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Learning Objectives

By the end of this chapter, you should be able to:

Introduction

In 1818 the French Academy of Sciences held a prize competition on the nature of light. Augustin-Jean Fresnel submitted a wave theory. Siméon Denis Poisson, a member of the judging committee and a convinced supporter of Newton’s particle theory, worked through Fresnel’s mathematics and triumphantly produced what he took to be its refutation: if Fresnel were right, then the shadow of a small circular disk, illuminated by a point source, would have a bright spot at its exact center — light would diffract around the rim, arrive at the axis having traveled equal distances from every point of that rim, and interfere constructively. The prediction was patently ridiculous.

A member of that committee, François Arago, went and looked. The spot was there.

That bright point — now called the Poisson spot, or the Arago spot, depending on whose role in the story one prefers to emphasize — is a fair emblem for this chapter. Diffraction is what waves do when they encounter an obstacle or a finite aperture: they bend into the geometric shadow, and they interfere with themselves in the process, producing patterns of light and dark that no ray-tracing argument can generate.

Chapter 4 worked with idealized slits: point-like Huygens sources, infinitesimally narrow, contributing one wavelet apiece. A real slit has a finite width aa, and every point across that width emits a wavelet. Summing those contributions is the whole subject of this chapter. Three results follow, in increasing order of consequence. First, a single slit, all by itself, produces a pattern of bright and dark bands. Second, real multiple-slit devices — above all the diffraction grating — combine the sharp interference maxima of Chapter 4 with a diffraction envelope that decides how bright each of those maxima actually is. Third, and most importantly, because every real optical instrument gathers light through an aperture of finite size, diffraction sets an absolute limit on the fineness of detail any instrument can resolve — a limit that no improvement in polishing, alignment, or manufacture can evade, because it is imposed by the wavelength of light itself.

5.1Diffraction Basics and the Single Slit

Diffraction Versus Interference: A Note on Words

It is worth settling a piece of vocabulary that causes more confusion than it should.

There is no physical distinction between interference and diffraction. Both are the same thing: coherent waves from different places arriving at a common point and adding as fields. The words differ only in bookkeeping convention. When the sources are a small, discrete set — two slits, five slits — the custom is to say interference and to write a sum. When the sources form a continuum across an aperture, the custom is to say diffraction and to write an integral. Richard Feynman put it bluntly: “no one has ever been able to define the difference between interference and diffraction satisfactorily. It is just a question of usage, and there is no specific, important physical difference between them.”

The reason the distinction survives is practical. In a real double slit there are two length scales — the slit separation dd and the slit width aa, with d>ad > a — and they produce structure on two very different angular scales. Calling the fine structure “interference” and the coarse envelope “diffraction” is a convenient way to keep track of which is which. That is all it is.

The Huygens–Fresnel Principle

Fresnel’s contribution was to make Huygens’s construction quantitative. Where Huygens drew an envelope of wavelets, Fresnel insisted on adding the wavelets as waves, with their phases, and then squaring the result to get an intensity. Stated for an aperture:

Every point of an open aperture acts as a source of secondary wavelets of equal amplitude and of the same phase as the incoming wave at that point. The field at any observation point is the sum, over the whole aperture, of these wavelets, each with the phase it has accumulated on its journey.

This Huygens–Fresnel principle reproduces the results of Chapter 4 when the aperture is a set of very narrow slits, and everything in this chapter when it is not. The sum becomes an integral, but the physics — add fields, account for phase, then square — is unchanged.

Near Field and Far Field

Whether the sum is easy or hard depends on the geometry, and the distinction matters enough to have names.

If the screen is far enough away that the rays converging on any observation point are effectively parallel, the phase of each wavelet is a linear function of its position in the aperture, and the integral is elementary. This is Fraunhofer diffraction, or far-field diffraction, and it is the case treated throughout this chapter.

If the screen is close, the rays are noticeably non-parallel, the phase varies quadratically across the aperture, and the pattern depends in a complicated way on distance. This is Fresnel diffraction, or near-field diffraction. The Poisson spot of the introduction is a Fresnel phenomenon; so are the fine bright and dark bands you can see just inside the edge of a sharp shadow cast by a small bright source.

The dividing line is set by the Fresnel number

F=a2Lλ,F = \frac{a^2}{L\lambda},

where aa is the aperture size and LL the aperture-to-screen distance. Fraunhofer diffraction applies when F1F \ll 1; Fresnel diffraction when F1F \gtrsim 1. For a 0.05 mm0.05\ \text{mm} slit, 550 nm550\ \text{nm} light, and a screen 2 m2\ \text{m} away, F=(5×105 m)2/[(2 m)(5.5×107 m)]=2×103F = (5\times10^{-5}\ \text{m})^2/[(2\ \text{m})(5.5\times10^{-7}\ \text{m})] = 2\times10^{-3}, comfortably in the far field. Conveniently, a lens converts the far field into something you can put on a bench: any lens placed after the aperture brings the parallel bundles to a focus in its focal plane, so the Fraunhofer pattern appears there no matter how short the bench.

Single-Slit Diffraction

Consider a slit of width aa illuminated by a plane wave of wavelength λ\lambda, with a distant screen. The clever step, due to Fresnel, is not to attempt the whole sum at once but to ask a narrower question: in which directions does everything cancel?

Divide the slit conceptually into two equal halves, each of width a/2a/2, as in Figure 5.1(a). Pair up the topmost point of the upper half with the topmost point of the lower half; they are a distance a/2a/2 apart. Pair the second point of the upper half with the second point of the lower half; also a/2a/2 apart. Every point in the upper half has a partner in the lower half exactly a/2a/2 below it. If the light heading off at angle θ\theta from each pair is exactly out of phase — path difference λ/2\lambda/2 — then every pair cancels, and so does the whole slit:

a2sinθ=λ2asinθ=λ.\frac{a}{2}\sin\theta = \frac{\lambda}{2} \qquad\Longrightarrow\qquad a\sin\theta = \lambda .
Two panels showing a slit divided into two halves and into four quarters, with a highlighted pair of source points separated by a over 2 and a over 4 and the extra path each pair accumulates.

Figure 5.1:Canceling the slit against itself. Dividing the slit into two strips pairs each point with a partner a/2a/2 away; when those pairs are a half wavelength out of step, the whole slit cancels, giving asinθ=λa\sin\theta = \lambda. Dividing into four strips pairs points a/4a/4 apart and gives asinθ=2λa\sin\theta = 2\lambda, and so on. Original schematic generated with matplotlib; see scripts/figures/.

Repeat the argument with four strips (Figure 5.1(b)): now partners are a/4a/4 apart, each pair cancels when (a/4)sinθ=λ/2(a/4)\sin\theta = \lambda/2, and the whole slit cancels at asinθ=2λa\sin\theta = 2\lambda. With 2m2m strips the condition is asinθ=mλa\sin\theta = m\lambda. The complete set of single-slit minima is therefore

asinθ=mλ,m=±1,±2,±3,(diffraction minima).a\sin\theta = m\lambda, \qquad m = \pm1, \pm2, \pm3, \ldots \qquad (\text{diffraction minima}).

Two things about this formula regularly trip people up, and both are worth stating explicitly.

It locates minima, not maxima. Compare with the double-slit condition dsinθ=mλd\sin\theta = m\lambda, which locates maxima. The two formulas look almost identical and mean opposite things. The distinction is not a convention: it comes from the fact that the pairing argument can only ever demonstrate cancellation.

m=0m = 0 is excluded. At θ=0\theta = 0 every point of the slit is in phase with every other, so the wavelets add rather than cancel — there is nothing to pair against. The center of the pattern is a broad, bright central maximum, not a minimum. Formally, the pairing argument demands a path difference of λ/2\lambda/2 within each pair, and θ=0\theta = 0 supplies a path difference of zero.

