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PhysicsOP

Wave Optics

Apply concepts from Wave Optics to problem-solving. Focus on numerical practice and real-world applications.

2-3 Qs/year45 minPhase 2 · APPLICATION

Concept Core

A wavefront is the locus of all points in a medium that are in the same phase. Types include spherical (from a point source), cylindrical (from a linear source), and plane (at very large distances). Huygens' principle states that every point on a wavefront acts as a secondary source of wavelets; the new wavefront is the forward envelope of these wavelets. This principle elegantly derives Snell's law: when a plane wavefront hits a boundary, the change in wave speed causes the wavefront to tilt, producing refraction.
The ratio sin θ1\theta_{1}/sin θ2\theta_{2} = v1v2\frac{v_{1}}{v_{2}} = n2n1\frac{n_{2}}{n_{1}}.

Young's double slit experiment (YDSE) demonstrates interference of coherent light. Two slits S1S_{1} and S2S_{2}, separated by distance d, illuminate a screen at distance D (where D >> d).
The path difference at a point P at distance y from the center is Δ\Delta = d sin θ\theta approximately equal to dy/D for small angles.

Bright fringes (constructive interference) occur when Δ\Delta = n λ\lambda, giving positions yny_{n} = n λ\lambda D/d (n = 0, 1, 2, ...).
Dark fringes (destructive interference) occur when Δ\Delta = (2n - 1) λ2\frac{\lambda}{2}, giving positions yny_{n} = (2n - 1) λ\lambda D/(2d) (n = 1, 2, ...).
The fringe width β\beta = λ\lambda D/d; [β\beta] = [L], SI unit: m. The central fringe is always bright, and all fringes (except possibly the central one with white light) have equal width. Increasing D or λ\lambda widens the fringes; increasing d narrows them.

Intensity distribution: For identical slits, I = 4I0  cos24I_{0} \; cos^{2}(ϕ2\frac{\phi}{2}), where ϕ\phi = (2 πλ\frac{\pi}{\lambda}) Δ\Delta is the phase difference.
ImaxI_{max} = 4I04I_{0} (constructive, ϕ\phi = 0, 2π2\pi, ...), IminI_{min} = 0 (destructive, ϕ\phi = π\pi, 3π3\pi, ...).
For unequal intensities: I = I1I_{1} + I2I_{2} + 2 I1I2\sqrt{{I}_{1} {I}_{2}} cos ϕ\phi.

Coherent sources are essential for sustained interference — they must have the same frequency and a constant phase difference. Two independent sources (e.g., two light bulbs) are NOT coherent because their phases fluctuate randomly.

Single slit diffraction produces a central maximum of width 2 λ\lambda D/a (where a is the slit width), which is the brightest and widest feature.
Secondary minima occur at a sin θ\theta = n λ\lambda (n = 1, 2, ...), and secondary maxima at a sin θ\theta = (2n + 1) λ2\frac{\lambda}{2}. Each secondary maximum has width λ\lambda D/a — half the central maximum width. Intensity drops rapidly for higher-order maxima. Resolving power improves with larger aperture and shorter wavelength (Rayleigh's criterion).

Polarization proves that light is a transverse wave.
Brewster's law: When light hits a surface at the Brewster angle θp\theta_{p}, the reflected light is completely plane-polarized; tan θp\theta_{p} = n (refractive index).
At Brewster's angle, reflected and refracted rays are perpendicular: θp\theta_{p} + θr\theta_{r} = 90 deg.
Malus's law: When polarized light of intensity I0I_{0} passes through an analyzer at angle θ\theta to the polarization direction, the transmitted intensity is I = I0  cos2  θI_{0} \; cos^{2} \; \theta.
Through crossed polaroids (θ\theta = 90 deg), I = 0.
Inserting a third polaroid at 45 deg between two crossed polaroids allows light through: I = I08\frac{I_{0}}{8}.

The key testable concept is the YDSE fringe width formula β\beta = λ\lambda D/d and its variations (effect of changing medium, slit separation, or screen distance), which is among the most frequently asked formulae in NEET Physics.

Solved Numericals

N1. In YDSE, slit separation d = 0.5 mm, screen distance D = 1 m, wavelength λ\lambda = 600 nm. Find fringe width, position of the 3rd bright fringe, and position of the 2nd dark fringe.

