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Optics



OPTICS


What is optics? Optics is a branch of physics. Its aim is the study of electromagnetic waves both from the visible part of the spectrum and from its neighbour regions: infrared and ultraviolet. The frequency spectrum and, respectively, the wavelength spectrum of electromagnetic waves are very large. The smaller observed frequency is 8 Hz. These electromagnetic waves, having frequency 8 Hz, are stationary wave formed between the Earth's surface and ionosphere. They are called Schumann resonances. The greater observed frequency is Hz. The electromagnetic waves, having this frequency, are gamma radiations generated by energetic process in universe. For example, the during the collapse of very massive stars, over 15 times more massive than our Sun, situated in distant galaxies, violent emissions of gamma radiation occur (called gamma-ray bursts) of huge energy in a time interval from one second to several minutes. The liberated energy in few seconds in such emission is greater than the energy liberated by the Sun in its all life, more than 10 billion years. Gamma-ray bursts are the most powerful explosions known. The bursts we detect today originated far away billions of years ago, before the Earth formed. Since, between the wavelength and frequency there is the relation:




(1)


the spectrum of electromagnetic waves in universe, both on frequency scale and on wavelength scale, is:

Hz (2)


  (3)



The spectrum of optics, from ultraviolet to infrared, is defined as follows (Fig.1):



Fig.1 Frequency spectrum and wavelength spectrum of optics


Fig. 2. An electromagnetic plane wave propagates in direction of wave vector . During this propagation, the two vectors, the intensity of electric field, , and the magnetic induction, , oscillate perpendicular each other and perpendicular on the direction of displacement. The electric field,, oscillates in the vertical plane and the magnetic induction, , oscillates in the horizontal plane. On consider that the sensation of light is given by the electric field,


What is light? In order to answer this question we must to take into account the light's dual character wave-particle. There are some experiments, like the photoelectric effect, the Compton effect, that can be explained if on consider that the light is formed by particles called photons. Others experiments, like interference, diffraction, polarization, can be explained if on consider that the light is an electromagnetic wave. Therefore, the light can be perceived either as a flux of photons, either as an electromagnetic wave, i.e., an electric field and a magnetic field propagating in space (Fig.2). While, light as photons is studied in geometrics optics, light as an electromagnetic wave is investigated in wave optics.

What are the physical mechanisms of light emission? How the emission of the electromagnetic waves or photons can be explained? Today, there are many possible mechanisms proposed to explain the emission of electromagnetic waves or photons, hence the emission of the light.

First, in classical physics, can be show, that any charged particle having an accelerated motion, is a source of electromagnetic waves, i.e., the electromagnetic waves will be emitted by any charged particle moving accelerated. Let us denote by q the charge of a particle and by a its acceleration. Then, according to classical physics, the radiated power is proportional to the square of the charge and the square of its acceleration .

A first example is the oscillatory motion of a charged particle, like is the case of the alternative current having the frequency Hz from the line system. The electrons oscillate with Hz. The oscillatory motion is always an accelerated motion, therefore, low frequency, , electromagnetic waves will be emitted by the electrons.

A second example is the X-ray tube. This is an evacuated bulb with two electrodes: a indirect heated cathode and an anode made by a metal with a high melting temperature (like tungsten, platinum). A voltage V is applied between these two electrodes (Fig.3). The electrons, emitted by the indirect heated cathode, are accelerated by the applied high voltage and the anode will be bombarded by the electrons.The kinetic energy of the electrons arriving at anode will be . Upon getting into the substance of the anode, a part of the electrons will undergo solid hits with the atoms of the anode and will be rapidly decelerated and almost all their kinetic energy will be emitted instantly in form of an energetic pulse of electromagnetic waves, called X-rays. Another part of the electrons will undergo glancing collisions with the atoms of the anode and first they will produce excitations and ionisations of the atoms in anode, losing their energy a little at a time, then they will make also sollid hits with the atoms of the anode. Again, the kinetic energy of decelerated electrons will be emitted as X-rays. This radiation is called bremsstrahlung radiation and its spectrum is continous. It must be noted that X-rays having a discrete spectrum and called characteristic radiation also exist, but they are not emitted by the electrons penetrating into anode. This characteristic radiation is due to excitation of the internal electron shells of the anode. The maximum frequency of the electromagnetic waves (bremsstrahlung radiation) emitted by the electrons penetrating into anode is determined as follows:

   (4)

hence

(5)



Fig.3 X-ray tube. A voltage V is applied between anode and cathode.


