Physics 2 Quiz: Diffraction And Resolving Power
15 questions · exam conditions
0:00
Diffraction And Resolving PowerQuestion 1 of 15

A radio telescope array is used to observe two closely spaced quasars at a wavelength of λ=21\lambda = 21 cm (the neutral hydrogen line). The array has a baseline (effective aperture diameter) of D=3000D = 3000 km. A single-dish optical telescope with a 10-meter mirror observing at λ=500\lambda = 500 nm is also available.

Which instrument has the finer angular resolution, and by approximately what factor does it outperform the other? Use the Rayleigh criterion θ1.22λ/D\theta \approx 1.22 \lambda / D.

The radio array is superior by a factor of approximately 700700 (roughly 10310^3), because although the radio wavelength is 4.2×1054.2 \times 10^5 times longer than optical, the baseline is 3×1083 \times 10^8 times larger, making the ratio θradio/θoptical1.4×103\theta_{\text{radio}}/\theta_{\text{optical}} \approx 1.4 \times 10^{-3}.
The optical telescope is superior by a factor of approximately 10310^3, because the much shorter wavelength overcomes the advantage of the large radio baseline, yielding θoptical/θradio103\theta_{\text{optical}}/\theta_{\text{radio}} \approx 10^{-3}.
The two instruments have nearly equal angular resolution because the longer wavelength of the radio array is offset by its proportionally larger baseline, and both yield θ108\theta \approx 10^{-8} rad.
The radio array is superior by a factor of approximately 10610^6, because the baseline of 3×1093 \times 10^9 m utterly dominates the wavelength difference, giving θradio1013\theta_{\text{radio}} \approx 10^{-13} rad.
← Back to quizzes

Physics 2 Quiz

Physics 2 Quiz: Diffraction And Resolving Power

Practice Diffraction And Resolving Power in Physics 2 with focused quiz questions that help you check what you know, review explanations, and build confidence with test-style prompts.

What this quiz covers

This quiz focuses on Diffraction And Resolving Power, giving you a quick way to practice the rules, question types, and explanations that matter most for Physics 2.

How to use this quiz

Try each quiz question before looking at the correct answer. Use the explanations to review missed ideas, then come back to similar questions until the pattern feels familiar.

All questions

Question 1

A radio telescope array is used to observe two closely spaced quasars at a wavelength of λ=21\lambda = 21 cm (the neutral hydrogen line). The array has a baseline (effective aperture diameter) of D=3000D = 3000 km. A single-dish optical telescope with a 10-meter mirror observing at λ=500\lambda = 500 nm is also available.

Which instrument has the finer angular resolution, and by approximately what factor does it outperform the other? Use the Rayleigh criterion θ1.22λ/D\theta \approx 1.22 \lambda / D.

  1. The radio array is superior by a factor of approximately 700700 (roughly 10310^3), because although the radio wavelength is 4.2×1054.2 \times 10^5 times longer than optical, the baseline is 3×1083 \times 10^8 times larger, making the ratio θradio/θoptical1.4×103\theta_{\text{radio}}/\theta_{\text{optical}} \approx 1.4 \times 10^{-3}. (correct answer)
  2. The optical telescope is superior by a factor of approximately 10310^3, because the much shorter wavelength overcomes the advantage of the large radio baseline, yielding θoptical/θradio103\theta_{\text{optical}}/\theta_{\text{radio}} \approx 10^{-3}.
  3. The two instruments have nearly equal angular resolution because the longer wavelength of the radio array is offset by its proportionally larger baseline, and both yield θ108\theta \approx 10^{-8} rad.
  4. The radio array is superior by a factor of approximately 10610^6, because the baseline of 3×1093 \times 10^9 m utterly dominates the wavelength difference, giving θradio1013\theta_{\text{radio}} \approx 10^{-13} rad.
Explanation: Whenever you compare angular resolution across instruments, remember that the Rayleigh criterion θ1.22λ/D\theta \approx 1.22\lambda/D means finer resolution (smaller θ\theta) comes from a smaller wavelength-to-diameter ratio. The instrument that wins is whichever minimizes λ/D\lambda/D. Let's compute both. For the radio array: λradio=0.21 m\lambda_{\text{radio}} = 0.21 \text{ m}, Dradio=3×106 mD_{\text{radio}} = 3 \times 10^6 \text{ m}, so θradio1.22×(0.21)/(3×106)8.5×108 rad\theta_{\text{radio}} \approx 1.22 \times (0.21)/(3\times10^6) \approx 8.5 \times 10^{-8} \text{ rad}. For the optical telescope: λopt=5×107 m\lambda_{\text{opt}} = 5\times10^{-7} \text{ m}, Dopt=10 mD_{\text{opt}} = 10 \text{ m}, so θopt1.22×(5×107)/106.1×108 rad\theta_{\text{opt}} \approx 1.22 \times (5\times10^{-7})/10 \approx 6.1\times10^{-8} \text{ rad}. The ratio is θradio/θoptical1.4×103\theta_{\text{radio}}/\theta_{\text{optical}} \approx 1.4\times10^{-3}... wait — that means the radio array has the smaller angle and wins by a factor of roughly 700103700 \approx 10^3. Answer A captures this correctly: even though the radio wavelength is 4.2×1054.2\times10^5 times longer, the baseline is 3×1083\times10^8 times larger, so the net ratio strongly favors the radio array. B is wrong because it claims the optical telescope wins — it inverts the correct conclusion. The optical wavelength is shorter, yes, but the 10 m mirror simply cannot match a 3000 km baseline. C is tempting but incorrect: the resolutions are close in order of magnitude, but they are not equal, and neither equals 10810^{-8} rad exactly — the radio array is meaningfully better. D uses a wildly wrong baseline (3×1093\times10^9 m instead of 3×1063\times10^6 m) and invents an implausible θ1013\theta \approx 10^{-13} rad. Your strategy: always plug in SI units carefully and compute both λ/D\lambda/D values before declaring a winner — intuition about "big wavelength" or "big aperture" alone will mislead you.