Given: d = 0.5 mm = 5 x 10410^{-4} m, D = 1 m, λ\lambda = 600 nm = 6 x 10710^{-7} m.

Fringe width: β\beta = λ\lambda D/d = (6 x 10710^{-7} m x 1 m) / (5 x 10410^{-4} m) = 6 x 10710^{-7} / 5 x 10410^{-4} m = 1.2 x 10310^{-3} m = 1.2 mm.

3rd bright fringe (n = 3): y3y_{3} = n λ\lambda D/d = 3 x β\beta = 3 x 1.2 mm = 3.6 mm from center.

2nd dark fringe (n = 2): y2y_{2} = (2n - 1) λ\lambda D/(2d) = (2 x 2 - 1) x β2\frac{\beta}{2} = 3 x 0.6 mm = 1.8 mm. Alternatively: y2y_{2} = (2 x 2 - 1) x 600 x 10910^{-9} x 1 / (2 x 5 x 10410^{-4}) = 3 x 6 x 10710^{-7} / (10310^{-3}) = 1.8 x 10310^{-3} m = 1.8 mm.

Note: The 2nd dark fringe lies between the 1st and 2nd bright fringes (at 1.5 β\beta from center). The nth dark fringe position = (n - 0.5) β\beta.

N2. Unpolarized light of intensity I0I_{0} passes through three polaroids. The first and third are crossed (90 deg apart). The second is at 30 deg to the first. Find the intensity after each polaroid.

After Polaroid 1 (polarizer): Unpolarized light becomes plane-polarized. By definition, the transmitted intensity is I1I_{1} = I02\frac{I_{0}}{2} (half the unpolarized intensity is transmitted).

After Polaroid 2 (at 30 deg to Polaroid 1): Apply Malus's law with θ\theta = 30 deg: I2I_{2} = I1  cos2I_{1} \; cos^{2}(30 deg) = (I02\frac{I_{0}}{2})(32\frac{\sqrt{3}}{2})2 = (I02\frac{I_{0}}{2})(34\frac{3}{4}) = 3I08\frac{3I_{0}}{8}.

After Polaroid 3 (at 90 deg to Polaroid 1, so at 90 - 30 = 60 deg to Polaroid 2): Apply Malus's law with θ\theta = 60 deg: I3I_{3} = I2  cos2I_{2} \; cos^{2}(60 deg) = (3I08\frac{3I_{0}}{8})(12\frac{1}{2})2 = (3I08\frac{3I_{0}}{8})(14\frac{1}{4}) = 3I032\frac{3I_{0}}{32}.

Final intensity: I = 3I032\frac{3I_{0}}{32}.

If Polaroid 2 were at 45 deg instead: I3I_{3} = (I02\frac{I_{0}}{2})(cos2cos^{2} 45)(cos2cos^{2} 45) = (I02\frac{I_{0}}{2})(12\frac{1}{2})(12\frac{1}{2}) = I08\frac{I_{0}}{8}.

Key insight: Without the middle polaroid, no light passes through crossed polaroids. Inserting a polaroid between them at any angle other than 0 deg or 90 deg allows some light through.

N3. Find Brewster's angle for a glass surface with refractive index n = 1.732. Verify that reflected and refracted rays are perpendicular.

Brewster's law: tan θp\theta_{p} = n = 1.732. θp\theta_{p} = arctan(1.732) = 60 deg.

Verification: At Brewster's angle, the refracted angle θr\theta_{r} satisfies: By Snell's law: sin θp\theta_{p} = n sin θr\theta_{r} sin 60 deg = 1.732 x sin θr\theta_{r} 0.866 = 1.732 x sin θr\theta_{r} sin θr\theta_{r} = 0.8661\frac{866}{1}.732 = 0.5 θr\theta_{r} = 30 deg.

Check perpendicularity: θp\theta_{p} + θr\theta_{r} = 60 + 30 = 90 deg. Verified.

The reflected and refracted rays are perpendicular at the Brewster angle. The reflected light is completely plane-polarized with the electric field vector perpendicular to the plane of incidence.

Key Testable Concept

The reflected and refracted rays are perpendicular at the Brewster angle. The reflected light is completely plane-polarized with the electric field vector perpendicular to the plane of incidence.