Obviously, depending on the voltage applied between anode and cathode, the maximum frecquency of radiation emitted by the electrons can be situated in the visible part of the spectrum, in ultraviolet, in X-rays or in gamma rays. For example, if the values of the applied voltage are in the range U =1,6-3,0 V, the maximum frecquency of radiation emitted will be in the visible part of the spectrum Hz). For values U =10-100 V, the maximum frecquency of radiation emitted will be in ultraviolet ( Hz), for values V, the maximum frecquency of radiation emitted will be in X-rays domain ( Hz) and for V, the maximum frecquency of radiation emitted will be in gamma rays domain ( Hz).

A third example is the case of a non-relativistic electron moving along the X-axis with the velocity and the acceleration . In this case, can be show, that the spatial distribution of the electromagnetic radiation emitted by electron has the form of a lobe having cylindrical symmetry, the maximum of the emitted electromagnetic energy being oriented on a direction perpendicular to the direction of the accelerated motion of the electron (Fig.4).

A forth example is the case of a relativistic electron moving along the X-axis with the velocity and the acceleration . The electromagnetic radiation emitted by electron has also the form of a lobe having cylindrical symmetry, the maximum of the emitted electromagnetic energy being oriented on a direction more close to the direction of the accelerated motion of the electron as the velocity of the electron is more close to velocity of light (Fig.5).


Fig.4 The spatial distribution of the electromagnetic radiation emitted by an non-relativistic electron moving with the acceleration . The maximum of the emitted electromagnetic energy is oriented on a direction perpendicular to the direction of the accelerated motion of the electron.


Fig. 5 The spatial distribution of the electromagnetic radiation emitted by an relativistic electron moving with the acceleration . The maximum of the emitted electromagnetic energy is oriented on a direction more close to the direction of the accelerated motion of the electron as the velocity of the electron is more close to velocity of light.

A fifth example is the case of electromagnetic radiation emitted by an oscillating dipole. Let us assume that the mass of the positive charge is so large that the positive charge can be considered as imobile and only the negative charge oscillates around the positive charge. In this case, the spatial distribution of the electromagnetic radiation emitted has a form similar with that emitted by a non-relativistic charged particle moving with the acceleration other than zero (Fig 6). Like before, the accelerated charged particle does not emit radiation on the direction of the accelerated motion. It must be noted that in the case of a non-relativistic charged particle moving with the acceleration , the electric field created by this particle at great distances , varies proportional as and also proportional with the projection on of the particle's acceleration at an anterior moment equal with .


Fig. 6 The spatial distribution of the electromagnetic radiation emitted by an oscillant dipole. The direction of the oscillation and hence of the accelerated motion coincide with the direction of the dipole moment . The maximum of the emitted electromagnetic energy is oriented on a direction perpendicular to the direction of the accelerated motion.


Second, it is known that every time when an electron jumps from an excited state to a stationary orbit of lower energy, a photon will be emitted by the electron. Let us consider that a hydrogen atom in the fundamental state (the state of minimum energy) is collided by another particle and then goes to an excited state, i.e. the electron will jump to another orbit more distanced from the nucleus. In this excited state the electrons remains only a time s , then he jumps to a lower energy orbit, the difference of energy of two orbits being emitted as a photon, i.e. as an elementary electromagnetic wave (Fig.7). The time interval, s, when the electron is on the stationary excited orbit, moving around the nucleus, is very small for us but great enough for the electron. Indeed, we know that the electron's velocity on the first Bohr's orbit is about , where is the light's velocity in the vacuum. Therefore, in the time interval s, the number of the electron's rotations around the nucleus is about .

Fig. 7 The emission of a photon or of an elementary electromagnetic wave during the jump of the electron from a excited state to a lower energy state.