Question 2

A diffraction grating with NN slits and slit spacing dd is used in order mm. A student argues: 'To double the resolving power of this grating without changing the wavelength or the order of diffraction, I can simply double the number of illuminated slits by using a wider beam.'

Is the student's reasoning correct, and what is the resolving power RR of a diffraction grating expressed in terms of the relevant parameters?

  1. The student is correct. The resolving power is R=mNR = mN, which depends only on the order mm and number of illuminated slits NN. Doubling NN at constant mm precisely doubles RR, regardless of grating spacing or aperture width. (correct answer)
  2. The student is incorrect. The resolving power is R=d/λR = d/\lambda, which depends on slit spacing and wavelength. Doubling the number of slits changes the aperture but not the spacing, so RR is unchanged.
  3. The student is correct only if the grating is used in first order (m=1m = 1). For higher orders, the resolving power saturates at R=NR = N regardless of mm, so doubling NN still doubles RR only in first order.
  4. The student is correct in principle, but the resolving power is R=mN/2R = mN/2 for a grating used in even orders and R=mNR = mN for odd orders, so the effect of doubling NN depends on which order is being used.
Explanation: When you encounter questions about diffraction grating resolution, the central formula to anchor on is the resolving power: R=mNR = mN, where mm is the diffraction order and NN is the number of illuminated slits. This formula comes directly from the Rayleigh criterion applied to grating diffraction — the minimum resolvable wavelength difference is Δλ=λ/mN\Delta\lambda = \lambda/mN, so R=λ/Δλ=mNR = \lambda/\Delta\lambda = mN. Notice what's in that formula and what isn't: no slit spacing dd, no aperture width on its own, just order and slit count. The student's reasoning in choice A is exactly right. If you keep mm fixed and double NN by widening the beam to illuminate more slits, you double RR directly and precisely. The relationship is linear and universal — it holds for any order, any spacing. Choice B is wrong because it invents a false formula R=d/λR = d/\lambda. Slit spacing dd determines where principal maxima appear (via dsinθ=mλd\sin\theta = m\lambda), not how well the grating resolves nearby wavelengths. Confusing the grating equation with the resolving power formula is a classic trap. Choice C introduces a fictitious "saturation" effect that doesn't exist in grating physics. The formula R=mNR = mN applies at all orders — there is no special behavior at m=1m = 1. Choice D fabricates an order-parity dependence (even vs. odd orders) that has no physical basis whatsoever. Study tip: Memorize R=mNR = mN as a standalone fact. On exam questions, watch for distractors that smuggle in dd or λ\lambda — those belong to the grating equation, not the resolving power.

Question 3

A coherent light source (laser) of wavelength λ\lambda illuminates two identical narrow slits separated by dd (Young's double-slit geometry). Due to the finite width aa of each slit (a<da < d), the intensity envelope is modulated by single-slit diffraction. The experimenter observes that the m=4m = 4 double-slit maximum is entirely missing from the pattern. Which of the following conditions on aa and dd must hold, and what does this imply about the effective number of observable bright fringes within the central diffraction maximum?

