.

For a lossless etalon with reflectance RR and transmittance T=1RT = 1 - RIlluminated at angle θ\theta inside a medium of refractive index nn:

ITI0=T2(1R)2+4Rsin2(δ/2)=11+Fsin2(δ/2)\frac{I_T}{I_0} = \frac{T^2}{(1 - R)^2 + 4R\sin^2(\delta/2)} = \frac{1}{1 + F\sin^2(\delta/2)}

Where δ=(4π/λ)ndcosθ\delta = (4\pi/\lambda)\,nd\cos\theta is the round-trip phase and F=4R/(1R)2F = 4R/(1-R)^2 is the coefficient of finesse.

Transmission maxima occur when δ=2mπ\delta = 2m\pi (m=0,1,2,m = 0, 1, 2, \ldots), i.e., 2ndcosθ=mλ2nd\cos\theta = m\lambda.

Finesse:

F=πF2=πR1R\mathcal{F} = \frac{\pi\sqrt{F}}{2} = \frac{\pi\sqrt{R}}{1 - R}

The finesse determines the sharpness of the peaks: higher RR gives sharper peaks.

Free spectral range (frequency spacing between adjacent peaks):

ΔνFSR=c2nd\Delta\nu_{\mathrm{FSR} = \frac{c}{2nd}}

Resolving power:

R=λδλ=mF\mathcal{R} = \frac{\lambda}{\delta\lambda} = m\mathcal{F}

Worked Example: Fabry-Perot resolving power

Problem. A Fabry-Perot etalon has plate separation d=1.00d = 1.00 mm, refractive index n=1.00n = 1.00 And reflectance R=0.90R = 0.90. Find the finesse, free spectral range, and minimum resolvable wavelength Difference at λ=500\lambda = 500 nm (normal incidence).

Solution. Finesse: F=π0.90/(10.90)=π(0.949)/0.10=29.8\mathcal{F} = \pi\sqrt{0.90}/(1 - 0.90) = \pi(0.949)/0.10 = 29.8.

Free spectral range: ΔνFSR=c/(2nd)=(3×108)/(2×1.00×103)=1.50×1011\Delta\nu_{\mathrm{FSR} = c/(2nd) = (3 \times 10^8)/(2 \times 1.00 \times 10^{-3}) = 1.50 \times 10^{11}} Hz.

Order number: m=2nd/λ=2(1.00)(1.00×103)/(500×109)=4000m = 2nd/\lambda = 2(1.00)(1.00 \times 10^{-3})/(500 \times 10^{-9}) = 4000.

Resolving power: R=mF=4000×29.8=1.19×105\mathcal{R} = m\mathcal{F} = 4000 \times 29.8 = 1.19 \times 10^5.

Minimum resolvable wavelength: δλ=λ/R=500/1.19×105=4.20×103\delta\lambda = \lambda/\mathcal{R} = 500/1.19 \times 10^5 = 4.20 \times 10^{-3} nm =4.20= 4.20 pm.

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