Third, the electromagnetic radiation can be emitted by a charged particle moving with a constant velocity in a medium, if the particle's velocity is greater that the light' velocity in the given medium. This is the Vavilov-Cerenkov effect. Pavel Cerenkov and Sergei Vavilov, for discovery of this effect, were awarded the Nobel Prize for physics. Also Igor Tamm and Ilya Frank, for its theoretical explanation, were awarded the Nobel Prize for physics too. In 1934, the soviet physicist Pavel Cerenkov, working under the supervision of physicist Serghei Vavilov, has observed an glow of a liquid under the action of radium gamma rays. Vavilov put forth the hypothesis that this radiation is emitted by the rapid electrons generated at interaction between gamma radiation and the liquid. As is known, while in vacuum the velocity of light is m/s, in a certain medium, like water, whose refractive index is n, the velocity of light will be . The explanation of this effect is based on the interaction wave-particle. The electrons whose velocity is will overtake the light wave and will push in the wave's wall, giving energy to the wave. The wave's amplitude will increase this meaning a waves emission by electrons (Fig. 8). The colour of the Vavilov-Cerenkov radiation is light blue. Wavefront of the emitted Cerenkov radiation propagates on a direction perpendicular to the surface of the cone whose axis coincide with the direction of charged particle's velocity (Fig. 9).

Fig. 8. Wave-particle interaction. The electrons whose velocity is will overtake the light wave and will push in the wave's wall, giving energy to the wave. The wave's amplitude will increase this meaning a waves emission by electrons.



Fig. 9 The Vavilov-Cerenkov radiation is emitted by the electrons moving in a liquid with a constant velocity , greater than the phase velocity of the light in the medium(). Wavefront of the Cerenkov emitted radiation propagates on a direction perpendicular to the surface of the cone whose axis coincide with the direction of charged particle's velocity. The angle between the direction of radiation's propagation and the velocity vector of the charged particle is defined by relation .



The angle between the direction of radiation's propagation and the velocity vector of the charged particle is determined by the relation:

(6)

Fourth, the electromagnetic radiation can be emitted during the transformation of the substance in field, when an electron and an positron, moving very slow one relative to another, meet and annihilate, their energy being liberated in form of two quanta of radiation. The inverse of this process is known as pair production.


(7)


Fifth, the electromagnetic radiation can be emitted when a charged particle cross the separation surface of two media, like the interface metal-vacuum. The explanation in this case is the reciprocal annihilation between the charged particle and its image in the metal, when the charged particle cross the interface metal-vacuum.

Planck' Quantum Hypothesis. In 1900, the german physicist Max Planck, trying to explain the blackbody radiation, made the nonclassical assumption that the emission of the electromagnetic waves is quantized. Therefore the radiation is not emitted in continous amounts but in discrete packets of energy, now called quanta or photons.

The photon. The particle of light or the the photon, is characterized by momentum and energy. The photon's energy is

(8)

where Js is the Planck constant, and n is the frequency.

The energy of the photon is defined as

(9)

where m is the mass of the moving photon (the rest mass of the photon is zero).

Therefore, the momentum of the photon is

(10)

where (11)

is the wavelength.

The photoelectric effect. The photoelectric effect refers to the emission of electrons from a substance, like an metal, when this substance is under the action of an electromagnetic radiation whose frequency is high, greater than a certain value (Fig. 10). This efffect was discovered in 1887 by the german physicist Heinrich Hertz. The explanation of the photoelectric effect was given in 1905 by Albert Einstein, who was awarded the Nobel Prize for physics. Einstein unfold Planck's ideea from 1900, related to the quantized emission of electromagnetic waves. In 1905 Einstein assumed that not only the emission of the electromagnetic waves but also their absorption is quantized in form of energy quanta called photons. In this way, Einstein succeeds to explain the two, experimental established, laws of photoelectric effects According to the first law, the increase of the monochromatic radiation's intensity falling on the surface of a metal determine an increase of the number of the emitted photoelectrons but their kinetic energy do not depend upon the light intensity. The second law shows that the kinetic energy of the emitted electrons depends upon the radiation's frequency. For frequencies greater than a certain threshold frequency, the kinetic energy of the emitted electrons increases with the increase of radiation's frequency The explanation given by Einstein is a simple one. It is known that the free electrons in the metal can be considered that are located inside a potential well (Fig. 11).


Fig. 10 The photoelectric effect. When a photon flux falls upon the surface of a cathode, having the energy, from this cathode the electrons are emitted, moving to the anode and creating a current of photoelectrons. Evidence for this current is given by the current meter placed on the external circuit.



Fig.11 When the electrons are in the metal they can be considered that are located inside a potential well. In order to get outside from the metal, the electrons must receive energy. In this case the energy is received by photon's absorption.