  1. The condition is d/a=4d/a = 4, meaning the 4th-order double-slit maximum coincides with the first single-slit minimum. Within the central diffraction envelope, there are 6 observable bright fringes (orders 2,1,0,+1,+2-2, -1, 0, +1, +2 are visible, while orders ±3\pm 3 are partially suppressed near the envelope edge).
  2. The condition is d/a=4d/a = 4, meaning the 4th-order double-slit maximum coincides with the first single-slit minimum. Within the central diffraction envelope, there are 8 observable bright fringes (orders 3-3 through +3+3 plus two half-intensity fringes at ±4\pm 4, which are suppressed but not fully absent).
  3. The condition is a/d=4a/d = 4, meaning the slit width is four times the slit separation, which places the first single-slit minimum at the position of the 4th double-slit maximum. Within the central envelope there are only 3 observable fringes (orders 1,0,+1-1, 0, +1) because the very wide slits suppress all higher orders rapidly.
  4. The condition is d/a=4d/a = 4, meaning the 4th-order double-slit maximum coincides with the first single-slit minimum. Within the central diffraction envelope (between the first single-slit minima), there are 7 observable bright fringes (orders 3,2,1,0,+1,+2,+3-3, -2, -1, 0, +1, +2, +3), since orders ±4\pm 4 are missing. (correct answer)
Explanation: When double-slit and single-slit effects combine, you need to track two separate conditions simultaneously: where double-slit maxima occur (dsinθ=mλd\sin\theta = m\lambda) and where single-slit minima occur (asinθ=pλa\sin\theta = p\lambda). A "missing order" happens when a double-slit maximum lands exactly on a single-slit minimum, making the envelope zero out that fringe entirely. If the m=4m = 4 double-slit maximum is missing, it must coincide with the first (p=1p = 1) single-slit minimum. Setting dsinθ=4λd\sin\theta = 4\lambda equal to asinθ=λa\sin\theta = \lambda gives d/a=4d/a = 4. This is the governing condition. The central diffraction envelope spans from the 1-1 to +1+1 single-slit minima, meaning it covers all double-slit orders satisfying m<d/a=4|m| < d/a = 4. That yields orders m=3,2,1,0,+1,+2,+3m = -3, -2, -1, 0, +1, +2, +3 — exactly 7 visible fringes — with m=±4m = \pm4 zeroed out. This confirms D is correct. A is wrong because it counts only 6 fringes and incorrectly claims orders ±3\pm3 are "partially suppressed." They sit well inside the central envelope and are fully visible. B is wrong because it invents "half-intensity fringes at ±4\pm4" — those orders are completely extinguished by the single-slit minimum, not merely dimmed. C has the ratio inverted (a/d=4a/d = 4 would mean the slits are wider than their separation, a physically nonsensical setup for standard double-slit geometry) and produces an entirely wrong fringe count. A handy rule: when d/a=Nd/a = N, the ±N\pm N orders vanish, and you get 2N12N - 1 observable fringes within the central maximum. Memorize this pattern — it appears frequently on diffraction problems.

Question 4

In a single-slit pattern, screen distance doubles, slit width halves, and wavelength doubles. Central maximum width:

  1. Quadruples
  2. Doubles
  3. Octuples (correct answer)
  4. Unchanged
Explanation: Central maximum width scales as wavelength times screen distance divided by slit width: W = 2λL/a. Doubling wavelength and screen distance each double the width, multiplying by 4; halving slit width doubles it again, so the width becomes 8 times larger. The tempting mistake is picking quadruples after doubling wavelength and screen distance but forgetting the slit-width factor.

Question 5

A 3.0 cm grating has 2000 lines/cm. In second order at 600 nm, the smallest resolvable Δλ is:

  1. 0.10 nm
  2. 0.30 nm
  3. 0.15 nm
  4. 0.05 nm (correct answer)
Explanation: Total lines on the grating are 3.0 cm times 2000 lines/cm = 6000. Resolving power is mN = 2 times 6000 = 12,000, so Δλ = 600 nm / 12,000 = 0.05 nm. The tempting 0.15 nm comes from using 2000 lines/cm instead of the full 6000 lines in the grating.

Question 6

A grating with 5000 lines/cm has slit width 1.0 μm. At which order is the first missing maximum?

  1. 2nd (correct answer)
  2. 1st
  3. 3rd
  4. 4th
Explanation: The grating spacing d is 1/5000 cm = 2 μm, twice the slit width a = 1 μm. A maximum vanishes when an interference order lands on a diffraction minimum: d sinθ = mλ and a sinθ = nλ give m/n = d/a = 2. The first such coincidence is n = 1, so m = 2, the 2nd order. The 1st order is tempting but it falls before the first diffraction minimum, so it isn't missing.

Question 7

Which change does NOT improve the resolution of a diffraction-limited telescope?

