Chapter 33 Interference and DiffractionConceptual Problems 1 • A phase difference due to path-length difference is observed for monochromatic visible light. Which phase difference requires the least (minimum) path length difference? (a) 90o (b) 180o (c) 270o (d) the answer depends on the wavelength of the light. Determine the Concept The phase difference δ due to a path difference Δr are related according to δ 2π = Δr λ . Therefore, the least path length difference corresponds to the smallest phase difference. (a ) is correct. 2 • Which of the following pairs of light sources are coherent: (a) two candles, (b) one point source and its image in a plane mirror, (c) two pinholes uniformly illuminated by the same point source, (d) two headlights of a car, (e) two images of a point source due to reflection from the front and back surfaces of a soap film. Determine the Concept Coherent sources have a constant phase difference. The pairs of light sources that satisfy this criterion are (b), (c), and (e). 3 • [SSM] The spacing between Newton’s rings decreases rapidly as the diameter of the rings increases. Explain qualitatively why this occurs. Determine the Concept The thickness of the air space between the flat glass and the lens is approximately proportional to the square of d, the diameter of the ring. Consequently, the separation between adjacent rings is proportional to 1/d. 4 • If the angle of a wedge-shaped air film, such as that in Example 32-2 is too large, fringes are not observed. Why? Determine the Concept There are two possible reasons that fringes might not be observed. (1) The distance between adjacent fringes is so small that the fringes are not resolved by the eye. (2) Twice the thickness of the air space is greater than the coherence length of the light. If this is the case, fringes would be observed in the region close to the point where the thickness of the air space approaches zero. 5 • Why must a film that is used to observe interference colors be thin? Determine the Concept Colors are observed when the light reflected off the front and back surfaces of the film interfere destructively for some wavelengths and 3047 3048 Chapter 33 constructively for other wavelengths. For this interference to occur, the phase difference between the light reflected off the front and back surfaces of the film must be constant. This means that twice the thickness of the film must be less than the coherence length of the light. The film is called a thin film if twice its thickness is less than the coherence length of the light. 6 • A loop of wire is dipped in soapy water and held up so that the soap film is vertical. (a) Viewed by reflection with white light, the top of the film appears black. Explain why. (b) Below the black region are colored bands. Is the first band red or violet? (a) The phase change due to reflection from the front surface of the film is 180°; the phase change due to reflection from the back surface of the film is 0°. As the film thins toward the top, the phase change due to the path length difference between the two reflected waves (the phase difference associated with the film’s thickness) becomes negligible and the two reflected waves interfere destructively. (b) The first constructive interference will arise when twice the thickness of the film is equal to half the wavelength of the color with the shortest wavelength. Therefore, the first band will be violet (shortest visible wavelength). 7 • [SSM] A two-slit interference pattern is formed using monochromatic laser light with a wavelength of 640 nm. At the second maximum from the central maximum, what is the path-length difference between the light coming from each of the slits? (a) 640 nm (b) 320 nm (c) 960 nm (d) 1280 nm. Determine the Concept For constructive interference, the path difference is an integer multiple of λ; that is, Δr = mλ . For m = 2, Δr = 2(640 nm) . (d ) is correct. 8 • A two-slit interference pattern is formed using monochromatic laser light with a wavelength of 640 nm. At the first minimum from the central maximum, what is the path-length difference between the light coming from each of the slits? (a) 640 nm (b) 320 nm (c) 960 nm (d) 1280 nm. Determine the Concept For destructive interference, the path difference is an odd-integer multiple of 1 λ ; that is Δr = m( 1 λ ), m = 1, 3, 5, ... . For the first 2 2 minimum, m = 1 and Δr = 1 2 (640 nm) = 320 nm . (b ) is correct. 9 • A two-slit interference pattern is formed using monochromatic laser light with a wavelength of 450 nm. What happens to the distance between the first maximum and the central maximum as the two slits are moved closer together? Interference and Diffraction 3049 (a) The distance increases. (b) The distance decreases. (c) The distance remains the same. Determine the Concept The relationship between the slit separation d and the angular position θm of each maximum is given by d sin θ m = mλ , m = 0,1, 2, ... (Equation 33-2). Because d and sinθm are inversely proportional for a given wavelength and interference maximum (value of m), decreasing d increases sinθm and θm. (a ) is correct. 10 • A two-slit interference pattern is formed using two different monochromatic lasers, one green and one red. Which color light has its first maximum closer to the central maximum? (a) Green, (b) red, (c) both maxima are in the same location. Determine the Concept The relationship between the slit separation d, the angular position θm of each maximum, and the wavelength of the light illuminating the slits is given by d sin θ m = mλ , m = 0,1, 2, ... (Equation 33-2). Because λ and sinθm are directly proportional for a given interference maximum (value of m) and the wavelength of green light is shorter than the wavelength of red light, (a ) is correct. 11 • A single slit diffraction pattern is formed using monochromatic laser light with a wavelength of 450 nm. What happens to the distance between the first maximum and the central maximum as the slit is made narrower? (a) The distance increases. (b) The distance decreases. (c) The distance remains the same. Determine the Concept The relationship between the slit width a, the angular position θm of each maximum, and the wavelength of the light illuminating the slit is given by a sin θ m = mλ , m =1, 2, 3, ... (Equation 33-11). Because a and sinθm are inversely proportional for a given diffraction maximum (value of m), narrowing the slit increases sin θ m and θm. (a ) is correct. 12 • Equation 33-2 which is d sin θm = mλ, and Equation 33-11, which is a sin θm = mλ, are sometimes confused. For each equation, define the symbols and explain the equation’s application. Determine the Concept Equation 33-2 expresses the condition for an intensity maximum in two-slit interference. Here d is the slit separation, λ the wavelength of the light, m an integer, and θm the angle at which the interference maximum appears. Equation 33-11 expresses the condition for an intensity minimum in single-slit diffraction. Here a is the width of the slit, λ the wavelength of the light, and θ m the angle at which the minimum appears, and m is (b) the interference fringes move closer together. (c) is correct. … ⎛λ⎞ θ1 = sin −1 ⎜ ⎟ ⎝d ⎠ θ green light < θ red light and (a) is correct. Determine the Concept The distance on the screen to mth bright fringe is given by: d where L is the distance from the slits to the screen. (b) is closer to the central maximum than the first-order maximum of blue light. 1. 2. Using light from a helium-neon laser. λn is the wavelength of the light in a medium whose index of refraction is n. (d) overlaps the second-order maximum of blue light. 13 • When a diffraction grating is illuminated by white light. the first-order maximum of green light (a) is closer to the central maximum than the first-order maximum of red light. and d is the separation of the slits. ym − ym−1. The interference maxima in a diffraction pattern are at angles θ given by: Solve for the angular location θ1 of the first-order maximum : Because λgreen light < λred light: d sin θ = mλ where d is the separation of the slits and m = 0. y m +1 − y m = (m + 1) ym = m λn L The separation of the interference fringes is given by: λn L d −m λn L d = λn L d Because the index of refraction of a vacuum is slightly less than the index of refraction of air. the removal of air increases λn and. Picture the Problem We can solve d sin θ = mλ for θ with m = 1 to express the location of the first-order maximum as a function of the wavelength of the light. one will note that (a) the interference fringes remain fixed. an interference pattern is observed when the chamber is open to air. 14 • A double-slit interference experiment is set up in a chamber that can be evacuated. (d) the interference fringes disappear completely. hence. (c) overlaps the second-order maximum of red light.3050 Chapter 33 a nonzero integer. (c) the interference fringes move farther apart. As the chamber is evacuated. . the narrower the slit. the wider the central maximum of the diffraction pattern. light from a two-slit device forms a pattern with very bright and very dark parts. the narrower the slit.Interference and Diffraction 3051 15 • [SSM] True or false: (a) (b) (c) (d) (e) When waves interfere destructively. the energy is no longer distributed evenly. Which color filter is most likely to prevent your resolving the images on your retinas as coming from two distinct sources? (a) red (b) yellow (c) green (d) blue (e) The filter choice is irrelevant. the energy is converted into heat energy.22 λ D ). the θ m = sin −1 a wider the central maximum of the diffraction pattern. The total energy over the entire pattern equals the energy from one slit plus the energy from the second slit. A circular aperture can produce both a Fraunhofer diffraction pattern and a Fresnel diffraction pattern. Hence. There is practically no energy at the dark fringes and a great deal of energy at the bright fringe. The width of the central maximum in the diffraction pattern is given by mλ where a is the width of the slit. (e) True. Interference patterns are observed only if the relative phases of the waves that superimpose remain constant. The ability to resolve two point sources depends on the wavelength of the light. (a) False. When destructive interference of light waves occurs. 16 • You observe two very closely-spaced sources of white light through a circular opening using various filters. . (b) True. The critical angle for the resolution of two sources is directly proportional to the wavelength of the light emitted by the sources ( α c = 1. (d) True. For example. (c) True. Interference re-distributes the energy. In the Fraunhofer diffraction pattern for a single slit. 17 •• Explain why the ability to distinguish the two headlights of an oncoming car. is easier for the human eye at night than during daylight hours. Because the diameter of the pupils of your eyes are larger at night. in this case headlights.22λ D (Equation 33-25). Check to see if this claim is true. The larger the critical angle required for resolution.3052 Chapter 33 Determine the Concept The condition for the resolution of the two sources is given by Rayleigh’s criterion: α c = 1. at a given distance. D is the diameter of the aperture. and λ is the wavelength of the light coming from the objects. Picture the Problem We’ll assume that the diameter of the pupil of the eye is 5. the less likely it is that you can resolve the sources as being two distinct sources.0 mm and use the best-case scenario (the minimum resolvable width varies directly with the wavelength of the light reflecting from the object) that the wavelength of light is 400 nm (the lower limit for the human eye). Relate the width w of an object that can be seen at an altitude h to the critical angular separation αc: tan α c = w ⇒ w = h tan α c h . Determine the Concept The condition for the resolution of the two sources is given by Rayleigh’s criterion: α c = 1. Assume the headlights of the oncoming car are on during both daytime and nighttime hours. (d ) is correct. where αc is the critical angular separation and D is the diameter of the aperture. Estimation and Approximation 18 • It is claimed that the Great Wall of China is the only man made object that can be seen from space with the naked eye. Then we can use the expression for the minimum angular separation of two objects than can be resolved by the eye and the relationship between this angle and the width of an object and the distance from which it is viewed to support the claim.22 λ D (Equation 33-25). the filter that passes the shorter wavelength light would be most likely to resolve the sources. based on the resolving power of the human eye. Because αc and λ are directly proportional. where αc is the critical angular separation. which means that at night you can resolve the light as coming from two distinct sources when they are at a greater distance. to be resolved. Assume the observers are in lowEarth orbit that has an altitude of about 250 km. the critical angle is smaller at night. (The Chinese astronaut Yang Liwei reported that he was not able to see the wall with the naked eye during the first Chinese manned space flight in 2003.Interference and Diffraction 3053 The minimum angular separation αc of two point objects that can just be resolved by an eye depends on the diameter D of the eye and the wavelength λ of light: Substitute for αc in the expression for w to obtain: α c = 1. d L where d is the separation of head lights (or tail lights) and L is the distance to approaching or receding automobile.) 