The Width of the Central Maximum

The central maximum is bounded by the first minima on either side, at sinθ=±λ/a\sin\theta = \pm\lambda/a. Its angular half-width is therefore

θ1=arcsinλaλa(for λa),\theta_1 = \arcsin\frac{\lambda}{a} \approx \frac{\lambda}{a} \quad (\text{for } \lambda \ll a),

exactly the λ/a\lambda/a scaling that the dimensional argument of Chapter 4 demanded. Note that in sinθ\sin\theta the central maximum runs from λ/a-\lambda/a to +λ/a+\lambda/a, while every other maximum spans only λ/a\lambda/a: the central peak is twice as wide as the rest, in addition to being far brighter.

The most important qualitative consequence is that narrowing the slit widens the pattern, as Figure 5.2 shows.

Four stacked intensity curves for slits of width one, two, five and twenty wavelengths, showing the diffraction pattern narrowing dramatically as the slit widens.

Figure 5.2:Single-slit patterns for four slit widths. The central maximum spans sinθ=±λ/a\sin\theta = \pm\lambda/a, so it narrows as the slit widens: a slit 20λ20\lambda across concentrates the light into a beam, while a slit only 1λ1\lambda across has no minimum at all and radiates almost like a single point source. Generated with matplotlib; see scripts/figures/.

This is the opposite of the naive expectation that a narrower opening should produce a narrower beam, and it is a genuinely wave-like signature. It also gives the correct picture of the limiting case: when aλa \le \lambda, the condition sinθ=λ/a1\sin\theta = \lambda/a \ge 1 has no solution, there are no minima anywhere, and the slit radiates into the entire forward hemisphere — behaving, exactly as Chapter 4 assumed, like a single Huygens point source. That is the justification, after the fact, for treating the slits of the double-slit experiment as points.

The inverse relationship between the aperture and its pattern is worth seeing rather than reading about, and Figure 5.3 shows the two side by side: the aperture on the left, the far-field pattern it produces on the right, with the aperture’s size and the wavelength both on sliders. Shrinking the opening spreads the pattern, and by exactly the ratio λ/a\lambda/a derived above. Two further controls make the point sharper than a single slit can. Squashing the round aperture into an ellipse produces an elliptical pattern elongated along the other axis, so the reciprocity holds direction by direction and not just on average; and the non-circular shapes on offer produce patterns of matching symmetry — an anticipation of the circular-aperture section below, where a round hole is found to give rings rather than a row of bands, and of the crystal lattices at the end of the chapter, where a periodic array of holes gives a periodic array of spots.

Screenshot of the Wave Interference simulation

Figure 5.3:An aperture and the far-field diffraction pattern it produces, with aperture size, shape, and wavelength adjustable. Everything narrow in the aperture is wide in the pattern, and vice versa — the θ1λ/a\theta_1 \approx \lambda/a scaling of this section, seen whole rather than one angle at a time.

Interactive simulation: Wave Interference

Worked Example: Width of the Central Maximum

A slit of width a=0.0400 mma = 0.0400\ \text{mm} is illuminated with λ=580 nm\lambda = 580\ \text{nm} light, and the pattern is observed on a screen L=2.00 mL = 2.00\ \text{m} away. Find the width of the central maximum.

The first minima are at

sinθ1=λa=580×109 m4.00×105 m=0.0145,\sin\theta_1 = \frac{\lambda}{a} = \frac{580\times10^{-9}\ \text{m}}{4.00\times10^{-5}\ \text{m}} = 0.0145,

so θ1=0.0145 rad=0.831°\theta_1 = 0.0145\ \text{rad} = 0.831° (the small-angle approximation is excellent here). On the screen,

y1=Ltanθ1Lθ1=(2.00 m)(0.0145 rad)=0.0290 m,y_1 = L\tan\theta_1 \approx L\theta_1 = (2.00\ \text{m})(0.0145\ \text{rad}) = 0.0290\ \text{m},

and the central maximum, running from y1-y_1 to +y1+y_1, has full width

w=2y1=5.80 cm.w = 2y_1 = 5.80\ \text{cm}.

Check the trend: halving the slit width to 0.0200 mm0.0200\ \text{mm} would double this to 11.6 cm11.6\ \text{cm}.

Worked Example: A Slit Too Narrow to Have Minima

At what slit width does the first minimum disappear entirely, for λ=580 nm\lambda = 580\ \text{nm}?

The first minimum requires sinθ1=λ/a1\sin\theta_1 = \lambda/a \le 1, so it exists only if aλ=580 nma \ge \lambda = 580\ \text{nm}. A slit narrower than one wavelength produces a smooth, minimum-free spread of light across the whole forward direction. Slits this narrow are difficult to make and transmit very little light, which is why the textbook idealization of a “point source slit” is easier to draw than to build — and why real double-slit experiments always show the envelope discussed below.

5.2Intensity Patterns and the Double Slit

Intensity in Single-Slit Diffraction

The pairing argument gives the zeros; getting the full curve requires actually doing the sum. The phasor picture of Chapter 4 makes this almost graphical.

Divide the slit into NN narrow strips and let NN\to\infty. Each strip contributes a tiny phasor of the same length, and each is rotated slightly relative to its neighbor, because it sits slightly farther along the slit and so contributes a slightly different path. Let β\beta be the total phase difference between the wavelet from one edge of the slit and the wavelet from the other:

β2πλasinθ.\beta \equiv \frac{2\pi}{\lambda}\,a\sin\theta .

The chain of tiny phasors therefore turns through a total angle β\beta from beginning to end. A chain of equal segments turning at a uniform rate is an arc of a circle, and the resultant field is its chord (Figure 5.4).

Three panels showing a chain of small phasors, straight for zero phase, curled into a semicircular arc, and closed into a full circle with zero resultant.

Figure 5.4:The single-slit phasor construction. The wavelets from across the slit form a chain of equal phasors turning through a total angle β\beta. At θ=0\theta = 0 the chain is straight and the resultant equals the full arc length. As θ\theta grows the chain curls and the chord falls behind the arc. At β=2π\beta = 2\pi the chain closes into a circle and the resultant vanishes — the first minimum, asinθ=λa\sin\theta = \lambda. Original schematic generated with matplotlib; see scripts/figures/.

Everything follows from the geometry of a circular arc. Let the arc length be E0E_0 (this is the resultant at θ=0\theta = 0, when the chain is straight). An arc of length E0E_0 subtending angle β\beta has radius R=E0/βR = E_0/\beta, and the chord across it is 2Rsin(β/2)2R\sin(\beta/2). So

E=2E0βsinβ2=E0sin(β/2)β/2,E = 2\frac{E_0}{\beta}\sin\frac{\beta}{2} = E_0\,\frac{\sin(\beta/2)}{\beta/2},

and squaring gives the single-slit intensity pattern

I(θ)=I0[sin(β/2)β/2]2,β=2πλasinθ.I(\theta) = I_0\left[\frac{\sin(\beta/2)}{\beta/2}\right]^2, \qquad \beta = \frac{2\pi}{\lambda}a\sin\theta .

The quantity in brackets is sinc(β/2)\mathrm{sinc}(\beta/2), where sinc(x)sinx/x\mathrm{sinc}(x) \equiv \sin x / x, so the pattern is often written I=I0sinc2(β/2)I = I_0\,\mathrm{sinc}^2(\beta/2).

Three checks confirm this is the right answer:

The sinc-squared single-slit intensity curve with side lobes shown at twenty times magnification and labeled 4.7, 1.6 and 0.8 percent, with the corresponding fringe pattern strip above.

Figure 5.5:Single-slit diffraction intensity. The central maximum is twice as wide as the side lobes and vastly brighter — the first side lobe reaches only 4.7%4.7\% of the peak, so it is shown here magnified 20×20\times. The strip above shows the pattern as it appears on a screen, with faint bands brightened so they reproduce. Generated with matplotlib; see scripts/figures/.