  1. Using blue instead of red
  2. Enlarging the objective
  3. Using a stronger eyepiece (correct answer)
  4. Decreasing the wavelength
Explanation: Resolution in a diffraction-limited telescope is set by 1.22 lambda / D. Shorter wavelength (blue) or larger objective diameter D shrinks that limit, so those improve it. A stronger eyepiece only magnifies the image; it cannot change lambda or D, so it doesn't improve resolution. The tempting wrong choice is enlarging the objective, which does improve resolution by increasing D.

Question 8

Two stars subtend 0.10 arcsec. What aperture diameter just resolves them at 550 nm?

  1. 1.1 m
  2. 1.4 m (correct answer)
  3. 2.8 m
  4. 0.69 m
Explanation: Convert 0.10 arcsec to radians: 0.10 / 206265 = 4.85 x 10^-7 rad. The Rayleigh criterion gives theta = 1.22 lambda / D, so D = 1.22 (550 x 10^-9) / (4.85 x 10^-7) = 1.4 m. The 1.1 m trap comes from omitting the 1.22 factor for a circular aperture.

Question 9

In X-ray crystallography, Bragg diffraction from crystal planes with spacing dd follows 2dsinθ=mλ2d\sin\theta = m\lambda. A crystallographer wants to improve the spatial resolution of the technique (i.e., resolve finer features in the electron density map). Which of the following strategies correctly achieves this and for the correct physical reason?

  1. Use a shorter X-ray wavelength, because smaller λ\lambda allows diffraction at larger angles θ\theta for a given dd, populating higher spatial-frequency components in reciprocal space and improving real-space resolution by the crystallographic analogue of Abbe's diffraction limit. (correct answer)
  2. Use a longer X-ray wavelength, because larger λ\lambda increases the Bragg angle θ\theta for the same crystal spacing, spreading diffraction spots further apart on the detector and making them easier to measure accurately, which improves resolution.
  3. Rotate the crystal more slowly during data collection, because slower rotation increases the exposure time per reflection, improving the signal-to-noise ratio of each Bragg peak and therefore the phase information needed for high-resolution maps.
  4. Increase the crystal-to-detector distance, because placing the detector farther from the crystal increases the angular spread of the diffraction pattern on the detector, improving the ability to distinguish closely spaced Bragg peaks and hence the resolution.
Explanation: Whenever you see a question about X-ray crystallography resolution, think in terms of reciprocal space: real-space resolution improves when you can measure diffraction data at higher spatial frequencies, meaning larger scattering angles and higher-order reflections. From Bragg's law 2dsinθ=mλ2d\sin\theta = m\lambda, you can solve for the minimum resolvable spacing: dmin=λ2sinθmaxd_{min} = \frac{\lambda}{2\sin\theta_{max}}. To resolve finer features (smaller dmind_{min}), you need either a smaller λ\lambda or a larger accessible θmax\theta_{max}. Using shorter-wavelength X-rays directly shrinks λ\lambda, which means reflections from smaller dd-spacings now satisfy Bragg's law within physically accessible angles (θ90°\theta \leq 90°). This populates higher spatial-frequency terms in the Fourier reconstruction of the electron density, directly analogous to Abbe's diffraction limit in optical microscopy. Answer A is correct for exactly this reason. Answer B is tempting because larger λ\lambda does increase θ\theta for a fixed dd, but this works against resolution—it actually excludes high-frequency data from being collected at all, since those reflections would require sinθ>1\sin\theta > 1, which is impossible. Spreading low-order spots apart does not improve resolution. Answer C confuses signal-to-noise with resolution. Better SNR improves the accuracy of measured intensities and phases, which helps map quality, but it does not extend the resolution limit. The two are related but distinct concepts. Answer D is similarly flawed: increasing crystal-to-detector distance spreads spots physically, aiding indexing, but it does not extend the maximum angle captured—it actually reduces the angular coverage of the detector, potentially losing high-angle data. Study tip: Always distinguish between factors that extend the resolution limit (access to higher spatial frequencies) versus those that improve data quality at existing resolution. These are a common point of confusion on physics and crystallography exams.

Question 10

Two stars separated by an angle θ=2.0×107\theta = 2.0 \times 10^{-7} rad are observed through a telescope with a circular aperture of diameter DD. The telescope operates at λ=550\lambda = 550 nm. What is the minimum aperture diameter required to resolve the stars by the Rayleigh criterion, and if the aperture is instead set to half this minimum value, by what factor does the minimum resolvable angle increase?