19 •• [SSM] (a) Estimate how close an approaching car at night on a flat.22 ⎟ D⎠ ⎝ Substitute numerical values and evaluate wmin for an altitude of 250 km: ⎛ ⎛ 400 nm ⎞ ⎞ wmin = (250 km ) tan ⎜1.5 m between typical automobile headlights and tail lights.22 λ D λ⎞ ⎛ w = h tan⎜1. This is because both binoculars and cameras have apertures that are larger than the pupil of the human eye. However. 550 nm for the wavelength of the light (as an average) emitted by the headlights. so this claim is likely false.22 λ The critical angular separation is also given by: α= .22⎜ ⎜ 5. and pictures can be taken of it using a camera. straight stretch of highway must be before its headlights can be distinguished from the single headlight of a motorcycle. it is easily seen using binoculars. α c = 1. a nighttime pupil diameter of 5.0 mm ⎟ ⎟ ≈ 24 m ⎟⎟ ⎜ ⎝ ⎠⎠ ⎝ This claim is probably false. Because the minimum width that is resolvable from low-Earth orbit (250 km) is 24 m and the width of the Great Wall is 5 to 8 m high and 5 m wide. 640 nm for red taillights.0 mm. (b) Estimate how far ahead of you a car is if its two red taillights merge to look as if they were one. and apply the Rayleigh criterion. (a) The Rayleigh criterion is given by Equation 33-25: D where D is the separation of the headlights (or tail lights). Picture the Problem Assume a separation of 1. (A test similar to this ″eye test″ was used in ancient Rome to test for eyesight acuity before entering the army.90 kHz.6 km 20 •• A small loudspeaker is located at a large distance to the east from you. Assume that the speaker and your ears are on the same line and let the distance between your ears be about 20 cm.22 ⇒ L = L D 1. The loudspeaker is driven by a sinusoidal current whose frequency can be varied. Anyone who could not tell there were two stars was rejected. Picture the Problem If your ears receive the sound exactly out of phase. f = 21 •• [SSM] Estimate the maximum distance a binary star system could be resolvable by the human eye.0 mm)(1. In this case. the stars were not a binary system.5 m ) ≈ 1. Assume the two stars are about fifty times further apart than the Earth and Sun are. Estimate the lowest frequency for which your ears would receive the sound waves exactly out of phase when you are facing north.86 kHz 2(20 cm ) or between 0.22(640 nm ) 11 km (b) For red light: 9.) .22(550 nm ) (5. A normal eye could just barely resolve two well-known close-together stars in the sky. the waves arriving at your ear that is farthest from the speaker must be traveling onehalf wavelength farther than the waves arriving at your ear that is nearest the speaker.3054 Chapter 33 Equate these expressions for αc to obtain: Substitute numerical values and evaluate L: λ d Dd = 1. Take the speed of sound in air to be 343 m/s. The lowest frequency corresponds to the longest wavelength. but the principle is the same.80 and 0.22λ L= L= (5.0 mm)(1. Neglect atmospheric effects.5 m ) ≈ 1. The frequency received by your ears is given by: Let Δr be the distance between your ears (the path difference) to obtain: Substituting for λ yields: f = v λ Δr = 1 λ ⇒ λ = 2Δr 2 v 2 Δr f = Substitute numerical values and evaluate f: 343 m/s = 0. then their angular separation is given by: The critical angular separation of the two sources is given by the Rayleigh criterion: For α = αc: α= d L α c = 1.22 ⇒ L = L D 1. If the distance between the binary stars is represented by d and the Earth-star distance by L. The difference in phase between the two waves is the sum of a π phase shift in the reflected wave and a phase shift due to the additional distance traveled by the wave reflected from the bottom of the water−air interface.22(550 nm ) 1c ⋅ y 9.59 × 1013 km × Phase Difference and Coherence 22 • Light of wavelength 500 nm is incident normally on a film of water 1. We can use the Rayleigh criterion for the separation of two sources and the geometry of the Earth-to-binary star system to derive an expression for the distance to the binary stars.22 λ D λ d Dd = 1.00 μm thick. (a) What is the wavelength of the light in the water? (b) How many wavelengths are contained in the distance 2t. The number of wavelengths of light contained in a given distance is the ratio of the distance to the wavelength of light in the given medium.0 mm)(50)(1.461× 1015 m 5. where t is the thickness of the film? (c) What is the phase difference between the wave reflected from the top of the air–water interface and the wave reflected from the bottom of the water–air interface in the region where the two reflected waves superpose? Picture the Problem The wavelength of light in a medium whose index of refraction is n is the ratio of the wavelength of the light in air divided by n.Interference and Diffraction 3055 Picture the Problem Assume that the diameter of a pupil at night is 5.9 c ⋅ y ≈ 5.22λ L= Substitute numerical values and evaluate L: (5.5 × 1011 m ) 1.33 . (a) Express the wavelength of light in water in terms of the wavelength of light in air: λwater = λair nwater = 500 nm = 376 nm 1.0 mm and that the wavelength of light is in the middle of the visible spectrum at about 550 nm. 6π rad or. Light of wavelength 700 nm is .00 cm )2 + (14.4π rad = 1. Relate a path difference Δr to a phase shift δ: The path difference Δr is: δ= Δr λ 2π Δr = 15.00 cm.00 μm ) = 5.9 rad ⎟ ⎠ Interference in Thin Films 24 • A wedge-shaped film of air is made by placing a small slip of paper between the edges of two flat plates of glass.682 cm ⎞ ⎟2π ≈ 2. 15.682 cm (3.0 cm) from the origin.64π rad from 12π rad.0 cm) and (3.50 cm ⎝ ⎛ 0. Picture the Problem The difference in phase depends on the path difference Δr according to δ = 2π .0 cm − = 0.32 rad ) = 11.3056 Chapter 33 N= 2t (b) Relate the number of wavelengths N to the thickness t of the film and the wavelength of light in water: (c) Express the phase difference as the sum of the phase shift due to reflection and the phase shift due to the additional distance traveled by the wave reflected from the bottom of the water−air interface: λ water = 2(1. If the sources are in phase. y = 14. one at x = 0.0 cm )2 Substitute numerical values and evaluate δ: δ =⎜ ⎜ 1. y = 15. δ = 0. The path difference is the difference in the distances of λ (0.00 cm.32 376 nm δ = δ reflection + δ additional distance traveled =π + 2t λwater 2π = π + 2π N Substitute for N and evaluate δ: δ = π rad + 2π (5.0 cm and the other at x = 3.0 cm. The sources are located in the z = 0 plane. subtracting 11. find the difference in phase between these two waves for a receiver located at the origin.1 rad 23 •• [SSM] Two coherent microwave sources both produce waves of wavelength 1. 14.50 cm.64π rad = 11. in turn. what are the limits on the diameter of the wire? Hint: The nineteenth fringe might not be right at the end.0 cm and that yellow sodium light (wavelength of 590 nm) is used for illumination. Two optically flat pieces of glass of length L are arranged with the wire between them. If 19 bright fringes are seen along this 20. and the resulting interference fringes are observed. and interference fringes are observed by reflection. what is the angle of the wedge? Picture the Problem Because the mth fringe occurs when the path difference 2t equals m wavelengths. The thickness of the wedge. . but you do not see a twentieth fringe at all. (a) Is the first fringe near the point of contact of the plates dark or bright? Why? (b) If there are five dark fringes per centimeter. as shown in Figure 33-40.Interference and Diffraction 3057 incident normally on the glass plates.0-cm distance. Suppose that L is 20. The setup is illuminated by monochromatic light. (a) The first fringe is dark because the phase difference due to reflection by the bottom surface of the top plate and the top surface of the bottom plate is 180° (b) The mth fringe occurs when the path difference 2t equals m wavelengths: Relate the thickness of the air wedge to the angle of the wedge: 2t = mλ t ⇒ t = xθ x where we’ve used a small-angle approximation to replace an arc length by the length of a chord. is related to the angle of the wedge and the distance from its vertex to the mth fringe. Picture the Problem The condition that one sees m fringes requires that the path difference between light reflected from the bottom surface of the top slide and the top surface of the bottom slide is an integer multiple of a wavelength of the light. θ= Substitute for t to obtain: 2 xθ = mλ ⇒ θ = mλ 1 m λ = 2x 2 x Substitute numerical values and evaluate θ : θ= ⎜ 1⎛ 5 ⎞ −4 ⎟ (700 nm ) = 1.75 × 10 rad 2 ⎝ cm ⎠ 25 •• [SSM] The diameters of fine fibers can be accurately measured using interference patterns. we can express the additional distance traveled by the light in air as an mλ. . the limits on d must be: Substitute numerical values to obtain: 2 where m = 19 (m − 1 ) λ < d < (m + 1 ) λ 2 2 2 2 or 5.5 μm < d < 5. and are separated at the other end by a wire that has a radius of 0. 1 2 glass plate glass plate wire t Relate the extra distance traveled by wave 2 to the distance equivalent to the phase change due to reflection and to the condition for constructive interference: 2t + 1 λ = λ ..8 μm (19 − 1 ) 590 nm < d < (19 + 1 ) 590 nm 2 2 2 26 •• Light that has a wavelength equal to 600 nm is used to illuminate two glass plates at normal incidence. 5 λ . 3 λ . . 2. This phase difference is the sum of a phase shift of π (equivalent to a λ/2 path difference) resulting from reflection plus a phase shift due to the additional distance traveled. 2λ ... 3λ . The plates are 22 cm in length. 2 0 ≤ t ≤ 2r and λ is the wavelength of light in air.3058 Chapter 33 2 d = mλ ⇒ d = mλ 2 The mth fringe occurs when the path difference 2d equals m wavelengths: Because the nineteenth (but not the twentieth) bright fringe can be seen. 1.025 mm. . touch at one end. How many bright fringes appear along the total length of the plates? Picture the Problem The light reflected from the top surface of the bottom plate (wave 2 in the diagram) is phase shifted relative to the light reflected from the bottom surface of the top plate (wave 1 in the diagram).. 2 2 2 and 2t = (m + 1 )λ where m = 0. …. 2 or 2t = 1 λ . the number of bright fringes is mmax + 1. …and 0 ≤ t ≤ 2r m= − ⎛ 2 (2r ) 1 ⎞ ⎛ 4r 1 ⎞ m max = int ⎜ − ⎟ = int ⎜ − ⎟ ⎝ λ 2⎠ 2⎠ ⎝ λ where r is the radius of the wire. (a) What is the thickness of the film? (b) What visible wavelengths are brightest in the reflected interference pattern? (c) If this film were resting on glass with an index of refraction of 1.60.025m m ) m max = int ⎜ − ⎝ 600 nm = int (166. for these wavelengths. 1. 450. N = mmax + 1 = 167 27 •• A thin film having an index of refraction of 1. we can use the condition for constructive interference to find the wavelengths in the visible portion of the spectrum that will be brightest in the reflected interference pattern and the condition for destructive interference to find the wavelengths of light missing from the reflected light when the film is placed on glass with an index of refraction greater than that of the film. It is illuminated normally by white light. Analysis of the reflected light shows that the wavelengths 360.Interference and Diffraction 3059 Solving for m gives: 1 λ 2 where m = 0. . (b) and (c) Once we’ve found the thickness of the film. and 602 nm are the only missing wavelengths in or near the visible portion of the spectrum. ⎛ 4 (0. there is destructive interference. what wavelengths in the visible spectrum would be missing from the reflected light? Picture the Problem (a) We can use the condition for destructive interference in a thin film to find the thickness of the film.50 is surrounded by air. 2.2 ) = 166 1⎞ 2⎟ ⎠ 2t Solve for the highest value of m: Substitute numerical values and evaluate m: Because we start counting from m = 0. That is. .. = (m + 1 )λ' 2 2 2 2 where λ′ is the wavelength of light in the oil and m = 0. 3 λ' . 2 2 2 2 or 2t = λ' . 2λ' . 3 λ' . 3. 2. 2. … Substitute for λ′ to obtain: 2nt λ 2t = (m + 1 ) ⇒ λ = 2 m+ 1 n 2 where n is the index of refraction of the film. 1. 2 or 2t = 1 λ' .. or λ (1) 2t = mλ' = m n where m = 1.. Substitute numerical values and simplify to obtain: λ= 2(1.2λ' .50 )(600 nm ) 1800 nm = m+ 1 m+ 1 2 2 .3060 Chapter 33 (a) Express the condition for destructive interference in the thin film: 2t + 1 λ' = 1 λ' .3λ' . . .. 5 λ' .. Solving for λ yields: λ= 2nt m 2nt 2nt and 360 nm = m m +1 Substitute for the missing wavelengths to obtain: Divide the first of these equations by the second and simplify to obtain: 450 nm = 2nt 450 nm m +1 = m = 2nt 360 nm m m +1 m = 4 for λ = 450 nm Solving for m gives: Solve equation (1) for t to obtain: t= mλ 2n Substitute numerical values and evaluate t: (b) The condition for constructive interference in the thin film is: t= 4(450 nm ) = 600 nm 2(1. … and λ′ is the wavelength of the light in the film.50) 2t + 1 λ' = λ' .. 5 λ' .... 3λ' . Picture the Problem Because there is a 1 2 λ phase change due to reflection at both the air-oil and oil-water interfaces. counting from the edge of the drop.. 5 λ' . . 