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Interference

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⁡(k⋅r−ωt+ϕ1)+E0cos⁡(k⋅r−ωt+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+2I1I2cos⁡ΔϕI = I_1 + I_2 + 2\sqrt{I_1 I_2}\cos\Delta\phi

Where Δϕ=ϕ2−ϕ1\Delta\phi = \phi_2 - \phi_1 is the phase difference.

3.2 Double-Slit Interference (Young”s Experiment)

Section titled “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 L≫dL \gg d.

Condition for bright fringes (constructive interference):

dsin⁡θ=mλ,m=0,±1,±2,…d\sin\theta = m\lambda, \quad m = 0, \pm 1, \pm 2, \ldots

Condition for dark fringes (destructive interference):

dsin⁡θ=(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=dsin⁡θ\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=(550×10−9)(2.0)/(0.10×10−3)=11.0×10−3\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) dsin⁡θ3=3λ  ⟹  sin⁡θ3=3(550×10−9)/(0.10×10−3)=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 sin⁡θ=λ/a=550/20=27.5×10−3\sin\theta = \lambda/a = 550/20 = 27.5 \times 10^{-3} Corresponding to interference order m=dsin⁡θ/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.

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: 2ntcos⁡θt2nt\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:

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

2ntcos⁡θt=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.

A beam splitter divides light into two beams that travel perpendicular paths and recombine. The path Difference Δ=2(d1−d2)\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=2000×632.8×10−9/2=6.328×10−4m = 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

Section titled “3.5 Coherence Length and Fringe Visibility”

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

V=Imax⁡−Imin⁡Imax⁡+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+I2 ∣γ(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(Δλ⋅Δxλ2)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 Δx≈λ2/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 Δx≪Lc\Delta x \ll L_c. A sodium lamp (Δλ≈0.6\Delta\lambda \approx 0.6 nm at λ=589\lambda = 589 nm) gives Lc≈0.58L_c \approx 0.58 mm. A HeNe laser (Δλ≈10−6\Delta\lambda \approx 10^{-6} nm) Gives Lc≈350L_c \approx 350 m — fringes are visible over enormous path differences.

3.6 Multiple-Beam Interference: The Fabry-Perot Etalon

Section titled “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=1−RT = 1 - RIlluminated at angle θ\theta inside a medium of refractive index nn:

ITI0=T2(1−R)2+4Rsin⁡2(δ/2)=11+Fsin⁡2(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) ndcos⁡θ\delta = (4\pi/\lambda)\,nd\cos\theta is the round-trip phase and F=4R/(1−R)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., 2ndcos⁡θ=mλ2nd\cos\theta = m\lambda.

Finesse:

F=πF2=πR1−R\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/(1−0.90)=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)/(2×1.00×10−3)=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)(1.00×10−3)/(500×10−9)=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=4.20×10−3\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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