  1. The minimum diameter is Dmin1.7D_{\min} \approx 1.7 m; at half this aperture (D=0.85D = 0.85 m), the minimum resolvable angle doubles to 4.0×1074.0 \times 10^{-7} rad, correctly placing the stars at the new Rayleigh limit and confirming they are unresolved.
  2. The minimum diameter is Dmin3.4D_{\min} \approx 3.4 m; at half this aperture, the minimum resolvable angle increases by a factor of 2\sqrt{2}, because the diffraction-limited intensity at the Rayleigh separation drops by half, and the angular criterion scales with the square root of intensity.
  3. The minimum diameter is Dmin3.4D_{\min} \approx 3.4 m; at half this aperture (D=1.7D = 1.7 m), the Rayleigh limit doubles to 4.0×1074.0 \times 10^{-7} rad, so the stars are no longer resolved and the minimum resolvable angle is twice as large as the stellar separation. (correct answer)
  4. The minimum diameter is Dmin3.4D_{\min} \approx 3.4 m; at half this aperture, the minimum resolvable angle increases by a factor of four, because diffraction peak intensity scales as D2D^2, so halving DD quarters the intensity and quadruples the effective angular resolution limit.
Explanation: When a question asks about resolving two objects through a circular aperture, your first instinct should be the Rayleigh criterion: θmin=1.22λD\theta_{min} = 1.22 \frac{\lambda}{D}. This sets the smallest angular separation a telescope can resolve — and it scales inversely with aperture diameter. To find the minimum diameter needed to resolve stars separated by θ=2.0×107\theta = 2.0 \times 10^{-7} rad at λ=550\lambda = 550 nm, set θmin=θ\theta_{min} = \theta and solve: Dmin=1.22λθ=1.22×550×1092.0×1073.4 mD_{min} = \frac{1.22\lambda}{\theta} = \frac{1.22 \times 550 \times 10^{-9}}{2.0 \times 10^{-7}} \approx 3.4 \text{ m} This confirms C starts correctly. Now, if you halve the aperture to D=1.7D = 1.7 m, the new Rayleigh limit becomes: θmin=1.22λD/2=2×1.22λD=2×(2.0×107)=4.0×107 rad\theta_{min}' = \frac{1.22\lambda}{D/2} = 2 \times \frac{1.22\lambda}{D} = 2 \times (2.0 \times 10^{-7}) = 4.0 \times 10^{-7} \text{ rad} The minimum resolvable angle doubles, and since the stellar separation is now below this limit, the stars are unresolved. Answer C is correct. A gets the doubling of the angle right but miscalculates DminD_{min} as 1.7 m — that's actually half the correct minimum, so it contradicts itself internally. B invents a square-root relationship between intensity and the angular criterion. The Rayleigh formula has no such dependence — this is a fabricated distractor. D incorrectly claims that halving DD quadruples the angular resolution limit by conflating intensity scaling (D2\propto D^2) with angular resolution. These are separate concepts — the Rayleigh criterion depends linearly on 1/D1/D, not 1/D21/D^2. Study tip: Memorize θmin=1.22λ/D\theta_{min} = 1.22\lambda/D and internalize that it's a linear inverse relationship — halving DD always doubles θmin\theta_{min}, nothing more complex.

Question 11

A spectrometer uses a diffraction grating with 600 lines/mm and a ruled width of 5.0 cm. A spectroscopist wants to resolve the sodium doublet, which consists of two lines at λ1=589.0\lambda_1 = 589.0 nm and λ2=589.6\lambda_2 = 589.6 nm.

What is the minimum resolving power required to separate the sodium doublet, and what is the lowest diffraction order in which this grating can achieve it?