2 2 2 or 2t = (m + 1 2 n where n is the index of refraction of the film and m = 0.33). the condition for constructive interference is that twice the thickness of the oil film equal an integer multiple of the wavelength of light in the film. 2. 1. 514 nm. 3 λ' . ..Interference and Diffraction 3061 Substitute numerical values for m and evaluate λ to obtain the following table: m λ (nm) 0 3600 1 1200 2 720 3 514 4 400 5 327 From the table. … )λ λ= 2nt m+ 1 2 2(1. 28 •• A drop of oil (refractive index of 1. and 400 nm. and 400 nm.5)(600 nm ) 1800 nm = m+ 1 m+ 1 2 2 Substitute numerical values and simplify to obtain: λ= Substitute numerical values for m and evaluate λ to obtain the following table: m λ (nm) 0 3600 1 1200 2 720 3 514 4 400 5 327 From the table we see that the missing wavelengths in the visible spectrum are 720 nm. the light reflected from the film-glass interface will be shifted by 1 λ (as is the wave reflected from 2 the top surface) and the condition for destructive interference becomes: Solving for λ yields: 2t = 1 λ' . 514 nm. as shown in Figure 33-41 what is the thickness of the drop at the point where the second red fringe. (c) Because the index of refraction of the glass is greater than that of the film. When reflected light is observed from above. we see that the only wavelengths in the visible spectrum are 720 nm. is observed? Assume red light has a wavelength of 650 nm.22) floats on water (refractive index of 1. 2..45 rests on an optically flat piece of glass with an index of refraction of 1.60. 3λ' . Express the condition for constructive interference: (1) where λ′ is the wavelength of light in the oil and m = 0. the condition for constructive interference is that twice the thickness of the oil film equal an integer multiple of the wavelength of light in the film. When illuminated by white light at normal incidence. … 2nt n m where n is the index of refraction of the oil. 2λ' . 2.. 3λ' . 2λ' .. Determine the thickness of the oil film. The condition for constructive interference is: or 2t = mλ' (1) where λ′ is the wavelength of light in the oil and m = 1.. 2t = m 2t = λ' . 3. Picture the Problem Because there is a 1 2 λ phase change due to reflection at both the air-oil and oil-glass interfaces.3062 Chapter 33 2t = λ' .. light of wavelengths 690 nm and 460 nm is predominant in the reflected light.. … 2t = m Substitute for λ′ to obtain: Substitute numerical values and evaluate t: λ n ⇒t = (2)(650 nm ) = t= 2(1. = mλ' Substitute for λ′ to obtain: λ ⇒λ = Substitute for the predominant wavelengths to obtain: Divide the first of these equations by the second and simplify to obtain: 690 nm = 2nt 2nt and 460 nm = m m +1 2nt 690 nm m +1 = m = ⇒m = 2 2nt 460 nm m m +1 t= mλ 2n Solve equation (1) for t: .22) mλ 2n 533 nm 29 •• [SSM] A film of oil that has an index of refraction of 1. 1. 1. When illuminated with white light at normal incidence. … λ= 2nt m+ 1 2 2nt 2nt and 500 nm = 1 m+ 2 m+ 3 2 700 nm = 2nt 700 nm m + 1 m + 3 2 2 = = ⇒m = 2 1 2nt m+ 2 500 nm m+ 3 2 t = (m + 1 ) 2 Solve equation (1) for t: λ 2n Substitute numerical values and evaluate t: t = (2 + 1 ) 2 700 nm = 603 nm 2(1. 2 or 2t = 1 λ' . Express the condition for constructive interference between the waves reflected from the airoil interface and the oil-glass interface: Substitute for λ' and solve for λ to obtain: Substitute the predominant wavelengths to obtain: Divide the first of these equations by the second to obtain: 2t + 1 λ' = λ' .. there is no phase shift in the light reflected from the oil-glass interface. We can use the condition for constructive interference to determine m for λ = 700 nm and then use this value in our equation describing constructive interference to find the thickness t of the oil film. 3λ' .45) ... 2λ' . Determine the thickness of the oil film. = (m + 1 )λ' 2 2 2 2 (1) where λ′ is the wavelength of light in the oil and m = 0. Because the index of refraction of the oil is greater than that of the glass.45 floats on water. 3 λ' . Picture the Problem Because the index of refraction of air is less than that of the oil. light of wavelengths 700 nm and 500 nm is predominant in the reflected light. 2.. there is a phase shift of π rad ( 1 λ ) in the light reflected at the air-oil 2 interface.. 5 λ' .Interference and Diffraction 3063 Substitute numerical values and evaluate t: t= (2)(690 nm ) = 2(1.45) 476 nm 30 •• A film of oil that has an index of refraction 1.. = (m + 1 )λ 2 2 2 2 where λ is the wavelength of light in air and m = 0. 2 or 2t = 1 λ . … Solving for t yields: t= (m + 1 ) λ .. A phase change of 180° ( 1 λ ) occurs 2 at the top of the flat glass plate.50 and water replaces the air between the two pieces of glass... (a) The condition for constructive interference is: 2t + 1 λ = λ . . . The thin film is air of variable thickness. the radius r of a fringe is related to t by r = 2tR . Picture the Problem This arrangement is essentially identical to a ″thin film″ configuration. 2. 2. 1. 2 2 2 (1) (b) From Figure 33-42 we have: r 2 + (R − t ) = R 2 or R 2 = r 2 + R 2 − 2 Rt + t 2 R 2 ≈ r 2 + R 2 − 2 Rt ⇒ r = For t << R we can neglect the last term to obtain: (c) Square equation (2) and substitute for t from equation (1) to obtain: 2 Rt (2) r 2 = (m + 1 )Rλ ⇒ m = 2 r2 1 − Rλ 2 . m = 0. 1. except that the ″film″ is air. 2 (b) Show that for t << R. We can use the condition for constructive interference to derive the result given in (a) and use the geometry of the lens on the plate to obtain the result given in (b).0 m and a lens diameter of 4.. The pattern is viewed by reflected light. (c) For a radius of curvature of 10. as shown in Figure 33-42. . explain qualitatively the changes that will take place in the bright-fringe pattern. . We can then use these results in the remaining parts of the problem. (a) Show that for a thickness t the condition for a bright (constructive) interference ring is 2t = (m + 1 )λ where m = 0. 3 λ . How many bright fringes would you see in the reflected light? (d) What would be the diameter of the sixth bright fringe? (e) If the glass used in the apparatus has an index of refraction n = 1.00 cm..1. 5 λ .3064 Chapter 33 Newton’s Rings 31 •• [SSM] A Newton’s ring apparatus consists of a plano-convex glass lens with radius of curvature R that rests on a flat glass plate.. The apparatus is illuminated from above by light from a sodium lamp that has a wavelength of 590 nm. 2.. 3λ .. 2λ . (d) The diameter of the mth fringe is: Noting that m = 5 for the sixth fringe. … Solving for t gives: t = (m + 1 ) . The separation between fringes is reduced (the fringes would become more closely spaced.00 m rests on an optically flat glass plate.. except that the ″film″ is air. The arrangement is illuminated from above with monochromatic light of 520-nm wavelength.Interference and Diffraction 3065 Substitute numerical values and evaluate m: m= (2. 3λ .00 cm)2 − 1 = 67 (10.. The condition for constructive interference is: 2t + 1 λ = λ . Determine the radii of the first and second bright fringe from the center in the reflected light. 2λ . The indexes of refraction of the lens and plate are 1.1.. 1.. = (m + 1 )λ 2 2 2 2 where λ is the wavelength of light in air and m = 0.33.0 m )(590 nm ) 2 = 1.) and the number of fringes that will be seen is increased by a factor of 1. substitute numerical values and evaluate D: D = 2r = 2 D = 2 (5 + 1 )(10. m = 0.. 2 or 2t = 1 λ . . 2.0 m )(590 nm) 2 (m + 1 )Rλ 2 and so there will be 68 bright fringes. Picture the Problem This arrangement is essentially identical to a ″thin film″ configuration. A phase change of 180° ( 1 λ ) occurs 2 at the top of the flat glass plate... 2. 5 λ . We can use the condition for constructive interference and the results from Problem 31(b) to determine the radii of the first and second bright fringes in the reflected light. 32 •• A plano-convex glass lens of radius of curvature 2. 2 2 λ In Problem 31(b) it was shown that: Substitute for t to obtain: r = 2tR r= (m + 1 )λR 2 . 3 λ .60..14 cm (e) The wavelength of the light in the film becomes λair/n = 444 nm. except that the ″film″ is oil. A phase change of 180° ( 1 λ ) occurs 2 at lens-oil interface.. 2.00 m ) = 0.82 is deposited on the plate. and the interference pattern is viewed on a screen 2.. … Substitute for λ′ and solve for t: . = (m + 1 )λ' 2 2 2 2 where λ′ is the wavelength of light in the oil and m = 0.. 2 or 2t = 1 λ' . . 2.535 mm 2 1.. 3 λ' .. The condition for constructive interference is: 2t + 1 λ' = λ' .00 m ) = 0..00 m ) = 1. a film of oil of refractive index 1. 1. 2n where λ is the wavelength of light in air. m = 0.. 5 λ' . 2λ' .926 mm 2 1.00 mm are illuminated by light of wavelength 600 nm. 3λ' . We can use the condition for constructive interference and the results from Problem 31(b) to determine the radii of the first and second bright fringes in the reflected light.721mm r= 3 2 (520 nm)(2.82 3 (520 nm )(2..00 m ) = 0.25 mm 33 ••• Suppose that before the lens of Problem 32 is placed on the plate. t = (m + 1 ) 2 λ In Problem 31(b) it was shown that: Substitute for t to obtain: r = 2tR r= (m + 1 ) λR 2 n 1 (520 nm )(2.82 The first fringe corresponds to m = 0: The second fringe corresponds to m = 1: r= r= Two-Slit Interference Patterns 34 • Two narrow slits separated by 1.3066 Chapter 33 The first fringe corresponds to m = 0: The second fringe corresponds to m = 1: r= 1 2 (520 nm)(2. What will then be the radii of the first and second bright fringes? Picture the Problem This arrangement is essentially identical to a ″thin film″ configuration.00 m .1. Express the distance on the screen to the mth and (m + 1)st bright fringe: Subtract the first of these equations from the second to obtain: Because the number of fringes per unit length N is the reciprocal of Δy: ym = m λL d and ym+1 = (m + 1) λL d Δy = λL d ⇒d = λL Δy d = Nλ L .00 m away. Because the number of bright fringes per unit length N is the reciprocal of Δy.Interference and Diffraction 3067 away. λ.00 mm = 8. and L. Calculate the number of bright fringes per centimeter on the screen in the region near the center fringe. 28 bright fringes per centimeter are observed near the center of a screen 3. Express the number N of bright fringes per centimeter in terms of the separation of the fringes: Express the distance on the screen to the mth and (m + 1)st bright fringe: Subtract the first of these equations from the second to obtain: Substitute in equation (1) to obtain: N= 1 Δy (1) ym = m λL d and ym+1 = (m + 1) λL d Δy = λL d d λL N= Substitute numerical values and evaluate N: N= 1. We can use the expression for the distance on the screen to the mth fringe to find the separation of the fringes. we can find d from N. Picture the Problem The number of bright fringes per unit distance is the reciprocal of the separation of the fringes.00 m ) 35 • [SSM] Using a conventional two-slit apparatus with light of wavelength 589 nm.33 cm −1 (600 nm )(2. What is the slit separation? Picture the Problem We can use the expression for the distance on the screen to the mth and (m + 1)st bright fringes to obtain an expression for the separation Δy of the fringes as a function of the separation of the slits d. To find the number of interference maxima that.06817 d≈ 633 nm = 9.95 mm ( ) 36 • Light of wavelength 633 nm from a helium–neon laser is shone normally on a plane containing two slits.29 μm = 9.06817 d sin θ = mλ. 2. Because there are 14 fringes on either side of the central maximum: N = 2mmax + 1 = 2(14) + 1 = 29 . possible to observe? Picture the Problem We can use the geometry of the setup. in principle..3 μm 0. (a) Find the separation of the slits. m = 0.1. to find the separation of the slits.3068 Chapter 33 Substitute numerical values and evaluate d: d = 28 cm −1 (589 nm )(3.. we can approximate sinθ1 as: From the right triangle whose sides are L and y1 we have: Substitute numerical values in equation (1) and evaluate d: (b) The equation describing two-slit interference maxima is: Because sinθ ≤ 1 determines the maximum number of interference fringes that can be seen: Substitute numerical values and evaluate mmax: sin θ1 ≈ λ d ⇒d ≈ λ sin θ1 (1) sin θ1 = 82 cm (12 m )2 + (82 cm)2 = 0.29 μm = 14 because m must 633 nm be an integer.00 m ) = 4. in principle. . y1 = 82 cm d θ θ1 0 L = 12 m λ Because d << L. d = mmax λ ⇒ mmax = d λ mmax = 9. The first interference maximum is 82 cm from the central maximum on a screen 12 m away. (b) How many interference maxima is it. we can apply the equation describing two-slit interference maxima and require that sinθ ≤ 1. can be observed. represented to the right. Picture the Problem Let the separation of the slits be d.00 cm.00 m ) = 1. In (c) we can use this same relationship to express the slit separation d.Interference and Diffraction 3069 37 •• Two narrow slits are separated by a distance d.00 m ) = 1. (b) Would you expect to be able to observe the interference of light on the screen for this situation? (c) How close together should the slits be placed for the maxima to be separated by 1. but not by much. (a) Calculate the spacing between successive maxima near the center fringe for light of wavelength 500 nm.500 mm 38 •• Light is incident at an angle φ with the normal to a vertical plane