The Secondary Maxima

Where are the maxima between the zeros? Setting dI/dβ=0\mathrm{d}I/\mathrm{d}\beta = 0 gives the transcendental condition tan(β/2)=β/2\tan(\beta/2) = \beta/2, which has no closed-form solution. Solving numerically puts the secondary maxima at

β2=1.4303π, 2.4590π, 3.4709π, \frac{\beta}{2} = 1.4303\pi,\ 2.4590\pi,\ 3.4709\pi,\ \ldots

slightly inside the naive halfway positions 1.5π1.5\pi, 2.5π2.5\pi, 3.5π3.5\pi — pulled toward the center because the envelope is falling. Relative to the central peak, the first three secondary maxima reach only

4.7%,1.6%,0.83%4.7\%, \qquad 1.6\%, \qquad 0.83\%

of I0I_0, falling off roughly as 1/m21/m^2. This is why a single-slit pattern does not look like a row of comparable fringes at all: it looks like one dominant bright band, flanked by faint ripples that most observers overlook entirely. It is also why Figure 5.5 has to magnify them 20×20\times before they are visible on the page.

Double-Slit Diffraction: Both Effects Together

Now put the two chapters together. A real double slit consists of two openings, each of finite width aa, whose centers are separated by d>ad > a. Both effects operate at once, and — because the field from each slit is the single-slit field, and the two slits then interfere — the intensities simply multiply:

I(θ)=I0cos2 ⁣(πdsinθλ)interference, set by d  [sin(β/2)β/2]2diffraction envelope, set by a,β=2πλasinθ.I(\theta) = I_0\underbrace{\cos^2\!\left(\frac{\pi d\sin\theta}{\lambda}\right)}_{\text{interference, set by }d}\;\underbrace{\left[\frac{\sin(\beta/2)}{\beta/2}\right]^2}_{\text{diffraction envelope, set by }a}, \qquad \beta = \frac{2\pi}{\lambda}a\sin\theta .

Since d>ad > a, the cos2\cos^2 factor oscillates rapidly and the sinc2\mathrm{sinc}^2 factor varies slowly: fine fringes under a broad envelope, as in Figure 5.6.

Closely spaced interference fringes modulated by a broad single-slit envelope, with markers at the fifth and tenth orders showing the missing orders.

Figure 5.6:A real double slit with d=5ad = 5a. The rapid cos2\cos^2 fringes are set by the slit separation dd; the dashed envelope is the single-slit sinc2\mathrm{sinc}^2 pattern set by the slit width aa. Orders m=±5m = \pm5 and ±10\pm10 vanish because they coincide with zeros of the envelope. Generated with matplotlib; see scripts/figures/.

Missing Orders

The striking feature of Figure 5.6 is that some interference maxima are simply absent. An interference maximum at dsinθ=mλd\sin\theta = m\lambda is wiped out if a diffraction minimum, asinθ=mλa\sin\theta = m'\lambda, falls at the same angle. Dividing one condition by the other, this happens when

mm=da,\frac{m}{m'} = \frac{d}{a},

that is, whenever m(a/d)m\,(a/d) is an integer. If d/ad/a is itself an integer, every (d/a)(d/a)-th order is missing — for d=5ad = 5a the missing orders are m=±5,±10,±15,m = \pm5, \pm10, \pm15,\ldots, exactly as in the figure. If d/ad/a is a ratio of small integers, say d/a=5/2d/a = 5/2, orders that are multiples of 5 still vanish but nothing else does. If d/ad/a is irrational, no order is exactly missing, though those near an envelope zero are suppressed almost to nothing.

Missing orders are a measurement, not a curiosity. Counting how many interference fringes fit inside the central diffraction maximum can reveal d/ad/a, without measuring either dd or aa: the central envelope spans sinθ<λ/a|\sin\theta| < \lambda/a and fringes are spaced by λ/d\lambda/d in sinθ\sin\theta. When d/a=qd/a=q is an integer, the visible orders are mq1|m|\le q-1, giving 2q12q-1 bright fringes inside the central envelope; the orders at m=q|m|=q are missing at its edges. For a noninteger ratio, use the integer orders satisfying m<d/a|m|<d/a instead; the count then gives the corresponding integer bound, while the missing-order pattern can identify a rational ratio. Looking at a laboratory double-slit pattern and counting bright fringes between the first envelope zeros is therefore a genuine measurement of a ratio of two dimensions far too small to measure with a ruler.

Worked Example: Reading a Double-Slit Pattern

A double slit has slit width a=0.0200 mma = 0.0200\ \text{mm} and separation d=0.100 mmd = 0.100\ \text{mm}, illuminated at λ=633 nm\lambda = 633\ \text{nm}. (a) Which orders are missing? (b) How many bright fringes lie inside the central diffraction maximum? (c) Find the angular width of the central envelope.

(a) d/a=(0.100 mm)/(0.0200 mm)=5d/a = (0.100\ \text{mm})/(0.0200\ \text{mm}) = 5, an integer, so orders m=±5,±10,±15,m = \pm5, \pm10, \pm15,\ldots are missing.

(b) The central envelope runs from sinθ=λ/a\sin\theta = -\lambda/a to +λ/a+\lambda/a; the fringes at its edges are the missing m=±5m = \pm5. The visible orders inside are m=4,,+4m = -4,\ldots,+4: nine bright fringes, of which the central one is brightest.

(c) sinθenv=λ/a=(633×109 m)/(2.00×105 m)=0.0317\sin\theta_{\text{env}} = \lambda/a = (633\times10^{-9}\ \text{m})/(2.00\times10^{-5}\ \text{m}) = 0.0317, so the envelope’s first zeros are at θ=±1.81°\theta = \pm1.81°, giving a full angular width of 3.63°3.63°. On a screen 2.00 m2.00\ \text{m} away that is a central band 12.7 cm12.7\ \text{cm} wide, containing nine fringes spaced λL/d=12.7 mm\lambda L/d = 12.7\ \text{mm} apart — a comfortable laboratory pattern.

5.3Diffraction Gratings

A diffraction grating is the NN-slit device of Chapter 4 built for real: thousands of parallel slits per millimeter, ruled onto glass (a transmission grating) or onto a reflective surface (a reflection grating, which is what most modern spectrometers use). A compact disc is an accidental reflection grating, its data tracks spaced 1.6 μm1.6\ \mu\text{m} apart; a DVD’s tracks are 0.74 μm0.74\ \mu\text{m} apart, which is why it throws colors more widely.

Everything derived for NN ideal slits carries over. The principal maxima satisfy the grating equation

dsinθ=mλ,m=0,±1,±2,d\sin\theta = m\lambda, \qquad m = 0, \pm1, \pm2,\ldots

with dd the spacing between adjacent rulings; their width scales as 1/N1/N and their peak intensity as N2N^2. What is new is only that NN is now enormous — a 1 cm1\ \text{cm} beam on a grating with 600 lines per millimeter illuminates 6000 lines at once — so the maxima are not fringes but needle-sharp spectral lines. And of course the finite width of each opening imposes a diffraction envelope, exactly as for the double slit, so some orders are weak or missing. (Precision gratings are blazed: each groove is cut at an angle chosen to steer the envelope’s peak into a chosen order, so that most of the light ends up where it is wanted rather than in the useless m=0m = 0 direction.)

Dispersion

Because the diffraction angle depends on λ\lambda, a grating spreads white light into a spectrum — one spectrum per order, on each side of the center. Differentiating the grating equation gives the angular dispersion

dθdλ=mdcosθ,\frac{\mathrm{d}\theta}{\mathrm{d}\lambda} = \frac{m}{d\cos\theta},

so the spectrum spreads out more in higher orders and with finer rulings. It also shows that the orders eventually overlap: the red end of order mm can fall on top of the blue end of order m+1m+1, which is why spectrometers often place a coarse filter in front of the detector to isolate a single order.

Since sinθ1|\sin\theta| \le 1, the mathematical upper bound on the order is mmax=d/λm_{\max} = \lfloor d/\lambda\rfloor — a grating so fine that d<λd < \lambda produces no spectrum at all beyond m=0m = 0. If d/λd/\lambda is exactly an integer, that limiting order is at grazing angle (θ=90\theta=90^\circ) and is not usable in an ordinary detector geometry.

Resolving Power

The property that makes gratings scientific instruments rather than ornaments is their resolving power: the ability to display two nearly equal wavelengths as two separate lines rather than one blur.