Comparison Tables

A) YDSE Formula Table

QuantityFormulaVariables (physical meaning)Dimensional FormulaSI Unit
Path differenceΔ\Delta = d sin θ\theta ~ dy/Dd = slit separation, y = distance from center, D = screen distance, θ\theta = angular position[L]m
Bright fringe position (nth)yny_{n} = n λ\lambda D/dn = order (0, 1, 2, ...), λ\lambda = wavelength[L]m
Dark fringe position (nth)yny_{n} = (2n-1) λ\lambda D/(2d)n = order (1, 2, 3, ...)[L]m
Fringe widthβ\beta = λ\lambda D/dλ\lambda, D, d as above[L]m
Intensity (equal slits)I = 4I0  cos24I_{0} \; cos^{2}(ϕ2\frac{\phi}{2})I0I_{0} = individual slit intensity, ϕ\phi = phase difference[M T3T^{-3}]W/m2m^{2}
Phase differenceϕ\phi = (2πλ\frac{2\pi}{\lambda}) Δ\DeltaΔ\Delta = path differenceDimensionlessradian
Maximum intensityImaxI_{max} = 4I04I_{0}At ϕ\phi = 0, 2π2\pi, 4π4\pi, ... (constructive)[M T3T^{-3}]W/m2m^{2}
Minimum intensityIminI_{min} = 0At ϕ\phi = π\pi, 3π3\pi, 5π5\pi, ... (destructive)[M T3T^{-3}]W/m2m^{2}

B) Single Slit Diffraction

FeatureFormulaConditionWidth
Central maximumAt θ\theta = 0Angular width = 2 λ\lambda/a; Linear width = 2 λ\lambda D/a
nth secondary minimuma sin θ\theta = n λ\lambdan = 1, 2, 3, ...
nth secondary maximuma sin θ\theta = (2n+1) λ2\frac{\lambda}{2}n = 1, 2, 3, ...
Angular width = λ\lambda/a; Linear width = λ\lambda D/a
Intensity patternCentral max is brightest; secondary maxima rapidly decreaseI1I0\frac{I_{1}}{I_{0}} ~ 4.5%, I2I0\frac{I_{2}}{I_{0}} ~ 1.6%Central is TWICE the width of secondary maxima

C) Polarization Formulas

LawFormulaVariablesConditionSI Unit
Brewster's lawtan θp\theta_{p} = nθp\theta_{p} = Brewster (polarizing) angle, n = refractive indexReflected light completely polarized; θp\theta_{p} + θr\theta_{r} = 90 degθp\theta_{p} in degrees or radians
Malus's lawI = I0  cos2  θI_{0} \; cos^{2} \; \thetaI0I_{0} = incident polarized intensity, θ\theta = angle between polarization and analyzer axisApplicable to polarized light through analyzerW/m2m^{2}
Unpolarized through polaroidI = I02\frac{I_{0}}{2}I0I_{0} = incident unpolarized intensityFirst polaroid always transmits halfW/m2m^{2}
Two crossed polaroidsI = 0θ\theta = 90 deg between axesNo transmissionW/m2m^{2}
Three polaroids (crossed + middle at 45 deg)I = I08\frac{I_{0}}{8}Middle at 45 deg to bothAllows light through despite crossed endsW/m2m^{2}

D) YDSE vs Single Slit Diffraction Comparison

FeatureYDSE (Interference)Single Slit (Diffraction)Key Difference
SourceTwo coherent slitsOne narrow slitDouble vs single aperture
Central fringeBright, same width as othersBright, TWICE as wide as secondary maximaCentral max much wider in diffraction
Fringe widthβ\beta = λ\lambda D/d (all equal)Central: 2 λ\lambda D/a; Secondary: λ\lambda D/aYDSE fringes are uniform; diffraction fringes are not
Intensity patternEqual maxima (ImaxI_{max} = 4I04I_{0})Central max brightest; secondary maxima much weakerYDSE maxima are equal; diffraction maxima decrease rapidly
Minima conditionΔ\Delta = (2n-1) λ2\frac{\lambda}{2}a sin θ\theta = n λ\lambdaDifferent conditions
Slit width roled = slit separation mattersa = slit width mattersd for interference, a for diffraction

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