containing two slits of separation d (Figure 33-43).00 mm 0. when L is 1. .0 μm (b) According to the Raleigh criterion you could resolve them.00 mm for this wavelength and screen distance? Picture the Problem We can use the equation for the distance on a screen to the mth bright fringe to derive an expression for the spacing of the maxima on the screen. Show that the interference maxima are located at angles θm given by sin θm + sin φ = mλ/d. (a) Express the distance on the screen to the mth and (m + 1)st bright fringe: Subtract the first of these equations from the second to obtain: Substitute numerical values and evaluate Δy: ym = m λL d and ym+1 = (m + 1) λL d Δy = λL d (1) Δy = (500 nm )(1.00 cm 50. Their interference pattern is to be observed on a screen a large distance L away.00 m and d is 1. Express the total path difference: The condition for constructive interference is: Δl = d sin φ + d sin θ m Δl = mλ where m is an integer. (c) Solve equation (1) for d to obtain: d= λL Δy Substitute numerical values and evaluate d: d= (500 nm )(1. We can find the total path difference when the light is incident at an angle φ and set this result equal to an integer multiple of the wavelength of the light to obtain the given equation. . What visible wavelengths give a bright interference maximum in the transmitted light in the direction normal to the plane? (See Problem 38. We can find the total path difference when the light is incident at an angle φ and set this result equal to an integer multiple of the wavelength of the light to relate the angle of incidence on the slits to the direction of the transmitted light and its wavelength.3070 Chapter 33 Substitute to obtain: Divide both sides of the equation by d to obtain: d sin φ + d sin θ m = mλ sin φ + sin θ m = mλ d 39 •• [SSM] White light falls at an angle of 30º to the normal of a plane containing a pair of slits separated by 2.50 μm.50 μm )sin 30° = 1. d sin φ + d sin θ = mλ sin φ + sin θ = d sin φ m mλ d λ= λ= Substitute numerical values and simplify to obtain: (2. Express the total path difference: The condition for constructive interference is: Substitute to obtain: Divide both sides of the equation by d to obtain: Set θ = 0 and solve for λ: Δl = d sin φ + d sin θ Δl = mλ where m is an integer.) Picture the Problem Let the separation of the slits be d.25 μm m m Evaluate λ for positive integral values of m: m 1 2 3 4 λ (nm) 1250 625 417 313 From the table we can see that 625 nm and 417 nm are in the visible portion of the electromagnetic spectrum. as shown in Figure 33-44. The distance y is measured from the center of the central-bright image. 2.Interference and Diffraction 3071 40 •• Two small loudspeakers are separated by 5. y θ L S1 d S2 Relate the distance Δy to the first minimum from the center of the central maximum to θ and the distance L from the speakers to the plane of the microphone: Interference minima occur where: tan θ = y ⇒ y = L tan θ L (1) d sin θ = (m + 1 )λ 2 where m = 0. Where does the microphone record the first minimum and the first maximum of the interference pattern from the speakers? The speed of sound in air is 343 m/s. A small microphone is placed a distance 1. 3.0 cm. 1. … Solve for θ to obtain: θ = sin −1 ⎢ ⎡ (m + 1 )λ ⎤ 2 ⎥ d ⎣ ⎦ Relate the wavelength λ of the sound waves to the speed of sound v and the frequency f of the sound: Substitute for λ in the expression for θ to obtain: Substituting for θ in equation (1) yields: λ= v f θ = sin −1 ⎢ ⎡ (m + 1 )v ⎤ 2 ⎥ ⎣ df ⎦ (2) ⎧ ⎡ (m + 1 )v ⎤ ⎫ 2 y = L tan ⎨sin −1 ⎢ ⎬ df ⎥ ⎭ ⎣ ⎦ ⎩ . and the microphone is then moved perpendicular to the axis. Picture the Problem The diagram shows the two speakers. the central-bright image and the first-order image to the left of the central-bright image. The speakers are driven in phase with a sine wave signal of frequency 10 kHz. We can apply the conditions for constructive and destructive interference from two sources and use the geometry of the speakers and microphone to find the distance to the first interference minimum and the distance to the first interference maximum.00 m away from the speakers on the axis running through the middle of the two speakers. S1 and S2. 10 mm: θ = sin −1 ⎜ ⎜ ⎛ 600 nm ⎞ ⎟ = 6. … ⎧ ⎡ mv ⎤ ⎫ y = L tan ⎨sin −1 ⎢ ⎥ ⎬ ⎣ af ⎦ ⎭ ⎩ For diffraction maxima.0 mm: sin θ = λ ⎛λ⎞ ⇒ θ = sin −1 ⎜ ⎟ a ⎝a⎠ ⎛ 600 nm ⎞ ⎟ = 0.010 mm: θ = sin −1 ⎜ ⎜ .010 mm.60 mrad ⎟ ⎝ 1.0 mm. 3. The first zeroes in the intensity occur at angles given by: (a) For a = 1. substitute numerical values and evaluate y: ⎧ ⎡ (1)(343 m/s ) ⎤ ⎫ y1st max = (1.00 m ) tan ⎨sin −1 ⎢ 2 ⎥ ⎬ = 37 cm ⎣ (5. and (c) 0.0 cm )(10 kHz ) ⎦ ⎭ ⎩ The maxima occur where: d sin θ = mλ where m = 1.0 mm ⎠ θ = sin −1 ⎜ ⎜ (b) For a = 0. Find the angle of the first diffraction minimum if the width of the slit is (a) 1.10 mm.10 mm ⎠ ⎛ 600 nm ⎞ ⎟ = 60 mrad ⎟ ⎝ 0. equation (2) becomes: Noting that the first maximum corresponds to m = 1.3072 Chapter 33 Noting that the first minimum corresponds to m = 0. 2.0 mrad ⎟ ⎝ 0. Picture the Problem We can use the expression locating the first zeroes in the intensity to find the angles at which these zeroes occur as a function of the slit width a.010 mm ⎠ (c) For a = 0. substitute numerical values and evaluate Δy: ⎧ ⎡ ( 1 )(343 m/s ) ⎤ ⎫ y1st min = (1.00 m ) tan ⎨sin −1 ⎢ ⎥ ⎬ = 94 cm ⎣ (5.0 cm )(10 kHz ) ⎦ ⎭ ⎩ Diffraction Pattern of a Single Slit 41 • Light that has a 600-nm wavelength is incident on a long narrow slit. (b) 0. the pulse is expanded so that it fills the aperture of a 6. 3.0 cm 43 ••• [SSM] Measuring the distance to the moon (lunar ranging) is routinely done by firing short-pulse lasers and measuring the time it takes for the pulses to reflect back from the moon. narrow slit of width 5. To send the pulse out.Interference and Diffraction 3073 42 • Plane microwaves are incident on the thin metal sheet that has a long. dtelescope L dmirror D Relate the diameter D of the beam when it reaches the moon to the distance to the moon L and the beam divergence angle θ : D ≈θ L (1) . What is the wavelength of the microwaves? Picture the Problem We can use the expression locating the first zeroes in the intensity to find the wavelength of the radiation as a function of the angle at which the first diffraction minimum is observed and the width of the plate. The first zeroes in the intensity occur at angles given by: Substitute numerical values and evaluate λ: sin θ = λ a ⇒ λ = a sin θ λ = (5. We can express the diameter of the beam at the moon as the product of the beam divergence angle and the distance to the moon and use the equation describing diffraction at a circular aperture to find the beam divergence angle. how large will the beam be when it reaches the Moon.00-in-diameter telescope. Assuming the only thing spreading the beam out is diffraction and that the light wavelength is 500 nm.82 × 105 km away? Picture the Problem The diagram shows the beam expanding as it travels to the moon and that portion of it that is reflected from the mirror on the moon expanding as it returns to Earth.0 cm )sin 37° = 3. The first diffraction minimum is observed at θ = 37º.0 cm in it. A pulse is fired from Earth. The microwave radiation strikes the sheet at normal incidence. 54 cm × 1 m ⎥ ⎢ in 10 2 cm ⎥ ⎣ ⎦ ( ) Interference-Diffraction Pattern of Two Slits 44 • How many interference maxima will be contained in the central diffraction maximum in the interference–diffraction pattern of two slits if the separation of the slits is exactly 5 times their width? How many will there be if the slit separation is an integral multiple of the slit width (that is d = na ) for any value of n? Picture the Problem We need to find the value of m for which the mth interference maximum coincides with the first diffraction minimum.22 λ d telescope Substitute for θ in equation (1) to obtain: D= 1. sinθ ≈ θ and: λ d telescope θ ≈ 1.22 Lλ d telescope Substitute numerical values and evaluate D: ⎡ ⎤ ⎢ ⎥ 1.00 in × 2.22(500 nm ) ⎥ = 1.53 km D = 3. Then there will be N = 2m − 1 fringes in the central maximum.22 The angle θ subtended by the first diffraction minimum is related to the wavelength λ of the light and the diameter of the telescope opening dtelescope by: Because θ << 1.82 × 10 8 m ⎢ ⎢ 6. The number of fringes N in the central maximum is: Relate the angle θ1 of the first diffraction minimum to the width a of the slits of the diffraction grating: Express the angle θm corresponding to the mth interference maxima in terms of the separation d of the slits: N = 2m − 1 (1) sin θ1 = λ a sin θ m = mλ d .3074 Chapter 33 sin θ = 1. how many bright interference fringes will be seen in the central diffraction maximum? Picture the Problem We can equate the sine of the angle at which the first diffraction minimum occurs to the sine of the angle at which the fifth interference maximum occurs to find a. (a) Find the width if the fifth interference maximum is at the same angle as the first diffraction minimum. We can then find the number of bright interference fringes seen in the central diffraction maximum using N = 2m − 1.Interference and Diffraction 3075 Because we require that θ1 = θm.100 mm = 20. The slits have a separation of 0. we can equate these expressions to obtain: Substituting for d and simplifying yields: Substitute for m in equation (1) to obtain: If d = na: d mλ λ = ⇒ m= d a a m= 5a =5 a N = 2(5) − 1 = 9 m= d na = = n and N = 2n − 1 a a 45 •• [SSM] A two-slit Fraunhofer interference–diffraction pattern is observed using light that has a wavelength equal to 500 nm. (a) Relate the angle θ1 of the first diffraction minimum to the width a of the slits of the diffraction grating: Express the angle θ5 corresponding to the mth fifth interference maxima maximum in terms of the separation d of the slits: Because we require that θ1 = θm5.0 μm 5 N = 2m − 1 = 2(5) − 1 = 9 . we can equate these expressions to obtain: Substituting the numerical value of d yields: (b) Because m = 5: sin θ1 = λ a sin θ 5 = 5λ d d 5λ λ = ⇒ a= d a 5 a= 0. (b) For that case.100 mm and an unknown width. How many interference fringes would you expect in the diffraction maximum adjacent to one side of the central diffraction maximum? Picture the Problem There are 8 interference fringes on each side of the central maximum. .20 mm ) − 1 = 39 0.20 mm. The number of fringes N in the central maximum is: Relate the angle θ1 of the first diffraction minimum to the width a of the slits of the diffraction grating: Express the angle θm corresponding to the mth interference maxima in terms of the separation d of the slits: Because we require that θ1 = θm. The secondary diffraction maximum is half as wide as the central one.010 mm 47 •• Suppose that the central diffraction maximum for two slits has 17 interference fringes for some wavelength of light. we can equate these expressions to obtain: Substitute for m in equation (1) to obtain: Substitute numerical values and evaluate N: N = 2m − 1 (1) sin θ1 = λ a sin θ m = mλ d mλ λ d = ⇒m = d a a N= 2d −1 a N= 2(0.010 mm and are separated by 0. We can then find the number of bright interference fringes seen in the central diffraction maximum using N = 2m − 1.3076 Chapter 33 46 •• A two-slit Fraunhofer interference–diffraction pattern is observed using light that has a wavelength equal to 700 nm. How many bright fringes will be seen in the central diffraction maximum? Picture the Problem We can equate the sine of the angle at which the first diffraction minimum occurs to the sine of the angle at which the mth interference maximum occurs to find m. It follows that it will contain 8 interference maxima. The slits have widths of 0. (a) The number of fringes N in the central maximum is: Relate the angle θ1 of the first diffraction minimum to the width a of the slits of the diffraction grating: Express the angle θm corresponding to the mth interference maxima in terms of the separation d of the slits: Because we require that θ1 = θm.Interference and Diffraction 3077 48 •• Light that has a wavelength equal to 550 nm illuminates two slits that both have widths equal to 0.15 mm ) −1 = 9 0. (a) How many interference maxima fall within the full width of the central diffraction maximum? (b) What is the ratio of the intensity of the third interference maximum to one side of the center interference maximum to the intensity of the center interference maximum? Picture the Problem We can equate the sine of the angle at which the first diffraction minimum occurs to the sine of the angle at which the mth interference maximum occurs to find m. we can equate these expressions to obtain: Substitute in equation (1) to obtain: N = 2m − 1 (1) sin θ1 = λ a sin θ m = mλ d mλ λ d = ⇒m = d a a N= 2d −1 a Substitute numerical values and evaluate N: (b) Express the intensity for a singleslit diffraction pattern as a function of the phase difference φ: N= 2(0. In (b) we can use the expression relating the intensity in a single-slit diffraction pattern to phase 2π constant φ = a sin θ to find the ratio of the intensity of the third interference λ maximum to one side of the center interference maximum.15 mm.030 mm and separations equal to 0. We can then find the number of bright interference fringes seen in the central diffraction maximum using N = 2m − 1.030 mm 2 ⎛ sin 1 φ ⎞ I = I0 ⎜ 1 2 ⎟ ⎜ φ ⎟ ⎝ 2 ⎠ 2π where φ = a sin θ λ (2) . 