Adopt the Rayleigh criterion — two lines are just resolved when the principal maximum of one falls on the first zero of the other. The principal maximum for wavelength λ\lambda in order mm sits at dsinθ=mλd\sin\theta = m\lambda, and its first zero is λ/(Ndcosθ)\lambda/(Nd\cos\theta) away in angle. The line at λ+Δλ\lambda + \Delta\lambda sits mΔλ/(dcosθ)m\,\Delta\lambda/(d\cos\theta) away. Setting these equal,

mΔλdcosθ=λNdcosθ  RλΔλ=mN  \frac{m\,\Delta\lambda}{d\cos\theta} = \frac{\lambda}{Nd\cos\theta} \qquad\Longrightarrow\qquad \boxed{\;R \equiv \frac{\lambda}{\Delta\lambda} = mN\;}

Figure 5.7 shows the criterion in action. The resolving power depends only on the order and on the number of lines actually illuminated. Two consequences are worth noting. First, resolving power improves with the illuminated width of the grating, not with the total number of lines ruled on it; underfilling a grating with a narrow beam throws resolution away. Second, working in second or third order doubles or triples the resolution, at the cost of dimmer lines and increased risk of overlapping orders — a trade every spectroscopist makes.

Three stacked panels showing the sodium doublet recorded with 300, 982 and 3000 illuminated grating lines, going from a single blur to two clearly separated peaks.

Figure 5.7:Resolving the sodium doublet (589.0 and 589.6 nm) in first order. With too few illuminated lines the two principal maxima are broader than their separation and merge into one feature. At N=982N = 982, R=mNR = mN equals λ/Δλ\lambda/\Delta\lambda and the peak of one line falls on the first zero of the other — the Rayleigh criterion. With N=3000N = 3000 the lines are cleanly separated. Generated with matplotlib; see scripts/figures/.

Worked Example: Resolving the Sodium Doublet

The sodium doublet — the pair of yellow lines responsible for the color of a sodium street lamp — consists of lines at λ1=589.0 nm\lambda_1 = 589.0\ \text{nm} and λ2=589.6 nm\lambda_2 = 589.6\ \text{nm}. How many grating lines must be illuminated to resolve them in first order?

The required resolving power is

R=λΔλ=589.0 nm0.6 nm=982.R = \frac{\lambda}{\Delta\lambda} = \frac{589.0\ \text{nm}}{0.6\ \text{nm}} = 982 .

From R=mNR = mN with m=1m = 1,

N=Rm=982 lines.N = \frac{R}{m} = 982\ \text{lines}.

On a grating with 600 lines per millimeter this needs a beam only 1.64 mm1.64\ \text{mm} wide — trivially met by any laboratory setup, which is why the sodium doublet is a standard first-week demonstration. In second order only 491 lines would be needed. By contrast, resolving the hyperfine structure within one of those lines requires a much larger resolving power than resolving the doublet — far beyond this simple demonstration and typically measured with specialized spectroscopic methods instead.

Worked Example: A Grating Spectrum

A transmission grating has 5000 lines per centimeter. (a) Find the line spacing. (b) Find the angle of the first-order maximum for λ=500 nm\lambda = 500\ \text{nm}. (c) Find the highest observable order. (d) Find the angular separation between the 486 nm486\ \text{nm} and 656 nm656\ \text{nm} hydrogen lines in first order.

(a) d=(1 cm)/5000=2.00×106 m=2.00 μmd = (1\ \text{cm})/5000 = 2.00\times10^{-6}\ \text{m} = 2.00\ \mu\text{m}.

(b) sinθ1=λ/d=(500×109 m)/(2.00×106 m)=0.250\sin\theta_1 = \lambda/d = (500\times10^{-9}\ \text{m})/(2.00\times10^{-6}\ \text{m}) = 0.250, so θ1=14.5°\theta_1 = 14.5°.

(c) mmax=d/λ=4.00=4m_{\max} = \lfloor d/\lambda\rfloor = \lfloor 4.00\rfloor = 4, but m=4m = 4 gives sinθ=1.00\sin\theta = 1.00 exactly — grazing emergence, unobservable in practice. The highest usable order is m=3m = 3, at θ=48.6°\theta = 48.6°.

(d) θ(486 nm)=arcsin(0.243)=14.06°\theta(486\ \text{nm}) = \arcsin(0.243) = 14.06° and θ(656 nm)=arcsin(0.328)=19.14°\theta(656\ \text{nm}) = \arcsin(0.328) = 19.14°, a separation of 5.08°5.08°. A grating spreads the visible spectrum over several degrees in first order — enough to project a spectrum across a wall.

5.4Resolution, Bragg Diffraction, and Holography

Circular Apertures and the Limits of Resolution

Every real optical instrument — a camera lens, a telescope mirror, a microscope objective, the pupil of the eye — collects light through a circular aperture of diameter DD. Its diffraction pattern is the circular analog of the single-slit pattern: a bright central disk, the Airy disk, surrounded by faint concentric rings.

The mathematics is harder than the slit case, because the integral runs over a disk rather than a line, and the answer involves a Bessel function rather than a sine. The structure of the result, however, is identical, differing only by a numerical factor that comes from the circular geometry: the first dark ring lies at

sinθmin=1.22λDθmin.\sin\theta_{\min} = 1.22\,\frac{\lambda}{D} \approx \theta_{\min}.

Compare this with λ/a\lambda/a for a slit. Nothing has changed except the 1.22 — which is, in fact, the first zero of the Bessel function J1J_1 divided by π\pi.

Where the factor 1.22 comes from

For a circular aperture of diameter DD, the far-field amplitude at angle θ\theta is proportional to the two-dimensional analog of the single-slit integral, evaluated over a disk instead of a line:

E(θ)2J1(kRsinθ)kRsinθ,k=2πλ,R=D2,E(\theta) \propto \frac{2J_1(kR\sin\theta)}{kR\sin\theta}, \qquad k = \frac{2\pi}{\lambda},\quad R = \frac{D}{2},

where J1J_1 is the Bessel function of the first kind, order one — the circular-geometry replacement for the sinx/x\sin x/x that came from integrating across a slit. This combination plays exactly the role sinc(β/2)\mathrm{sinc}(\beta/2) played in the single-slit case: it equals 1 at zero argument, giving the central Airy peak, and has its first zero at the first zero of J1J_1 itself,

kRsinθmin=3.8317kR\sin\theta_{\min} = 3.8317\ldots

Substituting k=2π/λk = 2\pi/\lambda and R=D/2R = D/2 and solving for sinθmin\sin\theta_{\min},

sinθmin=3.8317πλD=1.2197λD1.22λD.\sin\theta_{\min} = \frac{3.8317}{\pi}\,\frac{\lambda}{D} = 1.2197\,\frac{\lambda}{D} \approx 1.22\,\frac{\lambda}{D}.

The extra factor, compared with a slit’s plain λ/D\lambda/D, is a purely geometric consequence of integrating over a disk rather than a line. No new physics enters — only a different shape of aperture.

The Rayleigh Criterion

Two distant point sources — two stars, or two features on a microscope slide — each produce their own Airy pattern in the image. If the sources are close together in angle, the two patterns overlap and merge into a single blob. Lord Rayleigh proposed a workable convention for where to draw the line: two sources are just resolved when the center of one Airy disk falls on the first dark ring of the other. That is, when their angular separation equals

θmin=1.22λD(Rayleigh criterion).\theta_{\min} = 1.22\,\frac{\lambda}{D} \qquad (\textbf{Rayleigh criterion}).

Figure 5.8 shows what this looks like. At the criterion there is a shallow dip between the two peaks — about 26%26\% below the maxima. The criterion is a convention, not a law of nature: with a high signal-to-noise ratio and a known point-spread function, computational methods can do better, and some super-resolution fluorescence methods exploit temporal control or sparse emitters to distinguish features closer together than the Rayleigh separation. But as an estimate of what an instrument can do, it is excellent.

Three simulated images of two point sources separated by 0.5, 1.0 and 2.0 times the Rayleigh angle, with intensity cross-sections beneath each.

Figure 5.8:Two point sources imaged through a circular aperture, at separations of 0.5, 1.0, and 2.0 times θmin=1.22λ/D\theta_{\min} = 1.22\lambda/D, with intensity profiles beneath. At half the Rayleigh separation the pair is indistinguishable from a single elongated source; at the Rayleigh separation a shallow dip appears between the peaks; at twice it the two sources are unmistakable. Generated with matplotlib; see scripts/figures/.