  1. The required resolving power is R982R \approx 982. The number of illuminated slits is N=600×5.0=3,000N = 600 \times 5.0 = 3{,}000, giving R1=3,000R_1 = 3{,}000 in first order. This exceeds 982, so the doublet is resolved in m=1m = 1.
  2. The required resolving power is R982R \approx 982. With N=30,000N = 30{,}000 slits, first-order resolving power is R1=30,000R_1 = 30{,}000, which exceeds 982; however, the free spectral range in first order is ΔλFSR=λ/m589\Delta\lambda_{\text{FSR}} = \lambda/m \approx 589 nm, which is too narrow to include both sodium lines without order overlap, so m=2m = 2 is actually required.
  3. The required resolving power is R1,964R \approx 1{,}964, because both lines must each individually satisfy the Rayleigh criterion, effectively doubling the resolving power needed. With R1=30,000R_1 = 30{,}000 in first order, m=1m = 1 still suffices.
  4. The required resolving power is R982R \approx 982. With N=30,000N = 30{,}000 illuminated slits, the grating achieves R=mN=30,000R = mN = 30{,}000 in first order — far exceeding the requirement — so the doublet is resolved in m=1m = 1. (correct answer)
Explanation: When a question asks about resolving a spectral doublet with a diffraction grating, you need two formulas: the required resolving power and the grating's actual resolving power. The required resolving power is defined as R=λ/ΔλR = \lambda / \Delta\lambda, where λ\lambda is the average wavelength and Δλ\Delta\lambda is the separation between the two lines. Here, λ589.0\lambda \approx 589.0 nm and Δλ=0.6\Delta\lambda = 0.6 nm, giving R=589.0/0.6982R = 589.0/0.6 \approx 982. A grating's actual resolving power in order mm is R=mNR = mN, where NN is the total number of illuminated slits. With 600 lines/mm over 5.0 cm = 50 mm, you get N=600×50=30,000N = 600 \times 50 = 30{,}000 slits. In first order, R1=1×30,000=30,000R_1 = 1 \times 30{,}000 = 30{,}000, which vastly exceeds 982 — so the doublet is resolved in m=1m = 1. That makes D correct. Choice A makes a critical arithmetic error: it multiplies 600 lines/mm by 5.0 (treating the width as 5.0 mm instead of 50 mm), yielding only 3,000 slits — off by a factor of 10. Choice B correctly finds N=30,000N = 30{,}000 but then invents a free spectral range argument that doesn't apply here. The FSR concern arises when two lines from different orders overlap — not when both lines sit well within the same order. Choice C misunderstands the Rayleigh criterion: you only need one resolving power calculation for the pair of lines, not one per line. Study tip: Always convert grating width to millimeters before computing NN — unit errors here are the most common trap, as seen in choice A.

Question 12

A single slit of width aa is illuminated by monochromatic light of wavelength λ\lambda. An experimenter claims that doubling the slit width while simultaneously doubling the wavelength will keep the central diffraction maximum the same angular width AND double the intensity at the center. Which of the following correctly evaluates this claim?

  1. The claim is entirely correct: the angular half-width θλ/a\theta \approx \lambda/a is unchanged by the simultaneous doubling, and the on-axis intensity scales as a2a^2, which quadruples — contradicting the doubling claim for intensity but confirming the angular part.
  2. The claim is partially correct: the angular half-width remains the same since λ/a\lambda/a is unchanged, but the central-maximum intensity scales as (a/λ)2(a/\lambda)^2, which is also unchanged — so intensity does not double. (correct answer)
  3. The claim is entirely wrong: doubling both λ\lambda and aa narrows the central maximum by a factor of two because intensity redistributes into higher-order maxima, and on-axis intensity actually decreases.
  4. The claim is partially correct: the central maximum angular width is unchanged because λ/a\lambda/a is constant, but the on-axis intensity scales as a2/λa^2/\lambda, which doubles when both are doubled — so both parts of the claim are valid in this specific scenario.
Explanation: When analyzing single-slit diffraction, you need to track two separate quantities independently: the angular width of the central maximum and the on-axis intensity. Conflating their scaling behavior is the core trap in this question. The angular half-width of the central maximum is given by θλ/a\theta \approx \lambda/a. When both λ\lambda and aa are doubled, the ratio λ/a\lambda/a remains unchanged — so the angular width is indeed preserved. That part of the experimenter's claim holds up. Now for intensity. The on-axis intensity for single-slit diffraction scales as I0a2/λ2I_0 \propto a^2/\lambda^2, not simply a2a^2. When both aa and λ\lambda are doubled: the numerator scales by (2a)2=4a2(2a)^2 = 4a^2 and the denominator by (2λ)2=4λ2(2\lambda)^2 = 4\lambda^2, leaving the ratio — and therefore the intensity — completely unchanged. The experimenter's intensity claim fails entirely. This makes B the correct answer: the angular width is preserved, but the intensity does not double. Choice A is wrong because it claims intensity scales as a2a^2 alone, ignoring the λ2\lambda^2 dependence in the denominator — a partial formula that leads to an incorrect quadrupling prediction. Choice C is wrong on both counts: the central maximum width doesn't narrow, and intensity doesn't decrease; the λ/a\lambda/a ratio governs both behaviors here. Choice D invents a scaling of a2/λa^2/\lambda, which has no physical basis in the standard single-slit intensity formula. As a strategy: whenever a diffraction question changes multiple parameters simultaneously, always substitute into the full formula rather than reasoning about one variable at a time — that's where most errors occur.

Question 13

A microscope objective with numerical aperture NA=nsinα\text{NA} = n\sin\alpha (where nn is the refractive index of the medium and α\alpha is the half-angle of the acceptance cone) is used to image two fluorescent point sources. According to the Abbe diffraction limit, the minimum resolvable separation is δ=λ/(2NA)\delta = \lambda/(2\,\text{NA}). A student proposes that using a higher refractive-index immersion oil (increasing nn from 1.0 to 1.5 with the same objective lens geometry, so α\alpha is unchanged) will improve resolution by a factor of 1.5. A second student argues that the improvement is less than 1.5 because increasing nn also increases the optical path length, which effectively increases the wavelength seen by the objective. Which student is correct?