15 mm ⎠ 5 2 I 3 ⎛ sin 1 φ ⎞ 2 ⎟ =⎜ I0 ⎜ 1 φ ⎟ ⎝ 2 ⎠ ⎡ 1 ⎛ 6π ⎞ ⎤ sin ⎜ ⎟ I3 ⎢ 2 ⎝ 5 ⎠ ⎥ ⎥ = 0. y r E1 δ x r E r E2 The resultant of the two waves is of the form: r The magnitude of E is: r r E = E sin (ωt + δ ) i r E = (1) (2 A0 )2 + (3 A0 )2 = 3.030 mm ⎞ 6π ⎟= ⎟ ⎝ 0.3078 Chapter 33 sin θ 3 = 3λ d For m = 3: and φ= Substitute numerical values and evaluate φ: Solve equation (2) for the ratio of I3 to I0: Substitute numerical values and evaluate I3/I0: 2π λ a sin θ 3 = 2π ⎛ 3λ ⎞ ⎛a⎞ a⎜ ⎟ = 6π ⎜ ⎟ λ ⎝ d ⎠ ⎝d ⎠ φ = 6π ⎜ ⎜ ⎛ 0.98 rad ⎟ ⎝ 2 A0 ⎠ .25 =⎢ I 0 ⎢ 1 ⎛ 6π ⎞ ⎥ ⎢ 2⎜ 5 ⎟ ⎥ ⎣ ⎝ ⎠ ⎦ 2 Using Phasors to Add Harmonic Waves 49 • [SSM] Find the resultant of the two waves whose electric fields at a r ˆ given location vary with time as follows: E1 = 2 A0 sin ωt i and r ˆ E = 3 A sin (ωt + 3 π ) i . 2 0 2 Picture the Problem Chose the coordinate system shown in the phasor diagram. We can use the standard methods of vector addition to find the resultant of the two waves.6 A0 The phase angle δ is: δ = tan −1 ⎜ ⎜ ⎛ − 3 A0 ⎞ ⎟ = −0. We can use the standard methods of vector addition to find the resultant of the two waves.43 rad ⎣ 6. 6 Picture the Problem Chose the coordinate system shown in the phasor diagram.98 rad ) i (1) to obtain: 50 • Find the resultant of the two waves whose electric fields at a given r r ˆ ˆ location vary with time as follows: E1 = 4 A0 sin ωt i and E 2 = 3 A0 sin (ωt + 1 π ) i .Interference and Diffraction 3079 r Substitute for E and δ in equation r E = 3.08 A0 sin δ sin 120° r = r E2 E Applying the law of sines yields: Solve for δ to obtain: r ⎡ E 2 sin 120° ⎤ ⎥ δ = sin −1 ⎢ r ⎥ ⎢ E ⎦ ⎣ Substitute numerical values and evaluate δ: δ = sin −1 ⎢ ⎡ 3 A0 sin 120° ⎤ ⎥ = 0.6 A0 sin (ωt − 0.08 A0 ⎦ . r E y r E2 60° δ r E1 x The resultant of the two waves is of the form: Apply the law of cosines to the magnitudes of the scalars to obtain: r r E = E sin (ωt + δ ) i (1) r2 r 2 r 2 r r E = E1 + E 2 − 2 E1 E 2 cos120° or r E = r 2 r 2 r r E1 + E 2 − 2 E1 E 2 cos120° r r r Substitute for E1 and E 2 and evaluate E to obtain: r E = (4 A0 )2 + (3 A0 )2 − 2(4 A0 )(3 A0 )cos120° = 6. 100 mm. (b) For a screen distance of 1. 2.5 wavelengths. Let I0 be the intensity at the central maximum of the diffraction pattern on a distant screen. . What is the ratio if I to I0? Picture the Problem We can evaluate the expression for the intensity for a single-slit diffraction pattern at the second secondary maximum to express I2 in terms of I0. The distance from this second intensity maximum to the far edge of the slit is longer than the distance from the second intensity maximum to the near edge of the slit by approximately 2. (a) Show that the positions of the interference minima on a screen a large distance L away from the sheet that has the three equally spaced slits (spacing d. and a source spacing of 0. a light wavelength of 500 nm. . 8. 7. and let I be the intensity at the second intensity maximum from the central intensity maximum. that is. with d >> λ) are given approximately by y m = mλL 3d where m = 1. 4. 5.0162 ⎥ ⎥ ⎦ 2 52 •• Monochromatic light is incident on a sheet that has three long narrow parallel equally spaced slits a distance d apart.1A0 sin (ωt + 0. . 51 •• Monochromatic light is incident on a sheet with a long narrow slit (Figure 33-45). The intensity at the second secondary maximum is given by: ⎡ sin 1 φ ⎤ I ⎡ sin 1 φ ⎤ =⎢ 1 2 ⎥ I = I0 ⎢ 1 2 ⎥ ⇒ I0 ⎣ 2 φ ⎦ ⎣ 2φ ⎦ where 2π φ= a sin θ λ a sin θ = 2 2 At this second secondary maximum: 2π ⎛ 5λ ⎞ 5 λ and φ = ⎜ ⎟ = 5π λ ⎝ 2 ⎠ 2 Substitute for φ and evaluate I : I0 ⎡ ⎛ 5π sin⎜ I ⎢ ⎝ 2 =⎢ I 0 ⎢ 5π ⎢ 2 ⎣ ⎞⎤ ⎟⎥ ⎠ ⎥ = 0. calculate the width of the principal interference maxima (the distance between successive minima) for three sources.3080 Chapter 33 r Substitute for E and δ in equation r E = 6. . m is not a multiple of 3. 10.43 rad ) i (1) to obtain: Remarks: We could have used the law of cosines to find R and the law of sines to find δ.00 m. 4. 2. 6. 8.00 m ) = 3. m = 1. … (Note that m is not a multiple of 3. and a source .100 mm: 2 y min = 2(500 nm )(1. 2. (a) Show that the positions of the interference minima on a screen a large distance L away from four equally spaced sources (spacing d. (a) Express the phase angle δ in terms of the number of phasors N forming a closed polygon of N sides: For three equally spaced sources. m is not a multiple of 4. 5. 3d Substituting for Δr from equation (1) yields: (b) For L = 1. and d = 0. 6. … m = 1.7.00 m. 9. 5. 12. 2. with d >> λ) are given approximately by y m = mλL 4d where m = 1.7. 7. .) Express the path difference Δr in terms of sinθ and the separation d of the slits: Δr = d sin θ or. 3. provided the small angle approximation is valid. that is. 7. Applying a small angle approximation.00 m.33 mm 3(0. 6. .100 mm ) 53 •• [SSM] Monochromatic light is incident on a sheet that has four long narrow parallel equally spaced slits a distance d apart. … δ = m⎜ δ = m⎜ ⎛ 2π ⎞ ⎟ ⎝ 3 ⎠ (1) λ ⎛ λ ⎞ Δr = ⎜ ⎟δ = m 3 ⎝ 2π ⎠ m = 3. L yd ⇒ y = Δr Δr = d L y min = mλ L . . λ = 500 nm. . 10. 3. 2. 4.. 8..Interference and Diffraction 3081 Picture the Problem We can use phasor concepts to find the phase angle δ in terms of the number of phasors N (three in this problem) forming a closed polygon of N sides at the minima and then use this information to express the path difference Δr for each of these locations. the phase angle is: Express the path difference corresponding to this phase angle to obtain: Interference maxima occur for: Interference minima occur for: ⎛ 2π ⎞ ⎟ ⎝ N ⎠ where m = 1. 5. . 5 . (b) For a screen distance of 2. 9. we can obtain an expression for y that we can evaluate for enough of the path differences to establish the pattern given in the problem statement. 4. light wavelength of 600 nm. 6.7.100 mm. 4.00 m. 4d Substituting for Δr from equation (1) yields: (b) For L = 2. … m = 1. 5 .. m = 1. d = 0. 2. 7. calculate the width of the principal interference maxima (the distance between successive minima) for four sources. 8. L yd ⇒ y = Δr Δr = d L y min = mλL . … δ = m⎜ ⎛π ⎞ δ = m⎜ ⎟ ⎝2⎠ (1) λ ⎛ λ ⎞ Δr = ⎜ ⎟δ = m 4 ⎝ 2π ⎠ m = 3.. provided the small angle approximation is valid. Applying a small angle approximation. 3. 3. 6.00 m ) = 6. and n = 1: For two slits: 2 y min = 2(600 nm )(2. 5.) Express the path difference Δr in terms of sinθ and the separation d of the slits: Δr = d sin θ or.6. … (Note that m is not a multiple of 3. 4.00 mm 4(0.3082 Chapter 33 spacing of 0. 12. (a) Express the phase angle δ in terms of the number of phasors N forming a closed polygon of N sides: For four equally spaced sources. 9. λ = 600 nm. .. 5. the phase angle is: Express the path difference corresponding to this phase angle to obtain: Interference maximum occur for: Interference minima occur for: ⎛ 2π ⎞ ⎟ ⎝ N ⎠ where m = 1.100 mm ) 2(m + 1 )λL 2 d 2 ymin = . Compare this width with that for two sources with the same spacing. 9. 7. we can obtain an expression for y that we can evaluate for enough of the path differences to establish the pattern given in the problem statement.100 mm. 2. 2. Picture the Problem We can use phasor concepts to find the phase angle δ in terms of the number of phasors N (four in this problem) forming a closed polygon of N sides at the minima and then use this information to express the path difference Δr for each of these locations. in turn. 2. 3.100 mm The width for four sources is half the width for two sources. that. Picture the Problem We can use sin θ = λ a to find the first zeros in the intensity pattern. (a) Find the angular width of the of the central intensity maximum of the single-slit diffraction pattern on a distant screen.100 mm. d = 0.00 m. In (d) we’ll use a phasor diagram for a four-slit grating to find the resultant amplitude at a given point in the intensity pattern as a function of the phase constant δ. λ = 600 nm.0 mm 0. The four-slit interference maxima occur at angles given by d sin θ = mλ. … Substitute numerical values to obtain: θ m = sin −1 ⎢ = sin −1 (0. … . where m = 0. (b) Find the angular position of all interference intensity maxima that lie inside the central diffraction maximum.1. (c) Find the angular width of the central interference.Interference and Diffraction 3083 For L = 2. 54 •• Light of wavelength 480 nm falls normally on four slits.00 μm. That is.0800m ) ⎡ m(480 nm ) ⎤ ⎥ ⎣ 6. is a function of the angle θ that determines the location of a point in the interference pattern. and m = 0: 2 y min = (600 nm )(2. (d) Sketch the relative intensity as a function of the sine of the angle. In (c) we can use the result of Problem 53 to find the angular spread between the central interference maximum and the first interference minimum on either side of it.00 μm ⎠ ⎡ mλ ⎤ d sin θ = mλ ⇒ θ m = sin −1 ⎢ ⎦ ⎣ d ⎥ where m = 0.2. 1.00 μm ⎦ . (a) The first zeros in the intensity occur at angles given by: Substitute numerical values and evaluate θ : (b) The four-slit interference maxima occur at angles given by: sin θ = λ ⎛λ⎞ ⇒ θ = sin −1 ⎜ ⎟ a ⎝a⎠ θ = sin −1 ⎜ ⎜ ⎛ 480 nm ⎞ ⎟ = 242 mrad ⎟ ⎝ 2.00 m ) = 12. find the angle between the first intensity minima on either side of the central intensity maximum.00 μm wide and the center-to-center separation between it and the next slit is 6. Each slit is 2. 1.0800)] = ± 161mrad coincides with the first minimum in the diffraction pattern. 2.242 rad where θ3 will not be seen as it θ 2 = sin −1 [2(0.3084 Chapter 33 Evaluate θm for m = 0.0800)] = 0 θ1 = sin −1 [1(0.00 μm ) (d) Use the phasor method to show the superposition of four waves of the same 2π amplitude A0 and constant phase difference δ = d sin θ .0800)] = ± 80.1mrad θ 3 = sin −1 [3(0.0800)] = ±0. and 3: θ 0 = sin −1 [0(0. (c) From Problem 53: θ min = nλ 4d For n = 1: θ min = 480 nm = 20 mrad 4(6. λ α δ" A0 A φ A0 δ φ δ' δ" α A0 f δ δ A0 Express A in terms of δ ′ and δ ′′: Because the sum of the external angles of a polygon equals 2π: A = 2( A0 cos δ '' + A0 cos δ ' ) 2α + 3δ = 2π (1) . Note the excellent agreement with the results calculated in (a). (b) . The diffraction envelope was plotted using = 4 2 ⎜ 1 2 ⎟ .Interference and Diffraction 3085 Examining the phasor diagram we see that: Eliminate α and solve for δ '' to obtain: Because the sum of the internal angles of a polygon of n sides is (n − 2)π : From the definition of a straight angle we have: Eliminate φ between these equations to obtain: Substitute for δ '' and δ ' in equation (1) to obtain: Because the intensity is proportional to the square of the amplitude of the resultant wave: α + δ '' = π δ '' = 3 δ 2 3φ + 2δ '' = 3π φ −δ ' +δ = π δ' = 1δ 2 A = 2 A0 (cos 3 δ + cos 1 δ ) 2 2 I = 4 I 0 (cos 3 δ + cos 1 δ ) 2 2 2 The following graph of I/I0 as a function of sinθ was plotted using a spreadsheet ⎛ sin 1 φ ⎞ I program. φ= 2π a sin θ . where ⎜ φ ⎟ I0 ⎠ ⎝ 2 2 λ and (c). sin θ ≈ tan θ ≈ θ : sin θ ≈ tan θ = y L . Using the value of δ found in this fashion we can express the intensity at the point 1.72 cm from the central maximum. are illuminated at the central intensity maximum by a coherent light source of wavelength 550 nm.2 0. On the centerline.0 μm. The intensity is 50.0 mW/m2.3 55 ••• [SSM] Three slits.1 0 sin(theta) 0. (a) Draw a phasor diagram suitable for the addition of the three harmonic waves at that location.50 m from the slits. A screen is located 2. (b) From the phasor diagram.1 0. Picture the Problem We can find the phase constant δ from the geometry of the diagram to the right.2 -0.3 intensity diffraction envelope -0. calculate the intensity of light at that location. the amplitude of the resultant wave is 3 times that of each individual wave and the intensity is 9 times that of each source acting separately.3086 Chapter 33 18 16 14 12 10 I /I 0 8 6 4 2 0 -2 -0.72 cm from the centerline in terms of the intensity on the centerline. Consider a location 1. each separated from its neighbor by 60. y 1.72 cm θ L = 2.50 m (a) Express δ for the adjacent slits: δ= 2π λ d sin θ For θ << 1. The slits are extremely narrow. shown as the resultant R.72 cm from the centerline: Because I0 ∝ 9R2: I ∝ R2 I I R2 = ⇒ I= 0 2 I 0 9R 9 50.) 2 . A0 R = A0 A0 δ A0 (b) Express the intensity at the point 1.50 m ) 3π = rad = 270° 2 δ The three phasors. Note that they form three sides of a square. This intensity is given by I = I 0 ⎜ 1 2 ⎟ . their sum. Calculate the values of φ for the first three secondary maxima to one side of the central maximum by finding the values of φ for which dI/dφ is equal to zero. are shown in the diagram to the right.Interference and Diffraction 3087 Substitute to obtain: δ= 2πdy λL Substitute numerical values and evaluate δ : δ= 2π (60.56 mW/m 2 9 Substitute for I0 and evaluate I: 56 ••• In single-slit Fraunhofer diffraction.72 cm ) (550 nm )(2. 270° apart. Consequently.0 mW/m 2 I= = 5. equals the magnitude of one of the phasors.0 μ m )(1. ⎜ φ ⎟ ⎝ 2 ⎠ where φ is the phase difference between the wavelets arriving from the opposite edges of the slits. Check your results by comparing your answers with approximate values for φ of 3π. the intensity pattern (Figure 3311) consists of a broad central maximum with a sequence of secondary maxima to ⎛ sin 1 φ ⎞ either side of the central maximum. 