The crucial thing about the Rayleigh criterion is its universality. It applies to every instrument with aperture DD, however perfectly made. It is not an engineering shortcoming to be designed away; it is a consequence of light having a wavelength and the instrument having an edge. The only levers available are λ\lambda and DD: use a shorter wavelength, or build a bigger aperture.

Both levers are pulled hard in practice. Telescopes get larger, and radio astronomers link dishes thousands of kilometers apart to synthesize an aperture the size of the Earth. Photolithography, which prints circuit features by projecting a mask onto a silicon wafer, has driven its light source from visible wavelengths down through deep ultraviolet to today’s extreme-ultraviolet at 13.5 nm13.5\ \text{nm} for exactly this reason. And electron microscopy takes the argument to its conclusion by abandoning light altogether in favor of electron matter waves whose wavelength (Chapter 7) can be a hundred thousand times shorter than visible light.

Worked Example: The Hubble Space Telescope

The Hubble Space Telescope has a primary mirror of diameter D=2.4 mD = 2.4\ \text{m}. (a) Estimate its diffraction-limited resolution at λ=550 nm\lambda = 550\ \text{nm}. (b) What is the smallest feature it could resolve on the Moon, 3.84×108 m3.84\times10^8\ \text{m} away?

(a)

θmin=1.22λD=1.22550×109 m2.4 m=2.80×107 rad=0.058 arcsec.\theta_{\min} = 1.22\,\frac{\lambda}{D} = 1.22\,\frac{550\times10^{-9}\ \text{m}}{2.4\ \text{m}} = 2.80\times10^{-7}\ \text{rad} = 0.058\ \text{arcsec}.

(b)

s=θmind=(2.80×107 rad)(3.84×108 m)=107 m.s = \theta_{\min}\,d = (2.80\times10^{-7}\ \text{rad})(3.84\times10^8\ \text{m}) = 107\ \text{m}.

Hubble could not photograph the Apollo landing sites; the largest hardware left there is a few meters across. The limitation is not the telescope’s quality but its aperture, and no amount of image processing changes the fact that the information never entered the instrument.

Worked Example: The Eye, and Why Ground Telescopes Are Different

(a) The pupil of the eye is about D=4.0 mmD = 4.0\ \text{mm} in ordinary lighting. Its diffraction limit at λ=550 nm\lambda = 550\ \text{nm} is

θmin=1.22550×109 m4.0×103 m=1.68×104 rad0.6 arcmin.\theta_{\min} = 1.22\,\frac{550\times10^{-9}\ \text{m}}{4.0\times10^{-3}\ \text{m}} = 1.68\times10^{-4}\ \text{rad} \approx 0.6\ \text{arcmin} .

At a reading distance of 25 cm25\ \text{cm} this corresponds to s=(1.68×104 rad)(0.25 m)=42 μms = (1.68\times10^{-4}\ \text{rad})(0.25\ \text{m}) = 42\ \mu\text{m} — about half the width of a human hair, and in reasonable agreement with measured visual acuity of about 1 arcmin. The eye is, remarkably, working close to its diffraction limit.

(b) Now apply the same formula to a 2.4 m2.4\ \text{m} telescope on the ground: θmin=0.058\theta_{\min} = 0.058 arcsec, the same as Hubble. Yet ground-based images at visible wavelengths are typically blurred to about 1 arcsec, a factor of 17 worse. The culprit is not diffraction but atmospheric seeing: turbulent cells of air, of order 10 cm10\ \text{cm} across, refract the incoming wavefront by slightly different amounts and scramble it. The effective aperture is set by the turbulence, not the mirror. Two responses are possible — put the telescope above the atmosphere, which is why Hubble exists, or measure the distortion hundreds of times a second and cancel it with a deformable mirror, which is adaptive optics, and which now lets large ground telescopes reach their diffraction limits in the infrared.

This example is worth keeping in mind whenever a diffraction limit is quoted: it is a ceiling on performance, not a promise of it.

X-Ray Diffraction and Bragg’s Law

Gratings work because their line spacing is comparable to the wavelength of the light. To probe the arrangement of atoms in a solid, spaced a few tenths of a nanometer apart, we would need a grating with that spacing — and nature supplies one, in the form of a crystal, provided we bring a wave with a matching wavelength. That means X-rays, with λ0.1 nm\lambda \sim 0.1\ \text{nm}.

Max von Laue proposed the experiment in 1912 and his collaborators Friedrich and Knipping performed it, obtaining a pattern of discrete spots from a copper sulfate crystal that established two things at once: that X-rays are waves, and that crystals are periodic arrays of atoms. Both had been conjectures until that afternoon.

W. H. Bragg and his son W. L. Bragg supplied the simple picture that made the technique usable, shown in Figure 5.9. Regard the crystal as a stack of parallel atomic planes separated by dd, and consider X-rays reflecting specularly from successive planes. By long-standing crystallographic convention, the angle θ\theta is measured from the plane itself, not from the normal — a trap for anyone importing habits from optics.

Two parallel X-rays reflecting from successive atomic planes in a crystal, with the extra path length of the lower ray marked as two segments each equal to d sine theta.

Figure 5.9:Bragg reflection. Two parallel X-rays strike successive atomic planes separated by dd. Relative to the wavefronts through AA, the ray reflecting from the lower plane travels two extra legs, each of length dsinθd\sin\theta. Constructive interference requires the total, 2dsinθ2d\sin\theta, to be a whole number of wavelengths. Original schematic generated with matplotlib; see scripts/figures/.

Ray 2 penetrates one layer deeper. Measured between the wavefronts through the point AA where ray 1 reflects, it travels two extra legs — one on the way in, one on the way out — each of length dsinθd\sin\theta. Constructive interference between rays reflected from successive planes therefore requires

nλ=2dsinθ(Bragg’s law),n=1,2,3,n\lambda = 2d\sin\theta \qquad (\textbf{Bragg's law}), \qquad n = 1, 2, 3, \ldots

The consequence is that a crystal reflects a given X-ray wavelength strongly only at particular angles. Rotate a crystal in a monochromatic X-ray beam and the detector sees nothing at all until an angle satisfying Bragg’s law comes up, at which point a sharp peak appears. Measuring the set of such angles, for a set of crystal orientations, determines the spacings and symmetry of the atomic planes.

This is X-ray crystallography, and its record is hard to overstate: the structures of table salt and diamond (the Braggs, 1913), of penicillin and vitamin B12_{12} (Dorothy Hodgkin), of DNA — the double helix inferred by Watson and Crick from the diffraction photographs taken by Rosalind Franklin and Raymond Gosling — and of hundreds of thousands of proteins since. Nearly everything we know about where atoms sit in condensed matter came through Bragg’s law.

The lattice on the other side of Bragg’s law is the subject of Figure 5.10. Changing the unit cell changes the set of atomic planes, their spacings dd, and therefore the angles at which reflections appear — including the aperiodic case, where the diffraction pattern is as sharp as a crystal’s but carries a symmetry no crystal can have.

Screenshot of the Crystal Lattice simulation

Figure 5.10:Crystal structure in five screens: the two-dimensional Bravais lattices, cubic unit cells, close packing, Miller indices, and aperiodic order. The Miller-index screen is the direct companion to Bragg’s law — it is where the planes of spacing dd come from.

Interactive simulation: Crystal Lattice

Worked Example: An Interplanar Spacing

X-rays of wavelength λ=0.154 nm\lambda = 0.154\ \text{nm} (the copper KαK_\alpha line, the workhorse of laboratory diffractometers) produce a first-order Bragg reflection at θ=22.5°\theta = 22.5°. Find the spacing of the reflecting planes, and find where the second-order reflection appears.