  1. The first student is correct in conclusion and reasoning. The wavelength relevant to the Abbe limit is the free-space wavelength λ0\lambda_0, not the in-medium wavelength, so δ=λ0/(2nsinα)\delta = \lambda_0/(2\,n\sin\alpha). Increasing nn by 1.5 at fixed α\alpha decreases δ\delta by exactly 1.5, improving resolution by that factor.
  2. The second student is correct. Because the wavelength in the medium is λ=λ0/n\lambda = \lambda_0/n, the Abbe formula gives δ=λ0/(2nsinα)\delta = \lambda_0/(2\,n\sin\alpha), but the increased optical path length introduces a phase lag that partially offsets the resolution gain, reducing improvement to a factor of n1.22\sqrt{n} \approx 1.22.
  3. The first student's numerical conclusion is correct, but his physical reasoning is wrong. The Abbe formula uses the in-medium wavelength λ=λ0/n\lambda = \lambda_0/n, giving δ=λ0/(2nsinα)=λ0/(2NA)\delta = \lambda_0/(2\,n\sin\alpha) = \lambda_0/(2\,\text{NA}). The factor of nn appears through NA, not by holding wavelength fixed at λ0\lambda_0. Resolution improves by exactly 1.5×. (correct answer)
  4. Neither student is correct. Immersion oil changes both nn and α\alpha simultaneously via Snell's law at the coverslip interface, so the effective NA is not simply nsinαn\sin\alpha. The resolution improvement can be greater or less than 1.5 depending on the specific coverslip and objective geometry.
Explanation: When tackling resolution questions in wave optics, always trace where each variable comes from physically before plugging into a formula. The Abbe diffraction limit is derived by considering interference of waves inside the medium between the object and objective. The relevant wavelength is the in-medium wavelength λ=λ0/n\lambda = \lambda_0/n, because that governs the spatial period of the interference pattern. Substituting into the Abbe formula gives δ=λ/(2sinα)=(λ0/n)/(2sinα)=λ0/(2nsinα)=λ0/(2NA)\delta = \lambda/(2\sin\alpha) = (\lambda_0/n)/(2\sin\alpha) = \lambda_0/(2\,n\sin\alpha) = \lambda_0/(2\,\text{NA}). So the factor of nn enters through NA — not by treating λ0\lambda_0 as the relevant wavelength. Increasing nn from 1.0 to 1.5 at fixed α\alpha scales NA by 1.5, halving δ\delta by that exact factor. The first student reaches the right numerical answer (1.5× improvement), but for the wrong reason — he claims λ0\lambda_0 is the relevant wavelength, which misrepresents the physics. This makes C correct. A is wrong because it endorses the first student's flawed reasoning: the free-space wavelength is not what appears in the Abbe derivation; the in-medium wavelength is. The conclusion happens to be numerically correct, but the justification is not. B is wrong on two counts: the second student's claim that increased optical path length "partially offsets" the gain has no physical basis in the Abbe framework, and the invented n\sqrt{n} factor appears nowhere in the theory. D is wrong because standard immersion objectives are designed so that α\alpha remains effectively fixed when switching immersion media; Snell's law is already accounted for in the optical design. Study tip: On optics questions, always ask "which wavelength governs this phenomenon — in-medium or free-space?" The answer depends on where the interference occurs.

Question 14

The Sparrow criterion for resolving two point sources states that two sources are just resolved when the combined intensity distribution has a flat top — i.e., the second derivative of total intensity at the midpoint equals zero. For two incoherent point sources of equal intensity imaged through a circular aperture, how does the minimum resolvable angular separation θS\theta_S (Sparrow) compare to the Rayleigh criterion θR=1.22λ/D\theta_R = 1.22\lambda/D?