5π and 7π. (That these values for φ are approximately correct at the secondary intensity maxima is discussed in the discussion surrounding Figure 33-27. n = 1.3088 Chapter 33 Picture the Problem We can use the phasor diagram shown in Figure 33-26 to determine the first three values of φ that produce secondary intensity maxima.94π At the three intensity minima φ = 2π.86π.92π. 5π. secondary intensity maxima occur where: φ = 3π φ = 4π φ = 5π φ = (2n + 1)π. 2..92π. and 7π. At the intensity maxima φ ≈ 3π. and the first three secondary intensity maxima are at φ = 3π .94π. . and 6. and 6π . Setting the derivative of Equation 33-19 equal to zero will yield a transcendental equation whose roots are the values of φ corresponding to the intensity maxima in the diffraction pattern. 3. . 4π.. Referring to Figure 33-26 we see that the first subsidiary maximum occurs where: An intensity minimum occurs where: Another intensity maximum occurs where: Thus.86π. and at the three intensity maxima φ = 2. and 7π The intensity in the single-slit diffraction pattern is given by: ⎛ sin 1 φ ⎞ I = I0 ⎜ 1 2 ⎟ ⎜ φ ⎟ ⎝ 2 ⎠ 2 Set the derivative of this expression equal to zero for extreme values (relative minima and maxima): ⎛ sin 1 φ ⎞ ⎡ 1 φ cos 1 φ − 1 sin 1 φ ⎤ dI 2 2 2 = 2I 0 ⎜ 1 2 ⎟ ⎢ 4 ⎥ = 0 for extrema 2 ⎜ φ ⎟ 1 dφ (2 φ ) ⎢ ⎥ ⎝ 2 ⎠⎣ ⎦ Simplify to obtain the transcendental equation: Solve this equation numerically (use the ″Solver″ function of your calculator or trial-and-error methods) to obtain: tan 1 φ = 1 φ 2 2 φ = 2. 4. 5π . and 6. 4. How far apart must the sources be for their diffraction patterns to be resolved by Rayleigh’s criterion? . D θ ymin L (a) The angle between the central maximum and the first diffraction minimum for a Fraunhofer diffraction pattern is given by: Substitute numerical values and evaluate θ : (b) Referring to the diagram.86% and that the agreement improves as n increases.22 λ D θ = 1.9%.83 cm 58 • Two sources of light that both have wavelengths equal to 700 nm are 10.54 mrad 0.6%. we see that: Substitute numerical values and evaluate ymin: θ = 1.54 mrad) = 6. 1.100 mm ⎟ ⎝ ⎠ ymin = L tanθ y min = (8.22 D the central maximum and the first diffraction minimum for a Fraunhofer diffraction pattern and the diagram to the right to find the distance between the central maximum and the first diffraction minimum on a screen 8 m away from the pinhole. (a) What is the angle between the central maximum and the first diffraction minimum for a Fraunhofer diffraction pattern? (b) What is the distance between the central maximum and the first diffraction minimum on a screen 8. Diffraction and Resolution 57 • [SSM] Light that has a wavelength equal to 700 nm is incident on a pinhole of diameter 0. and 0.Interference and Diffraction 3089 Remarks: Note that our results in (b) are smaller than the approximate values found in (a) by 4.100 mm.0 m away from the pinhole of Problem 57.00 m away? Picture the Problem We can use λ to find the angle between θ = 1.00 m ) tan (8.22⎜ ⎜ ⎛ 700 nm ⎞ ⎟ = 8. 54 cm 59 • Two sources of light that both have wavelengths of 700 nm are separated by a horizontal distance x.100 mm 8.22 L D D Substitute numerical values and evaluate Δy: Δy = 1. What is the smallest value of x for which the diffraction pattern of the sources can be resolved by Rayleigh’s criterion? Picture the Problem We can use Rayleigh’s criterion for slits and the geometry of the diagram to the right showing the overlapping diffraction patterns to express x in terms of λ.22 (700 nm )(10.22 ⇒ Δy = 1. They are 5. and the width a of the slit. L.0 m ) = 0.500 mm. Pinhole Δy αc L αc Rayleigh’s criterion is satisfied provided: Relate αc to the separation Δy of the light sources: Equate these expressions to obtain: α c = 1. αc αc x L .3090 Chapter 33 Picture the Problem We can apply Rayleigh’s criterion to the overlapping diffraction patterns and to the diameter D of the pinhole to obtain an expression that we can solve for Δy.00 m from a vertical slit of width 0. L Δy λ λL = 1.22 αc ≈ λ D Δy provided αc << 1. and the diameter D of your pupil. and x: For slits.Interference and Diffraction 3091 Referring to the diagram.22λ . Picture the Problem We can use Rayleigh’s criterion for circular apertures and the geometry of the diagram to the right showing the overlapping diffraction patterns to express L in terms of λ.500 mm 7. L. and x: For circular apertures. relate αc.0 mm. (b) Could you resolve these holes better using red light or using violet light? Explain your answer. (a) Using light that has a wavelength of 500 nm.22 ⇒ L = L D 1.00 m ) = 0. Rayleigh’s criterion is: αc ≈ αc = x L λ a Equate these two expressions to obtain: Substitute numerical values and evaluate x: λL x λ = ⇒x = L a a x= (700 nm )(5.22 λ D x λ xD = 1. Rayleigh’s criterion is: Equate these two expressions to obtain: αc ≈ x provided α << 1 L α c = 1. x.00 mm 60 •• The ceiling of your lecture hall is probably covered with acoustic tile. relate αc. how far could you be from this tile and still resolve these holes? Assume the diameter of the pupil of your eye is about 5. which has small holes separated by about 6. L.0 mm. Your pupil x L αc αc (a) Referring to the diagram. Suppose a double star were 4. The critical angle for resolution is proportional to the wavelength. Your pupil Δx αc αc L Rayleigh’s criterion is satisfied provided: Relate αc to the separation Δx of the light sources: Equate these expressions to obtain: α c = 1. Under ideal conditions. 61 •• [SSM] The telescope on Mount Palomar has a diameter of 200 in.54 cm ⎜ ⎟ 200 in × ⎜ ⎟ 1in ⎝ ⎠ . the holes can be resolved better with violet light which has a shorter wavelength.22 ⇒ Δx = 1.0 mm ) = 1.22 L D D Substitute numerical values and evaluate Δx: 15 ⎛ ⎛ ⎞⎞ ⎜ (550 nm )⎜ 4 c ⋅ y × 9.00 light-years away. the shorter the wavelength the farther away you can be and still resolve the two images. Thus.00 × 10 9 m Δx = 1.22 αc ≈ λ D Δx because αc << 1 L Δx λ λL = 1.3092 Chapter 33 L= Substitute numerical values and evaluate L: (6.0 mm )(5.22⎜ ⎟ 2.461× 10 m ⎟ ⎟ ⎜ ⎟⎟ 1c ⋅ y ⎜ ⎝ ⎠ = 5.22(500 nm ) 49 m (b) Because L is inversely proportional to λ. what must be the minimum separation of the two stars for their images to be resolved using light that has a wavelength equal to 550 nm? Picture the Problem We can use Rayleigh’s criterion for circular apertures and the geometry of the diagram to obtain an expression we can solve for the minimum separation Δx of the stars. Your pupil Δx αc D αc L Rayleigh’s criterion is satisfied provided: Substitute numerical values and evaluate D: α c = 1. … . 2. (a) At what angles in the first-order spectrum would you expect to find the two violet lines that have wavelengths of 434 nm and 410 nm? (b) What are the angles if the grating has 15 000 slits per centimeter? Picture the Problem We can solve d sin θ = mλ for θ with m = 1 to express the location of the first-order maximum as a function of the wavelength of the light.9 mm ≈ 1cm Diffraction Gratings 63 • [SSM] A diffraction grating that has 2000 slits per centimeter is used to measure the wavelengths emitted by hydrogen gas.22 λ αc ⎞ ⎛ ⎟ ⎜ 550 nm ⎟ D = 1. The angular separation between the two stars is 14 seconds of arc. What is the minimum diameter of the pupil that allows resolution of the two stars using light that has a wavelength equal to 550 nm? Picture the Problem We can use Rayleigh’s criterion for circular apertures and the geometry of the diagram to obtain an expression we can solve for the minimum diameter D of the pupil that allows resolution of the binary stars. (a) The interference maxima in a diffraction pattern are at angles θ given by: d sin θ = mλ where d is the separation of the slits and m = 0.22 λ D ⇒ D = 1.Interference and Diffraction 3093 62 •• The star Mizar in Ursa Major is a binary system of stars of nearly equal magnitudes.22⎜ ⎜ 14'' × 1° × π rad ⎟ ⎟ ⎜ 3600'' 180° ⎠ ⎝ = 9. 1. … d sin θ = mλ ⇒ λ = Relate the number of slits N per centimeter to the separation d of the slits: N= 1 d .3094 Chapter 33 Solve for the angular location θm of the maxima : Relate the number of slits N per centimeter to the separation d of the slits: Substitute for d to obtain: Evaluateθ for λ = 434 nm and m =1: θ m = sin −1 ⎜ 1 d ⎛ mλ ⎞ ⎟ ⎝ d ⎠ N= θ m = sin −1 (mNλ ) (1) θ1 = sin −1 [(2000 cm −1 )(434 nm )] = 86. 2.32 × 10–1 rad. 1. What are the wavelengths of these lines? Picture the Problem We can solve d sin θ = mλ for λ with m = 1 to express the location of the first-order maximum as a function of the angles at which the firstorder images are found. two other lines in the first-order hydrogen spectrum are found at angles of 9.72 × 10–2 rad and 1.9 mrad Evaluateθ for λ = 410 nm and m = 1: θ1 = sin −1 [(2000 cm −1 )(410 nm )] = 82.1 mrad (b) Use equation (1) to evaluateθ for λ = 434 nm and m = 1: Evaluate θ for λ = 410 nm and m = 1: θ1 = sin −1 [(15000 cm −1 )(434 nm )] = 709 mrad θ1 = sin −1 [(15000 cm −1 )(410 nm )] = 662 mrad 64 • Using a diffraction grating that has 2000 lines per centimeter. The interference maxima in a diffraction pattern are at angles θ given by: d sin θ m where d is the separation of the slits and m = 0. … θ = sin −1 ⎢ ⎡ mλ ⎤ ⎦ ⎣ d ⎥ Substitute numerical values and evaluate θ1: θ = sin −1 ⎢ ⎡ (1)(440 nm )⎤ ⎥ = 30.72 ×10–2 rad: Substitute numerical values and evaluate λ1 for θ 2 = 1. 2. At what angle will the first diffraction maximum occur for normally incident light diffracted by the butterfly’s wings? Assume the light is blue with a wavelength of 440 nm.0° ⎣ 880 nm ⎦ 66 •• A diffraction grating that has 2000 slits per centimeter is used to analyze the spectrum of mercury. In Part (b) we can apply the definition of the resolving power of the grating to find the width of the grating that must be illuminated for the lines to be resolved. (a) Find the angular separation in the first-order spectrum of the two lines of wavelength 579 nm and 577 nm.32 ×10–1 rad: λ= sin θ N sin 9. where m = 1.32 ×10−1 rad = 658 nm 2000 cm−1 ( ) 65 • The colors of many butterfly wings and beetle carapaces are due to effects of diffraction.72 ×10−2 rad λ1 = = 485 nm 2000 cm−1 ( ) λ1 = sin 1. 3.Interference and Diffraction 3095 Let m = 1 and substitute for d to obtain: Substitute numerical values and evaluate λ1 for θ1 = 9. The grating equation is: Solve for θ to obtain: d sin θ = mλ . (b) How wide must the beam on the grating be for these lines to be resolved? Picture the Problem We can use the grating equation to find the angular separation of the first-order spectrum of the two lines. The Morpho butterfly has structural elements on its wings that effectively act as a diffraction grating with spacing 880 nm. (a) Express the angular separation in the first-order spectrum of the two lines: Solve the grating equation for θ : Δθ = θ 579 − θ 577 θ = sin −1 ⎜ ⎛ mλ ⎞ ⎟ ⎝ d ⎠ . Picture the Problem We can use the grating equation to find the angle at which normally incident blue light will be diffracted by the butterfly’s wings. 3096 Chapter 33 Substitute for θ579 and θ577 to obtain: ⎤ ⎡ ⎤ ⎡ ⎢ m(577 nm ) ⎥ ⎢ m(579 nm ) ⎥ ⎥ = sin −1 [0.1154m] = 6. the wavelength of the light λ. 3. and the angle θ.. substitute numerical values and evaluate w: w= w= (578 nm )⎜ ⎜ ⎞ 1 ⎟ −1 ⎟ ⎝ 2000 cm ⎠ = 1mm 2 nm ⎛ 67 •• [SSM] A diffraction grating that has 4800 lines per centimeter is illuminated at normal incidence with white light (wavelength range of 400 nm to 700 nm). 2. describe the overlapping regions.1158m] − sin −1 [0. Picture the Problem We can use the grating equation d sin θ = mλ. How many orders of spectra can one observe in the transmitted light? Do any of these orders overlap? If so. to express the order number in terms of the slit separation d.63° = 0. .1154m] ⎥ − sin −1 ⎢ Δθ = sin −1 ⎢ 1 1 ⎥ ⎢ ⎥ ⎢ ⎢ 2000 cm −1 ⎥ ⎢ 2000 cm −1 ⎥ ⎦ ⎣ ⎦ ⎣ For m = 1: Δθ = sin −1 [0. m = 1.1158m] − sin −1 [0.02° (b) The width of the beam necessary for these lines to be resolved is given by: Relate the resolving power of the diffraction grating to the number of slits N that must be illuminated in order to resolve these wavelengths in the mth order: For m = 1: w = Nd (1) λ = mN Δλ N= λ Δλ λd Δλ Substitute for N in equation (1) to obtain: Letting λ be the average of the two wavelengths.65° − 6.. . 98. 2. The interference maxima in the diffraction pattern are at angles θ given by: The resolving power R is given by: d sin θ = mλ.98 700 nm mmax = 1 4800 cm −1 λmax Because mmax = 2. Express the condition for overlap: m1 λ1 ≥ m2 λ 2 One can see the complete spectrum for only the first and second order spectra. 3. … sin θ ≤ 1 ⇒ m ≤ d λ 1 4800 cm −1 = = 2. 2.0 cm2 has a resolution of 22 000 in the fourth order. only for m = 1 and 2. That is. 68 •• A square diffraction grating that has an area of 25. however. Because 700 nm < 2 × 400 nm.. there is no overlap of the second-order spectrum into the first-order spectrum.. one can see the complete spectrum only for m = 1 and 2. At what angle should you look to see a wavelength of 510 nm in the fourth order? Picture the Problem We can use the grating equation and the resolving power of the grating to derive an expression for the angle at which you should look to see a wavelength of 510 nm in the fourth order. (1) R = mN where N is the number of slits and m is the order number. there is overlap of long wavelengths in the second order with short wavelengths in the third-order spectrum. . 