First order, n=1n = 1:

d=nλ2sinθ=0.154 nm2sin22.5°=0.154 nm2(0.3827)=0.201 nm,d = \frac{n\lambda}{2\sin\theta} = \frac{0.154\ \text{nm}}{2\sin 22.5°} = \frac{0.154\ \text{nm}}{2(0.3827)} = 0.201\ \text{nm},

a typical interatomic spacing. For n=2n = 2,

sinθ2=2λ2d=0.154 nm0.201 nm=0.766θ2=50.0°.\sin\theta_2 = \frac{2\lambda}{2d} = \frac{0.154\ \text{nm}}{0.201\ \text{nm}} = 0.766 \quad\Longrightarrow\quad \theta_2 = 50.0°.

Note that a third order would require sinθ3=1.149>1\sin\theta_3 = 1.149 > 1: with this wavelength and this spacing, only two orders exist. Requiring nλ2dn\lambda \le 2d also shows why X-rays are essential — with visible light, λ2d\lambda \gg 2d and no order exists at all, which is exactly why crystals look like ordinary transparent solids rather than gratings.

Not Just X-Rays

Bragg’s law contains no reference to what kind of wave is diffracting. Any wave whose wavelength is comparable to the interplanar spacing will do — and by the time you reach Chapter 7, you will know that electrons and neutrons are such waves.

That is not a rhetorical flourish; it is the historical route by which matter waves were confirmed. In 1927 Clinton Davisson and Lester Germer fired low-energy electrons at a nickel crystal and found the scattered intensity peaking at exactly the angles Bragg’s law predicts, for a wavelength matching de Broglie’s λ=h/p\lambda = h/p. Neutron diffraction, which is sensitive to light atoms in a way X-rays are not, is now the standard way to locate hydrogen in a crystal structure and to map magnetic ordering. The same equation, first written for X-rays, ended up as one of the sharpest pieces of evidence for the wave nature of matter.

Holography

An ordinary photograph records intensity and throws away phase, which is why it is flat: all the information about the shape of the wavefront arriving from the scene is lost. A hologram, invented by Dennis Gabor in 1947, records the phase as well — by the only means available, namely by converting phase differences into intensity differences through interference.

The recording step splits a laser beam in two. One part, the object beam, illuminates the subject and scatters from it onto the film. The other, the reference beam, goes straight to the film. Where the two arrive in phase the film is exposed; where they arrive out of phase it is not. What the film records is therefore a dense, fine interference pattern — nothing resembling a picture, just an apparently random speckle of microscopic fringes — which encodes both the amplitude and the phase of the light arriving from every point of the object.

The reconstruction step is pure diffraction. Illuminate the developed film with the reference beam alone, and the recorded fringe pattern acts as a complicated diffraction grating, diffracting the reference beam into exactly the wavefront that the object originally sent out. An observer looking into the film sees that wavefront and cannot tell it from the object: it has full parallax, and looking around the edge of a foreground object reveals what is behind it.

Two properties follow directly from this account. First, holography demands a source with a coherence length longer than the depth of the scene, which is why it was impossible before the laser and why Gabor’s original demonstrations were so limited. Second, every part of the hologram receives light from every part of the object, so a hologram cut in half still reconstructs the whole scene — from a smaller effective aperture, and therefore, by the Rayleigh criterion, with correspondingly poorer resolution.

Looking Ahead: Diffraction and the Uncertainty Principle

There is one more thing to extract from single-slit diffraction, and it is the reason this chapter belongs in a book on modern physics.

Take the pattern seriously as a statement about photons. A photon that passes through a slit of width aa has, at that moment, a position along the slit known to within

Δya.\Delta y \approx a .

It arrives traveling straight ahead, with no transverse momentum. Yet it lands somewhere within the central diffraction maximum, which means that on emerging it has acquired a transverse momentum of order psinθ1p\sin\theta_1, where θ1\theta_1 is the angle to the first minimum. Using sinθ1=λ/a\sin\theta_1 = \lambda/a and the photon momentum p=h/λp = h/\lambda (established in Chapter 6),

Δpypsinθ1=hλλa=ha.\Delta p_y \approx p\sin\theta_1 = \frac{h}{\lambda}\cdot\frac{\lambda}{a} = \frac{h}{a}.

Multiply:

ΔyΔpyaha=h.\Delta y\,\Delta p_y \approx a \cdot \frac{h}{a} = h .

The width of the slit has canceled out. Squeeze the slit to pin down the photon’s position and the diffraction pattern widens by exactly enough to keep the product fixed; open it up and the reverse happens. There is no way to make both small at once — not because the measuring apparatus is clumsy, but because the light is a wave, and this relation is a property of waves.

This is the Heisenberg uncertainty principle, arrived at from nothing but classical wave optics and one quantum fact (p=h/λp = h/\lambda). Chapter 7 derives it properly, shows that it applies to electrons and every other particle, and works out its consequences. But it is worth seeing now, in this chapter, that its origin lies in the ordinary mathematics of diffraction — that the strangest feature of quantum mechanics is, at bottom, the same phenomenon that spreads light behind a narrow slit.

5.5Summary

5.6Conceptual Questions

  1. State, in one sentence each, the physical difference between the conditions dsinθ=mλd\sin\theta = m\lambda for a double slit and asinθ=mλa\sin\theta = m\lambda for a single slit. Why do two nearly identical formulas describe opposite things?

  2. Explain, using the pairing argument, why θ=0\theta = 0 can never be a diffraction minimum, no matter how many strips the slit is divided into.

  3. A single slit is illuminated with red light, then with blue light. Which pattern is wider, and why? Now the same slit is made narrower. Which way does the pattern change? Are the two answers consistent with a single rule?

  4. Explain why a wider telescope aperture improves angular resolution, while a wider slit narrows the diffraction pattern. These sound like opposite statements about what a bigger aperture does. Show that they are the same statement.

  5. In a real double-slit pattern, some interference maxima are missing entirely. Explain what has happened to the light that “should” have been there, and why energy is nonetheless conserved.

  6. Why can visible light not be used to determine crystal structures by Bragg diffraction? Answer quantitatively, using the constraint nλ2dn\lambda \le 2d.

  7. A hologram is cut in half. Explain why each half still reconstructs the entire scene, and what is degraded.

  8. A camera lens is stopped down from f/2f/2 to f/16f/16, reducing the aperture diameter by a factor of 8. Aberrations improve when a lens is stopped down, but diffraction gets worse. Explain the trade-off, and state which effect dominates at very small apertures.

5.7Problems

Solution to Exercise 5.1 #

The minima obey asinθm=mλa\sin\theta_m=m\lambda. With a=0.0250 mm=2.50×105 ma=0.0250\ \text{mm}=2.50\times10^{-5}\ \text{m} and λ=633 nm\lambda=633\ \text{nm},

sinθ1=0.02532,θ1=1.45,sinθ2=0.05064,θ2=2.90.\sin\theta_1=0.02532,\quad\theta_1=1.45^\circ,\qquad \sin\theta_2=0.05064,\quad\theta_2=2.90^\circ.

The central maximum extends from the first minimum on one side to that on the other, so its small-angle width is

w=2Lλa=2(1.80 m)(633×109 m)2.50×105 m=9.12×102 m=9.12 cm.w=\frac{2L\lambda}{a}=\frac{2(1.80\ \text{m})(633\times10^{-9}\ \text{m})}{2.50\times10^{-5}\ \text{m}}=9.12\times10^{-2}\ \text{m}=9.12\ \text{cm}.

Therefore, the first and second minima are at 1.451.45^\circ and 2.902.90^\circ, and the central maximum is 9.12 cm9.12\ \text{cm} wide.

Solution to Exercise 5.2 #

For a central-maximum width w=2Lλ/aw=2L\lambda/a,

a=2Lλw=2(1.50 m)(520×109 m)4.00×102 m=3.90×105 m.a=\frac{2L\lambda}{w}=\frac{2(1.50\ \text{m})(520\times10^{-9}\ \text{m})}{4.00\times10^{-2}\ \text{m}}=3.90\times10^{-5}\ \text{m}.

Therefore, the slit width is 3.90×105 m3.90\times10^{-5}\ \text{m}, or 0.0390 mm0.0390\ \text{mm}.