  1. θS0.85θR\theta_S \approx 0.85\, \theta_R, because the Sparrow criterion requires less separation than Rayleigh — the dip in intensity between the two peaks need not reach any specific depth, so sources can be closer than the Rayleigh limit and still be declared resolved. (correct answer)
  2. θS=θR\theta_S = \theta_R exactly, because both criteria locate the point at which the overlap of the two Airy disks produces a detectable feature, and the flat-top condition coincides with the first zero of the Airy pattern of each source.
  3. θS1.22θR\theta_S \approx 1.22\, \theta_R, because the Sparrow criterion is more conservative than Rayleigh — requiring a flat top demands more separation between sources to eliminate any dip, effectively doubling the minimum separation relative to Rayleigh.
  4. θS0.5θR\theta_S \approx 0.5\, \theta_R, because the Sparrow criterion only requires the midpoint intensity to equal the peak intensity, which occurs when the sources are separated by exactly half the Rayleigh distance, making it far more permissive than any other criterion.
Explanation: When comparing resolution criteria, think about what each one demands from the intensity profile. The Rayleigh criterion requires the intensity maximum of one Airy disk to fall exactly on the first zero of the other, producing a modest ~26% dip between the two peaks. The Sparrow criterion is fundamentally more permissive: it asks only that the combined intensity profile shows a flat top at the midpoint — meaning the second derivative of total intensity equals zero there. No dip is required at all. This means two sources can be brought closer together than the Rayleigh limit before the Sparrow condition is triggered. Numerically, for two incoherent point sources imaged through a circular aperture, the Sparrow limit works out to approximately θS0.85θR\theta_S \approx 0.85\,\theta_R. Answer A is correct: the Sparrow criterion is less demanding (more permissive) because it declares sources resolved the moment any central feature — even just a flattening — disappears, rather than requiring a measurable valley. Answer B is wrong because the flat-top condition does not coincide with the first zero of the Airy pattern — that's the Rayleigh criterion's defining feature, not Sparrow's. Answer C inverts the logic entirely: requiring a flat top is less restrictive than requiring a dip, so the Sparrow limit is smaller than Rayleigh, not larger. Answer D confuses "flat top" with "equal midpoint and peak intensities at half the Rayleigh separation" — the actual geometry gives ~0.85, not 0.5, and the reasoning about what triggers the criterion is flawed. A useful mnemonic: Sparrow < Rayleigh < Dawes in terms of minimum resolvable separation — each successive criterion is stricter. When a question names a criterion, ask yourself whether it requires a dip, a zero, or just a flat profile.

Question 15

A laser of wavelength λ\lambda passes through a circular aperture of diameter DD and illuminates a screen at distance LL. An observer notes that the radius of the central Airy disk on the screen is rr. The observer then submerges the entire apparatus in a liquid of refractive index n>1n > 1 (the same laser operates at the same frequency). Which of the following correctly describes what happens to the radius rr of the central Airy disk and the angular resolution θR\theta_R of the aperture?

  1. θR\theta_R decreases by a factor of nn (angular resolution improves), but rr remains unchanged because the physical distance LL also effectively decreases by nn in the medium, and the two effects cancel.
  2. Both rr and θR\theta_R decrease by a factor of nn, because the wavelength in the medium is λ/n\lambda/n, which reduces both the diffraction angle and the physical size of the Airy disk on the screen. (correct answer)
  3. Neither rr nor θR\theta_R changes, because while the wavelength decreases by nn, the speed of light also decreases by nn, and the Rayleigh criterion depends on frequency (which is unchanged), not wavelength.
  4. rr decreases by a factor of nn because the reduced wavelength shrinks the diffraction pattern, but θR\theta_R remains the same because angular resolution is a geometric property of the aperture that does not depend on the medium's refractive index.
Explanation: Whenever you see a diffraction question involving a medium with refractive index nn, your first move should be to identify how the wavelength changes — because wavelength, not frequency, governs diffraction. When light enters a medium of refractive index nn, its frequency stays constant (it's set by the source), but its wavelength shrinks to λn=λ/n\lambda_n = \lambda/n. The Rayleigh criterion for angular resolution is θR=1.22λ/D\theta_R = 1.22\,\lambda/D, so substituting the new wavelength gives θR=1.22λ/(nD)\theta_R' = 1.22\,\lambda/(nD) — a factor of nn smaller. Since the screen is still physically at distance LL, the Airy disk radius is r=θRL=1.22λL/(nD)r' = \theta_R' \cdot L = 1.22\,\lambda L/(nD), also reduced by nn. Both quantities shrink together, confirming B is correct. A is wrong because it invents a fictitious "effective decrease in L." The physical distance to the screen doesn't change; only the wavelength does, so there is no cancellation. C is the most tempting trap — it sounds sophisticated to say frequency is unchanged — but diffraction is a wave-interference phenomenon that depends explicitly on wavelength, not frequency. Plugging frequency into the Rayleigh formula would give you the wrong units entirely. D gets the radius right but incorrectly claims θR\theta_R is purely geometric. Angular resolution directly involves λ/D\lambda/D; the medium absolutely affects it. Your study tip: always separate what changes (wavelength) from what doesn't (frequency, physical geometry) when a wave crosses into a new medium. Diffraction formulas use λ\lambda — substitute λ/n\lambda/n immediately and carry it through every quantity.