3. it must be true that: Evaluate mmax: d sin θ = mλ ⇒ m = d sin θ λ where m = 1. where m = 1. d= w N mw R Relate d to the width w of the grating: Substitute for N and simplify to obtain: d= .Interference and Diffraction 3097 The interference maxima in the diffraction pattern are at angles θ given by: If one is to see the complete spectrum. 2. 1.) Picture the Problem The distance on the screen to the mth bright fringe can be found using d sin θ = mλ (where d is the slit separation and m = 0.00 cm ⎞ 2 2 ⎜ ⎟ − m (589 nm ) 4000 ⎠ ⎝ 2 . … . and (c) the resolution in the first order. where N is the number of slits in the grating. The Fraunhofer diffraction pattern is projected onto a screen a distance of 1. (1) θ is also related to the distance to the screen L and the positions of the intensity maxima ym: Substituting for sin θ in equation (1) yields: Substituting numerical values yields: sin θ = ym 2 L + ym 2 dym 2 L2 + ym = mλ ⇒ ym = mλ L d 2 − m 2λ2 ym = m(589 nm )(1. the wavelength of the incident light λ.00-cm-square diffraction grating ruled with 4000 lines per centimeter.50 m from the grating by a 1. We can use θ min = λ Nd = Δy 2 L to find the width of the central maximum and R = mN.00 cm ⎣ ⎦ 69 •• Sodium light that has a wavelength equal to 589 nm falls normally on a 2. and the order number m according to: d sin θ = mλ where m = 0.50-m-focal-length lens that is placed immediately in front of the grating. to find the resolving power in the first order. 2. (a) The angle θ at which maxima occur is related to the slit separation d. 1.3098 Chapter 33 mw ⎛ Rλ ⎞ sin θ = mλ ⇒ θ = sin −1 ⎜ ⎟ R ⎝ w ⎠ Substitute for d in equation (1) to obtain: Substitute numerical values and evaluate θ : θ = sin −1 ⎢ ⎡ (22. (Assume the entire grating is illuminated.000)(510 nm ) ⎤ ⎥ = 13. Find (a) the distance of the first and second order intensity maxima from the central intensity maximum.50 m ) ⎛ 1. …) and the geometry of the grating and projection screen. (b) the width of the central maximum.0° 5. Interference and Diffraction 3099 Evaluate this expression for m = 1 and m = 2 to obtain: (b) The angle θmin that locates the first minima in the diffraction pattern is given by: y1 = 36. Express the width w of the grating as a function of the number of lines N and the slit separation d: The resolving power R of the grating is given by: Substitute for N in the expression for w to obtain: w = Nd R= λ λ = mN ⇒ N = Δλ m Δλ λd mΔλ w= . θ min = λ = Substitute numerical values and evaluate Δy: Δy = 2(1. what must be the width of the grating that is illuminated.4 μm (c) The resolving power R in the mth order is given by: Substitute numerical values and evaluate R: R = mN R = (1)(8000) = 8000 70 •• The spectrum of neon is exceptionally rich in the visible region. Because the resolution of the grating is a function of the average wavelength.50 m )(589 nm ) ⎛ ⎞ (8000 lines)⎜ 1 −1 ⎟ ⎜ 4000 cm ⎟ ⎝ ⎠ = 88.1cm Δy 2 Lλ ⇒ Δy = Nd Nd 2 L where Δy is the width of the central maximum. and the order number.322 nm.4 cm and y 2 = 80.313 nm and 519. If light from a neon discharge tube is normally incident on a transmission grating with 8400 lines per centimeter and the spectrum is observed in second order. we can express w in terms of these quantities. so that these two lines can be resolved? Picture the Problem The width of the grating w is the product of its number of lines N and the separation of its slits d. the difference in the wavelengths. Among the many lines are two lines at wavelengths of 519. 3100 Chapter 33 Letting λ be the average of the given wavelengths, substitute numerical values and evaluate w: 1 2 w= (519.313 nm + 519.322 nm )⎜ ⎜ ⎞ 1 ⎟ −1 ⎟ ⎝ 8400 cm ⎠ = 3 cm 2(519.322 nm − 519.313 nm ) ⎛ •• [SSM] Mercury has several stable isotopes, among them 198Hg and 202 Hg. The strong spectral line of mercury, at about 546.07 nm, is a composite of spectral lines from the various mercury isotopes. The wavelengths of this line for 198 Hg and 202Hg are 546.07532 nm and 546.07355 nm, respectively. What must be the resolving power of a grating capable of resolving these two isotopic lines in the third-order spectrum? If the grating is illuminated over a 2.00-cm-wide region, what must be the number of lines per centimeter of the grating? 71 Picture the Problem We can use the expression for the resolving power of a grating to find the resolving power of the grating capable of resolving these two isotopic lines in the third-order spectrum. Because the total number of the slits of the grating N is related to width w of the illuminated region and the number of lines per centimeter of the grating and the resolving power R of the grating, we can use this relationship to find the number of lines per centimeter of the grating. The resolving power of a diffraction grating is given by: Substitute numerical values and evaluate R: R= λ = mN Δλ 546.07532 546.07532 − 546.07355 (1) R= = 3.0852 × 10 5 = 3.09 × 10 5 Express n, be the number of lines per centimeter of the grating, in terms of the total number of slits N of the grating and the width w of the grating: From equation (1) we have: n= N w N= R m R mw Substitute for N to obtain: n= Interference and Diffraction 3101 Substitute numerical values and evaluate n: n= 3.0852 ×105 = 5.14 ×10 4 cm −1 (3)(2.00 cm) 72 ••• A diffraction grating has n lines per unit length. Show that the angular separation (Δθ ) of two lines of wavelengths λ and λ + Δλ is approximately 1 Δθ = Δλ − λ2 where m is the order number. 2 n m2 Picture the Problem We can differentiate the grating equation implicitly and approximate dθ /dλ by Δθ /Δλ to obtain an expression Δθ as a function of m, n, Δλ, and cosθ. We can use the Pythagorean identity sin2θ + cos2θ = 1 and the grating equation to write cosθ in terms of n, m, and λ. Making these substitutions will yield the given equation. The grating equation is: Differentiate both sides of this equation with respect to λ: d sin θ = mλ, m = 0, 1, 2, ... (1) d (d sin θ ) = d (mλ ) dλ dλ or dθ d cos θ =m dλ cos θ 1 dθ dθ = nm ⇒ n = cos θ m dλ dλ Because n = 1/d: Approximate dθ /dλ by Δθ /Δλ: n= 1 Δθ cos θ m Δλ nmΔλ cos θ Solving for Δθ yields: Δθ = Substitute for cosθ to obtain: Δθ = nmΔλ 1 − sin 2 θ mλ = nmλ d From equation (1): sin θ = Substituting for sinθ yields: Δθ = nmΔλ 1 − n 2 m 2λ2 3102 Chapter 33 Simplify by dividing the numerator and denominator by nm to obtain: Δθ = Δλ 1 1 − n 2 m 2λ2 nm = Δλ 1 − n 2 m 2λ2 n2m2 = Δλ 1 − λ2 2 2 nm 73 ••• [SSM] For a diffraction grating in which all the surfaces are normal to the incident radiation, most of the energy goes into the zeroth order, which is useless from a spectroscopic point of view, since in zeroth order all the wavelengths are at 0º. Therefore, modern reflection gratings have shaped, or blazed, grooves, as shown in Figure 33-45. This shifts the specular reflection, which contains most of the energy, from the zeroth order to some higher order. (a) Calculate the blaze angle φm in terms of the groove separation d, the wavelength λ, and the order number m in which specular reflection is to occur for m = 1, 2, . . . . (b) Calculate the proper blaze angle for the specular reflection to occur in the second order for light of wavelength 450 nm incident on a grating with 10 000 lines per centimeter. Picture the Problem We can use the grating equation and the geometry of the grating to derive an expression for φm in terms of the order number m, the wavelength of the light λ, and the groove separation d. (a) Because θi = θr, application of the grating equation yields: Because φ and θi have their left and right sides mutually perpendicular: Substitute for θi to obtain: Solving for φm yields: d sin (2θ i ) = mλ, where m = 0, 1, 2, ... (1) θ i = φm d sin(2φ m ) = mλ φm = 1 2 ⎛ λ⎞ sin −1 ⎜ m ⎟ ⎝ d⎠ ⎞ ⎟ ⎟ = 32.1° ⎟ ⎟ ⎠ (b) For m = 2: ⎛ ⎜ 450 nm −1 ⎜ 1 φ2 = 2 sin 2 1 ⎜ ⎜ 10,000 cm −1 ⎝ In this problem, you will derive the relation R = λ Δλ = mN (Equation 33-27) for the resolving power of a diffraction grating containing N slits separated by a distance d. To do this, you will calculate the angular 74 ••• Interference and Diffraction 3103 separation between the intensity maximum and intensity minimum for some wavelength λ and set it equal to the angular separation of the mth-order maximum for two nearby wavelengths. Picture the Problem We can follow the procedure outlined in the problem statement to obtain R = λ Δλ = mN . (c) Then for N slits. equals the angular separation of the interference maximum and the interference minimum given by the Part (c) result. the angular λ separation between an interference maximum and an interference minimum corresponds to a phase change of dφ = 2 π/N. (e) According nearly equal wavelengths differing by dλ is given by dθ = d cos θ to Rayleigh’s criterion. λ (a) Express the relationship between the phase difference φ and the path difference Δr: Because Δr = dsinθ : 2πΔr φ Δr ⇒φ= = 2π λ λ φ= 2πd λ sin θ (b) Differentiate this expression with respect to θ to obtain: Solve for dφ: dφ d ⎡ 2πd ⎤ 2πd = ⎢ λ sin θ ⎥ = λ cos θ dθ d θ ⎣ ⎦ dφ = 2πd λ cos θ dθ (c) From Part (b): dθ = λ dφ 2πd cos θ . (a) First show that the phase difference φ between 2π d the waves from two adjacent slits is given by φ = sin θ . two wavelengths will be resolved in the mth order if the angular separation of the wavelengths. (d) Next use the fact that the angle of Nd cos θ the mth-order interference maximum for wavelength λ is specified by d sin θ = mλ (Equation 33-26). Use this to arrive at R = λ Δλ = mN (Equation 3327) for the resolving power of a grating. (b) Next differentiate λ this expression to show that a small change in angle dθ results in a change in 2π d phase of dφ given by dφ = cos θ dθ . Compute the differential of each side of this equation to show that angular separation of the mth-order maximum for two m dλ . Use this to show that the angular separation dθ between the intensity maximum and intensity minimum for some wavelength λ is given by dθ = . given by the Part (d) result. m = 0. and that the Fraunhofer diffraction pattern from an opaque disk is the same as the pattern from an aperture of the same diameter.. d [d sin θ ] = d [mλ ] dλ dλ or dθ d cos θ =m dλ Solve for dθ to obtain: dθ = mdλ d cos θ = mdλ d cos θ (e) Equate the two expressions for dθ obtained in (c) and (d): Approximating dλ by Δλ and allowing for the possibility that Δλ < 0 yields: Solving for R = λ/Δλ yields: λ Nd cos θ λ Nd cosθ = m Δλ d cosθ R= λ = mN Δλ General Problems 75 • [SSM] Naturally occurring coronas (brightly colored rings) are sometimes seen around the Moon or the Sun when viewed through a thin cloud. 1.3104 Chapter 33 dθ = Substitute 2π/N for dφ to obtain: λ Nd cos θ (d) Equation 33-26 is: Differentiate this expression implicitly with respect to λ to obtain: d sin θ = mλ. or a traffic pole to safeguard your eyes. 2. Assume that the water droplets can be modeled as opaque disks with the same radius as the droplet. From this.) These coronas are due to diffraction of light by small water droplets in the cloud. a tree.) Picture the Problem We can use sin θ = 1.. be sure that the entire sun is blocked by the edge of a building. . . We’ll assume a wavelength of 500 nm. estimate the size of the water droplets in the cloud. A typical angular diameter for a coronal ring is about 10º.22λ D to relate the diameter D of the opaque-disk water droplets to the angular diameter θ of a coronal ring and to the wavelength of light. (This last statement is known as Babinet’s principle. (Warning: When viewing a sun corona. 