Solution to Exercise 5.3 #

At β/2=1.5π\beta/2=1.5\pi,

II0=[sin(1.5π)1.5π]2=(14.712)2=0.0450.\frac{I}{I_0}=\left[\frac{\sin(1.5\pi)}{1.5\pi}\right]^2=\left(\frac{-1}{4.712}\right)^2=0.0450.

The true first secondary maximum is 0.0470I00.0470I_0, so the midpoint estimate is lower by 0.0020I00.0020I_0, or about 4%4\% of the secondary-maximum value. Therefore, the halfway-point intensity is 4.50%4.50\% of the central maximum and is already a good approximation to the true 4.7%4.7\% secondary maximum.

Solution to Exercise 5.4 #

The Fresnel number is F=a2/(λL)F=a^2/(\lambda L). Setting F1F\sim1 gives

La2λ=(0.10×103 m)2550×109 m=1.82×102 m=1.8 cm.L\sim\frac{a^2}{\lambda}=\frac{(0.10\times10^{-3}\ \text{m})^2}{550\times10^{-9}\ \text{m}}=1.82\times10^{-2}\ \text{m}=1.8\ \text{cm}.

Therefore, distances only of order 2 cm2\ \text{cm} are still at the Fresnel--Fraunhofer boundary; the far-field formulas require a screen appreciably farther away than this scale.

Solution to Exercise 5.5 #

The ratio is

da=0.100 mm0.020 mm=5.\frac da=\frac{0.100\ \text{mm}}{0.020\ \text{mm}}=5.

An interference maximum is missing when mλ/d=pλ/am\lambda/d=p\lambda/a, or m=p(d/a)=5pm=p(d/a)=5p. Up to m=12m=12, the missing orders are m=5m=5 and m=10m=10. The central envelope contains m<d/a=5|m|<d/a=5, namely m=4,,4m=-4,\ldots,4, for nine nonmissing bright fringes — exactly the pattern plotted in Figure 5.6, whose missing orders m=±5,±10m=\pm5,\pm10 are this problem’s d/a=5d/a=5. Therefore, d/a=5d/a=5, orders 5 and 10 are absent, and nine bright fringes lie inside the central diffraction maximum.

Solution to Exercise 5.6 #

If d/ad/a is an integer qq, the central maximum contains the orders m=(q1),,0,,q1m=-(q-1),\ldots,0,\ldots,q-1, a total of 2q12q-1 bright fringes. Hence

2q1=7q=4.2q-1=7\quad\Rightarrow\quad q=4.

Therefore, the slit-separation-to-width ratio is d/a=4d/a=4.

Solution to Exercise 5.7 #

The line density is 5000 cm1=5.00×105 m15000\ \text{cm}^{-1}=5.00\times10^5\ \text{m}^{-1}, so

d=15.00×105 m1=2.00×106 m.d=\frac1{5.00\times10^5\ \text{m}^{-1}}=2.00\times10^{-6}\ \text{m}.

For first order, sinθ=λ/d=(500 nm)/(2000 nm)=0.250\sin\theta=\lambda/d=(500\ \text{nm})/(2000\ \text{nm})=0.250, so θ=14.5\theta=14.5^\circ. The largest order is mmax=d/λ=4m_{\max}=\lfloor d/\lambda\rfloor=4. Differentiating dsinθ=mλd\sin\theta=m\lambda gives

dθdλ=mdcosθ=5.16×105 rad/m=0.0296/nm.\frac{d\theta}{d\lambda}=\frac{m}{d\cos\theta}=5.16\times10^5\ \text{rad/m}=0.0296^\circ/\text{nm}.

Therefore, the spacing is 2.00 μm2.00\ \mu\text{m}, the first-order angle is 14.514.5^\circ, the mathematical upper-bound order is 4, and the first-order dispersion is 0.0296/nm0.0296^\circ/\text{nm}. The fourth order is at grazing angle, so the highest usable order is 3.

Solution to Exercise 5.8 #

Resolving power is R=mN=λ/ΔλR=mN=\lambda/\Delta\lambda. In second order,

Δλ=600 nm(2)(4000)=0.0750 nm.\Delta\lambda=\frac{600\ \text{nm}}{(2)(4000)}=0.0750\ \text{nm}.

In first order it is 600/4000=0.150 nm600/4000=0.150\ \text{nm}, twice as large, so the resolution is two times poorer. If only 1000 lines are illuminated in second order, R=2000R=2000 and Δλ=0.300 nm\Delta\lambda=0.300\ \text{nm}; only illuminated lines contribute coherently, exactly as Figure 5.7 shows for the sodium doublet: raising NN narrows each order’s peak until two close wavelengths separate. Therefore, second order resolves 0.0750 nm0.0750\ \text{nm} versus 0.150 nm0.150\ \text{nm} in first order, and narrowing the beam reduces the resolving power in direct proportion to the illuminated line count.

Solution to Exercise 5.9 #

The spacing is d=(600 mm1)1=1.667 μmd=(600\ \text{mm}^{-1})^{-1}=1.667\ \mu\text{m}. In first order the endpoint angles are sin1(400/1667)=13.9\sin^{-1}(400/1667)=13.9^\circ and sin1(700/1667)=24.8\sin^{-1}(700/1667)=24.8^\circ, so the width is 10.910.9^\circ. In second order they are sin1(0.480)=28.7\sin^{-1}(0.480)=28.7^\circ and sin1(0.840)=57.1\sin^{-1}(0.840)=57.1^\circ, so the width is 28.428.4^\circ.

Overlap begins where 2λ2=3λ32\lambda_2=3\lambda_3. The first common direction occurs for λ2=600 nm\lambda_2=600\ \text{nm} and λ3=400 nm\lambda_3=400\ \text{nm}, at sinθ=0.720\sin\theta=0.720 or θ=46.1\theta=46.1^\circ. The overlap ends where the second-order red limit is reached, at λ2=700 nm\lambda_2=700\ \text{nm} and θ=57.1\theta=57.1^\circ (which corresponds to λ3=466.7 nm\lambda_3=466.7\ \text{nm} in third order).

Diffraction angle versus wavelength for the first, second, and third grating orders, with the angular band where the second and third orders overlap shaded.

Figure 5.11:The three orders’ angular ranges as λ\lambda sweeps across the visible spectrum. The shaded band is where 2nd- and 3rd-order light arrive at the same angle; it begins where the 2nd order’s 600 nm600\ \text{nm} meets the 3rd order’s 400 nm400\ \text{nm}, both at 46.146.1^\circ.

Therefore, the first- and second-order widths are 10.910.9^\circ and 28.428.4^\circ, and second and third orders overlap from 46.146.1^\circ to 57.157.1^\circ.

Solution to Exercise 5.10 #

The Rayleigh limit is

θmin=1.22λD=1.22(550×109 m)4.0×103 m=1.68×104 rad=34.6 arcsec.\theta_{\min}=\frac{1.22\lambda}{D}=\frac{1.22(550\times10^{-9}\ \text{m})}{4.0\times10^{-3}\ \text{m}}=1.68\times10^{-4}\ \text{rad}=34.6\ \text{arcsec}.

At L=0.250 mL=0.250\ \text{m}, sLθ=(0.250)(1.68×104)=4.19×105 m=42 μms\simeq L\theta=(0.250)(1.68\times10^{-4})=4.19\times10^{-5}\ \text{m}=42\ \mu\text{m}. This is the “just resolved” case of Figure 5.8, where the two Airy patterns are separated by exactly θmin\theta_{\min}. Therefore, the ideal eye resolves about 34.6 arcsec34.6\ \text{arcsec}, corresponding to 42 μm42\ \mu\text{m} at reading distance.

Solution to Exercise 5.11 #

Using s=Lθmins=L\theta_{\min},

Lmax=1.3 m1.68×104 rad=7.75×103 m=7.8 km.L_{\max}=\frac{1.3\ \text{m}}{1.68\times10^{-4}\ \text{rad}}=7.75\times10^3\ \text{m}=7.8\ \text{km}.

Therefore, diffraction alone would permit resolution to roughly 7.8 km7.8\ \text{km}. In ordinary viewing, the eye’s aberrations and retinal sampling usually make the practical limit less favorable; atmospheric turbulence can add further blur over long paths.

Solution to Exercise 5.12 #

Since θmin=1.22λ/D\theta_{\min}=1.22\lambda/D, doubling DD changes the limit to θmin/2\theta_{\min}/2. Halving λ\lambda from 550 nm550\ \text{nm} to 275 nm275\ \text{nm} at fixed DD also changes it to θmin/2\theta_{\min}/2. Therefore, either modification improves the angular resolution by a factor of two.

Solution to Exercise 5.13 #

The half-angle subtended by the objective is α=arctan[(D/2)/L]=arctan(2.5/8.0)=17.4\alpha=\arctan[(D/2)/L]=\arctan(2.5/8.0)=17.4^\circ, so in air its numerical aperture is NA=sinα=0.298\mathrm{NA}=\sin\alpha=0.298 (the small-angle estimate D/(2L)=0.313D/(2L)=0.313 is close). Thus

dmin0.61λNA=0.61(550 nm)0.298=1.13 μm.d_{\min}\simeq\frac{0.61\lambda}{\mathrm{NA}}=\frac{0.61(550\ \text{nm})}{0.298}=1.13\ \mu\text{m}.

At the same aperture angle, replacing 550 nm550\ \text{nm} by 4.0 pm4.0\ \text{pm} gives dmin=8.2 pmd_{\min}=8.2\ \text{pm}, an improvement by 550 nm/4.0 pm=1.38×105550\ \text{nm}/4.0\ \text{pm}=1.38\times10^5. Therefore, the light microscope resolves about 1.1 μm1.1\ \mu\text{m} and the electron microscope about 8 pm8\ \text{pm} under the stated idealized comparison.

Solution to Exercise 5.14 #

Bragg’s law is 2dsinθ=mλ2d\sin\theta=m\lambda. For first order,

d=0.0709 nm2sin15.0=0.137 nm.d=\frac{0.0709\ \text{nm}}{2\sin15.0^\circ}=0.137\ \text{nm}.

For second order, sinθ2=2λ/(2d)=0.518\sin\theta_2=2\lambda/(2d)=0.518, so θ2=31.2\theta_2=31.2^\circ. Finally m2d/λ=3.86m\le2d/\lambda=3.86, so mmax=3m_{\max}=3.

Bar chart of sin(theta_m) for orders m = 1 through 5, with m = 1, 2, 3 below the sin(theta) = 1 limit and m = 4, 5 shown as impossible above it.

Figure 5.12:sinθm=mλ/2d\sin\theta_m=m\lambda/2d grows in equal steps with mm; it crosses the physical ceiling sinθ=1\sin\theta=1 between m=3m=3 and m=4m=4, so no reflection of any order beyond m=3m=3 exists for these planes.

Therefore, the plane spacing is 0.137 nm0.137\ \text{nm}, the second-order reflection is at 31.231.2^\circ, and orders through m=3m=3 exist.

Solution to Exercise 5.15 #

For first order,

λ=2dsinθ=2(0.282 nm)sin20.0=0.193 nm.\lambda=2d\sin\theta=2(0.282\ \text{nm})\sin20.0^\circ=0.193\ \text{nm}.

This is 1.93×1010 m1.93\times10^{-10}\ \text{m}, in the X-ray region. Since sinθ1\sin\theta\le1, the longest diffracting wavelength is λmax=2d=0.564 nm\lambda_{\max}=2d=0.564\ \text{nm}. Therefore, the required wavelength is 0.193 nm0.193\ \text{nm} and no wavelength longer than 0.564 nm0.564\ \text{nm} can produce a Bragg reflection from these planes.

Solution to Exercise 5.16 #

Bragg’s law requires mλ=2dsinθm\lambda=2d\sin\theta. Because sinθ1\sin\theta\le1 and the smallest order is m=1m=1, an order can exist only if λ2d\lambda\le2d. For d=0.3 nmd=0.3\ \text{nm}, 2d=0.6 nm2d=0.6\ \text{nm}, whereas visible light has λ=550 nm\lambda=550\ \text{nm}. Therefore, visible light is about 900 times too long in wavelength to diffract from atomic crystal planes.

Solution to Exercise 5.17 #

The first minimum of a narrow slit obeys θ1λ/a\theta_1\simeq\lambda/a, so decreasing aa makes the diffracted beam wider: localization at a smaller opening creates a larger angular spread. A telescope, however, uses a large aperture to make the diffraction pattern of each point source narrower, allowing two nearby patterns to be distinguished. Therefore, the statements are complementary rather than contradictory: a narrow aperture spreads one beam widely, while a large collecting aperture reduces the diffraction blur of an image.

Solution to Exercise 5.18 #

For a=1.0 μma=1.0\ \mu\text{m}, sinθ1=λ/a=0.500\sin\theta_1=\lambda/a=0.500, hence θ1=30.0\theta_1=30.0^\circ. Taking Δpypsinθ1\Delta p_y\sim p\sin\theta_1 and p=h/λp=h/\lambda,

Δpyhλλa=ha=6.63×1028 kg m/s,\Delta p_y\sim\frac{h}{\lambda}\frac{\lambda}{a}=\frac{h}{a}=6.63\times10^{-28}\ \text{kg m/s},

so ΔyΔpy(1.0×106 m)(6.63×1028 kg m/s)=6.63×1034 J s=h\Delta y\Delta p_y\sim(1.0\times10^{-6}\ \text{m})(6.63\times10^{-28}\ \text{kg m/s})=6.63\times10^{-34}\ \text{J s}=h. For a=0.50 μma=0.50\ \mu\text{m}, the first minimum is at 9090^\circ, Δpyh/(0.50 μm)=1.33×1027 kg m/s\Delta p_y\sim h/(0.50\ \mu\text{m})=1.33\times10^{-27}\ \text{kg m/s}, and the product is again hh. Therefore, halving the slit doubles the momentum uncertainty while leaving ΔyΔpy\Delta y\Delta p_y of order hh.

Solution to Exercise 5.19 #

The synthesized aperture has

θmin=1.22(1.3×103 m)1.0×107 m=1.59×1010 rad=32.7 μarcsec.\theta_{\min}=\frac{1.22(1.3\times10^{-3}\ \text{m})}{1.0\times10^7\ \text{m}}=1.59\times10^{-10}\ \text{rad}=32.7\ \mu\text{arcsec}.

Since 32.7 μarcsec<40 μarcsec32.7\ \mu\text{arcsec}<40\ \mu\text{arcsec}, the shadow is just resolvable.

Log-log plot of angular resolution versus aperture diameter at 1.3 millimeter wavelength, marking a 100 meter single dish, the 40 microarcsecond M87 shadow, and the Earth-scale synthesized aperture that reaches it.

Figure 5.13:Angular resolution improves only as 1/D1/D, so reaching 40 μarcsec40\ \mu\text{arcsec} at λ=1.3 mm\lambda=1.3\ \text{mm} requires an aperture the size of the Earth; even the largest single dish (D100 mD\sim100\ \text{m}) falls short by a factor of 105.

Therefore, Earth-scale interferometry provides just enough resolution, whereas a single dish would need an impossible diameter comparable to Earth to supply the same aperture.

Solution to Exercise 5.20 #

For a CD, d=1.6 μmd=1.6\ \mu\text{m} and sinθ1=650/1600=0.406\sin\theta_1=650/1600=0.406, so θ1=24.0\theta_1=24.0^\circ. The maximum order is 1600/650=2\lfloor1600/650\rfloor=2. For a DVD, d=0.74 μmd=0.74\ \mu\text{m}, so sinθ1=650/740=0.878\sin\theta_1=650/740=0.878 and θ1=61.4\theta_1=61.4^\circ.

Bar chart comparing diffraction angles for orders 1 through 3 on a CD and a DVD, with the DVD's first order already larger than the CD's second order, and higher orders impossible for the DVD.

Figure 5.14:At the same wavelength, the DVD’s smaller track spacing pushes every order to a larger angle; its first order alone exceeds the CD’s, and no second order exists for the DVD at all, since 2λ/d>12\lambda/d>1 there.

Therefore, a DVD sends the first order to a much larger angle than a CD, producing a wider color spread because its track spacing is smaller.