33.8 nm ) = 0.59.00 μm ) = 6. typically of birch or pine.33)(5.65° 77 • Coronas (see Problem 74) can be caused by pollen grains.22)(632. Such grains are irregular in shape. Assuming that the water has an index of refractive equal to 1.Interference and Diffraction 3105 The angle θ subtended by the first diffraction minimum is related to the wavelength λ of light and the diameter D of the opaque-disk water droplet: Because of the great distance to the cloud of water droplets. θ << 1 and: Substitute numerical values and evaluate D: sin θ = 1.00-μm-diameter particles are illuminated by light from a helium–neon laser with wavelength in air of 632. The angle θ subtended by the first diffraction minimum is related to the wavelength λn of light in water and the diameter D of the microspheres: Because θ << 1: sin θ = 1. but they can be treated as if they had an average diameter of about 25 μm. What is the angular diameter (in degrees) of the corona for blue light? What is the diameter (in degrees) of the corona for red light? .22(500 nm ) = 3.22 λ D θ ≈ 1.22 λ nD Substitute numerical values and evaluate θ : θ≈ (1. uniform spheres made of plastic with an index of refraction equal to 1.22 λ nD θ ≈ 1. Polystyrene microspheres are small.116 rad (1.8 nm? Picture the Problem We can use sin θ = 1.22λ θ 1.5 μm π rad 10° × 180° 76 • An artificial corona (see Problem 75) can be made by placing a suspension of polystyrene microspheres in water. what is the angular diameter of such an artificial corona if 5.22 D= λ D ⇒D = 1.22 λn D = 1.22λn D to relate the diameter D of a microsphere to the angular diameter θ of a coronal ring and to the wavelength of light in water. the screen a distance L from the hair. What is the diameter of the hair? (The diffraction pattern of a hair with diameter d is the same as the diffraction pattern of a single slit with width a = d. and the central diffraction maximum is measured to be 14. We can use the geometry of the experiment to relate Δy to L and a and the condition for diffraction maxima to express θ1 in terms of the diameter of the hair and the wavelength of the light illuminating the hair.5° 78 • Light from a He-Ne laser (632. The angleα subtended by the first diffraction intensity minima is related to the wavelength λ of light and to the diameter D of the microspheres: D or.44(450 nm ) = 4.6 cm wide. See Babinet’s principle. The hair is mounted in a frame 7.6° Substitute numerical values and evaluate θ for blue light: θ blue ≈ 2.392 × 10 − 2 rad 25 μm = 2. λ sin 1 θ = 1.5 m from a wall. because α = 1 θ where θ is the 2 angular diameter of the coronal ring. sinθ ≈ θ and: θ ≈ 1.8 nm wavelength) is directed upon a human hair.22 2 D 1 2 sin α = 1.22λ D to relate the diameter D of a pollen grain to the angular diameter θ of a coronal ring and to the wavelength of light.44(650 nm ) = 6. We’ll assume a wavelength of 450 nm for blue light and 650 nm for red light.22 λ D ⇒ θ ≈ 2.) Picture the Problem The diagram shows the hair whose diameter d = a.22 λ Because θ << 1.344 × 10 − 2 rad 25 μm = 3. a θ1 L Δy . and the separation Δy of the first diffraction peak from the center.44 λ D Substitute numerical values and evaluate θ for red light: θ red ≈ 2.3106 Chapter 33 Picture the Problem We can use sin θ = 1. Problem 75. in an attempt to measure its diameter by examining the diffraction pattern. (a) Find the distance from the mirror to the first maximum. which is in the horizontal plane. the wave from the image is 180o out of phase with that from the source. due to reflection. (b) How many dark bands per centimeter are seen on the screen? Picture the Problem We can apply the condition for constructive interference to find the angular position of the first maximum on the screen. 3. The wavelength of the light is 600 nm.8 nm ) 2 ⎡ ⎛ 14. the distance from the mirror to the first maximum is given by: Express the condition for constructive interference: Solving for θ yields: y0 = Lθ 0 (1) d sin θ = (m + 1 )λ 2 where m = 0. 2. 2. … λ⎤ ⎡ θ = sin −1 ⎢(m + 1 ) ⎥ 2 d⎦ ⎣ θ 0 = sin −1 ⎢ ⎡λ ⎤ ⎣ 2d ⎥ ⎦ For the first maximum. m = 0 and: Substitute in equation (1) to obtain: ⎡λ ⎤ y 0 = L sin −1 ⎢ ⎥ ⎣ 2d ⎦ .Interference and Diffraction 3107 Relate θ to Δy: 1 2 tan θ = Δy ⎛ Δy ⎞ ⇒ θ = tan −1 ⎜ ⎟ L ⎝ 2L ⎠ Diffraction maxima occur where: a sin θ = (m + 1 )λ ⇒ a = 2 where m = 1. 1.00 m from the slit. narrow horizontal slit lies 1. Note that. The interference pattern produced by the slit and its image is viewed on a screen 1.5 m ) ⎟⎥ ⎟ ⎝ ⎠⎦ ⎣ = 98 μm 79 • [SSM] A long.6 cm ⎞⎤ sin ⎢ tan −1 ⎜ ⎜ 2(7. … (m + 1 )λ 2 sin θ Substituting for θ yields: a= (m + 1 )λ 2 ⎡ ⎛ Δy ⎞⎤ sin ⎢ tan −1 ⎜ ⎟⎥ ⎝ 2 L ⎠⎦ ⎣ Substitute numerical values and evaluate a for m = 1: a= (1 + 1 )(632. (a) Because y0 << L.00 μm above a plane mirror. by reflection from the surface of the lake. Hint: The interference is caused by the light reflecting off the lake and remember that this reflection will result in a 180º phase shift.00 m )sin −1 ⎢ ⎥ ⎣ 2(2. one coming directly from the galaxy and the other reflected from the surface of the lake. d = 2. The radio waves reflected from the surface of the lake are phase shifted 180°.33 m −1 (600 nm )(1.00 m ) n= 80 • A radio telescope is situated at the edge of a lake. The telescope is looking at light from a radio galaxy that is just rising over the horizon. Substitute numerical values and evaluate y0: ⎡ 600 nm ⎤ y 0 = (1.3108 Chapter 33 Because the image of the slit is as far behind the mirror’s surface as the slit is in front of it. relative to the radio waves reaching the telescope directly.00 μm ) ⎦ = 15.00 μm.1cm (b) The separation of the fringes on the screen is given by: The number of dark bands per unit length is the reciprocal of the fringe separation: Substitute numerical values and evaluate n: Δy = λL d n= 1 d = Δy λ L 2. We can use the condition for constructive interference of two waves to find the angle above the horizon at which the radio waves from the galaxy will interfere constructively. If the height of the antenna is 20 m above the surface of the lake. Radio waves directly from galaxy Telescope P θ e lak he t d θ ave f s re l ed ect fro m w Δr dio Ra θ . Picture the Problem The radio waves from the galaxy reach the telescope by two paths.00 μm = 3. at what angle above the horizon will the radio galaxy be when the telescope is centered in the first intensity interference maximum of the radio waves? Assume the wavelength of the radio waves is 20 cm. 22 λ D Substitute numerical values and evaluate αc: α c = 1.29° 81 • The diameter of the radio telescope at Arecibo.50. What should the minimum thickness of the material be for the material to be nonreflecting for light that has a wavelength 600 nm? Picture the Problem Note that reflection at both surfaces involves a phase shift of π rad.22⎜ ⎜ ⎛ 3. Puerto Rico. 2. λ = 600 nm π Air t π Coating Glass .00 × 10 rad ⎣ 20 m ⎦ Noting that m = 0 for the first interference maximum. Rayleigh’s criterion for resolution is: α c = 1. … sin θ ≈ Δr ⎡ Δr ⎤ ⇒ θ = sin −1 ⎢ ⎥ d ⎣d ⎦ Substitute for Δr to obtain: θ = sin −1 ⎢ ⎡ (m + 1 )λ ⎤ 2 ⎥ ⎣ d ⎦ ⎡ 1 (20 cm ) ⎤ −3 ⎥ = 5.30 is used as a nonreflective coating on the surface of glass that has an index of refraction of 1. is 300 m.2 cm ⎞ ⎟ = 0. substitute numerical values and evaluate θ0: θ 0 = sin −1 ⎢ 2 = 0. note that: Δr = (m + 1 )λ 2 where m = 0.13 mrad ⎟ ⎝ 300 m ⎠ 82 •• A thin layer of a transparent material that has an index of refraction of 1. What is the smallest angular separation of two objects that this telescope can detect when it is tuned to detect microwaves of 3. Hence we can use Rayleigh’s criterion to find the resolving power of the Arecibo telescope. 1.Interference and Diffraction 3109 Because the reflected radio waves are phase shifted by 180°. the condition for constructive interference at point P is: Referring to the figure.2-cm wavelength? Picture the Problem The resolving power of a telescope is the ability of the instrument to resolve two objects that are close together. We can apply the condition for destructive interference to find the thickness t of the nonreflective coating. and 633 nm.. half-silvered mirrors that face each other and are separated by a small distance a. there are gaps in the visible spectrum at 421. the transmitted light will have maximum intensity when 2a = mλ/cos θ. This path difference can be found using the geometry of the interferometer.30) 83 •• [SSM] A Fabry–Perot interferometer (Figure 33-47) consists of two parallel. mλ = 2a cos θ 2a = mλ cosθ 84 •• A mica sheet 1. m = 0. A half-silvered mirror is one that transmits 50% of the incident intensity and reflects 50% of the incident intensity. 2.20 μm thick is suspended in air. In reflected light. 1. 474. Show that when light is incident on the interferometer at an angle of incidence θ. Find the index of refraction of the mica sheet. a θ Express the path difference between the two rays that emerge from the interferometer: For constructive interference we require that: Equate these expressions to obtain: Solve for 2a to obtain: Δr = 2a cos θ Δr = mλ. For constructive interference in the transmitted light the path difference must be an integral multiple of the wavelength of the light.. . 542.3110 Chapter 33 The condition for destructive interference is: Solve for t to obtain: 2t = (m + 1 )λcoating = (m + 2 t = (m + 1 2 ) λair ncoating 1 2 ) λair 2ncoating Evaluate t for m = 0: t = (1 ) 2 600 nm = 115 nm 2(1. . Picture the Problem The Fabry-Perot interferometer is shown in the figure. 58 ⎟ ⎝ ⎠ 85 •• [SSM] A camera lens is made of glass that has an index of refraction of 1. 2. The purpose of this film is to produce zero reflection for light of wavelength 540 nm. the condition for destructive interference is: Solving for n yields: 2t = mλmica = m λair n . . (a) What minimum thickness of this film will accomplish its objective? (b) Would there be destructive interference for any other visible wavelengths? (c) By what factor would the reflection for light of 400 nm wavelength be reduced by the presence of this film? Neglect the variation in the reflected light amplitudes from the two surfaces. This lens is coated with a magnesium fluoride film (index of refraction 1. 3.60. Air Mica t Air π n Because there is a π rad phase shift at the first air-mica interface. we can use the condition for destructive interference to find the index of refraction n of the mica sheet. ..Interference and Diffraction 3111 Picture the Problem The gaps in the spectrum of the visible light are the result of destructive interference between the incident light and the reflected light. Treat the lens surface as a flat plane and the film as a uniformly thick flat film..38) to enhance its light transmission. m = 1. Noting that there is a π rad phase shift at the first air-mica interface.20 μm ) ⎟ = 1. n=m λair 2t (1) For λ = 474 nm: For λ = 421 nm: Equate these two expressions and solve for m to obtain: Substitute numerical values in equation (1) and evaluate n: 2t = (474 nm) m 2t = (421nm)(m + 1) m = 8 for λ = 474 nm ⎛ 474 nm ⎞ n = 8⎜ ⎜ 2(1. 1. 2 Air Film t Lens π π n (a) Express the condition for destructive interference between the light reflected from the air-film interface and the film-lens interface: Solving for t gives: 2t = (m + 1 2 )λfilm = (m + 1 ) λair 2 n (1) where m = 0.38) (b) Solve equation (1) for λair to obtain: Evaluate λair for m = 1: λair = 2tn m+ 1 2 2(97. because 180 nm is not in the visible portion of the spectrum.8 nm ⎝ 2 ⎠ 2(1. (c) Express the reduction factor f as a function of the phase difference δ between the two reflected waves: Relate the phase difference to the path difference Δr: Because Δr = 2t: f = cos 2 1 δ 2 (2) ⎛ Δr ⎞ δ Δr = ⇒ δ = 2π ⎜ ⎜λ ⎟ ⎟ 2π λfilm ⎝ film ⎠ δ = 2π ⎜ ⎜ ⎛ 2t ⎞ ⎟ ⎟ ⎝ λfilm ⎠ .3112 Chapter 33 Picture the Problem Note that the light reflected at both the air-film and film-lens interfaces undergoes a π rad phase shift. We can use the condition for destructive interference between the light reflected from the air-film interface and the film-lens interface to find the thickness of the film.83 nm = 97. 2.38) = 180 nm 1+ 1 2 λair = No.8 nm )(1. … t = (m + 1 2 ) λair 2n Evaluate t for m = 0: ⎛ 1 ⎞ 540 nm t =⎜ ⎟ = 97. In (c) we can find the factor by which light of the given wavelengths is reduced by this film from I ∝ cos 2 1 δ . express the angular width of the diffraction pattern: Equate these two expressions to obtain: 2θ = D D ⇒θ= L 2L θ diffraction = 1. Object Film D 2θ L Express the angular width of the a distant object at the film in terms of the diameter D of the pinhole and the distance L from the pinhole to the object: Using Rayleigh’s criterion.22 λ D λ D = 1. The optimum size of the pinhole for the sharpest possible image occurs when the spread due to diffraction equals the spread due to the geometric effects of the pinhole. Picture the Problem As indicated in the problem statement.83 nm ) ⎤ f 400 = cos 2 ⎢ ⎥ 400 nm ⎣ ⎦ = 0.38)(97.273 86 •• In a pinhole camera. As the pinhole is made smaller.0 cm and the wavelength of the light is 550 nm.22 ⇒ D = 2.Interference and Diffraction 3113 Substitute in equation (2) to obtain: ⎡ ⎛ 2t ⎞⎤ ⎡ 2π t ⎤ ⎟⎥ = cos 2 ⎢ f = cos 2 ⎢ 1 2π ⎜ 2 ⎥ ⎜λ ⎟ ⎝ film ⎠⎦ ⎣ λfilm ⎦ ⎣ ⎡ 2π nt ⎤ = cos 2 ⎢ ⎥ ⎣ λair ⎦ Evaluate f for λ = 400 nm: ⎡ 2π (1.44λL 2L D . we can find the optimal size of the pinhole by equating the angular width of the object at the film and the angular width of the diffraction pattern. Estimate the optimum size of the pinhole if the distance from the pinhole to the film is 10. the fuzziness due to geometry is reduced. the image is fuzzy because of geometry (rays arrive at the film after passing through different parts of the pinhole) and because of diffraction. but the fuzziness due to diffraction is increased. Picture the Problem We can use the geometry of the dots and the pupil of the eye and Rayleigh’s criterion to find the greatest viewing distance that ensures that the effect will work for all visible wavelengths. Use the wavelength of visible light that requires the greatest distance between dots.22 ⇒ L = L D 1. apply Rayleigh’s criterion to obtain: Set θ = αc to obtain: θ≈ d L α c = 1. Assume the pupil of the eye has a diameter of 3. Calculate the minimum viewing distance for this effect to work properly.22 λ D λ d Dd = 1. express the angle subtended by the adjacent dots: Letting the diameter of the pupil of the eye be D. in which his paintings are composed of small. Dots of paint d θ Pupil αc L Referring to the diagram.0 mm) = (1. The illusion of the colors blending together smoothly is produced in the eye of the viewer by diffraction effects.366 mm Substitute numerical values and evaluate D: 87 •• [SSM] The Impressionist painter Georges Seurat used a technique called pointillism.0 mm )(2.22λ L= Evaluate L for the shortest wavelength light in the visible portion of the spectrum: (3. each about 2. so that you are sure the effect will work for all visible wavelengths.44(550 nm )(10.3114 Chapter 33 D = 2.0 mm in diameter.0 cm ) = 0.0 mm.22)(400 nm ) 12 m . closely spaced dots of pure color.