The depth of this potential well is equal with the work function, and its value depends on the type of metal. For most of the metals the work function value is between 1 and 5 eV. When an electromagnetic radiation (or a photon flux) is sent on the surface of a metal, a free electron from near to the metal's surface can to absorb a photon. A part of the photon's energy will be used to bring the electron to the surface of the metal, and the remaining energy will be given to the free electron in form of kinetic energy. Therefore, we can write:

(12)

This is Einstein's relation for the photoelectric effect. L is the work function of the metal, h is Planck's constant, n is the radiation's frequency, m is the mass of the electron and is its velocity.

Compton effect In 1923 A. H. Compton performed the following experiment: he has sent a beam of X-rays at a block of graphite and measured, for different angles to the incident beam, the dependence of the intensity of scattered X-rays on their wavelength (Fig. 12). Compton found two maxima of scattered X-rays. The first maximum corresponds to the wavelength l, of the incident X-rays, and the second corresponds to a greater wavelength . The difference is called Compton displacement and depends on the scattering angle. In order to explain the results of this experiment, Compton considered the X-rays beam like flux of photons interacting with the free electrons located in the block of graphite.



Fig. 12. The Compton experiment.


Starting from the collision between an electron and a photon Compton has theoretically found an expression for the displacement , the theoretical value of the displacement being in good keeping with the experimental data. For this experiment, considered as a new experimental evidence for the corpuscular nature of radiation, Compton was awarded the Nobel Prize for physics. In Fig. 13 the collision between a photon and an electron at rest placed in the origin of the coordinate system is illustrated.





Fig. 13 The collision between a photon and a free electron at rest.

Before the collision, the photon's energy is , his momentum is , the electron's energy is and his momentum is zero. After collision the photon's energy is and his momentum is , the electron's energy is and his momentum is .

The laws of conservation of energy and momentum can be written as follows:


(13)


(14)


(15)


where is the rest mass of the electron, and


(16)


is the moving electron mass. The equations (14) and (15) represent the conservation of the momentum on the X-axis and Y-axis. Since, the wavelength has the form


(17)


result that both the energy and the momentum can be written as


(18)


Taking into account (16), (17) and (18), result that the relations (13), (14) and (15) can be written as follows:


(19)


    (20)


(21)


We have a system of three equations with five unknowns (). Eliminating the unknowns and , the following relation between variables and is obtained:


(22)


where is Compton displacement.

Interference of light. Interference refers to the superposition in a space region of two or many separate waves, leading to emergence of a new wave, called resultant wave, whose amplitude depends on the phase difference between the initial waves. Let us consider the simple case when the interference of two separate waves of small intensity is investigated. In this case, the superposition principle is valid, i.e., when many separate vector waves of small intensity arrive simultaneously at a point in space, the resultant vector wave is the vector sum of the separate vector waves. In order that the interference of two light waves to exist, the following four conditions must be satisfied:

a) both waves must to have the same frequency;

b) the planes of the oscillations generated by the two waves must coincide;

c) the two waves must be coherent, i.e., their phase difference must be independent of time.

d) the optical path difference between the two waves must be smaller than a certain value, called interference length, since the emission of light radiation is quantized in form of wave trains. The emission's duration of an atom, jumping from an excited state to a lower energy state is about s. The interference length represents the length of a wave train in vacuum, i.e., the trip of light in s. It is given be relation: m.

As a result of light waves interference a redistribution of the waves' energy in space is realized, leading to the emergence of alternating regions of maximum and minimum of intensity, called the dark and bright interference fringes.

Because the emission's process is random, in order that the optical path difference between the two waves must be smaller the interference length, the two separate waves that interfere must be emitted by the same light source. For example, this is the case of interference of two waves, one emitted by a light source and another emitted by the image of this light source in a mirror (Fig. 14).


Fig. 14 Interference of two light waves generated by a source and its image in a mirror.


Let us consider now the interference of two coherent light waves emitted by two point sources and . Let us assume that both waves have the same frequency and arrive simultaneously at a point P in space. Let us denote by and the distances from the two light sources to the point P (Fig. 15). If the point P is located far away from the two sources, then on can suppose that the waves emitted by two sources propagate along the same direction. Let us denote by


, (23)




Fig. 15 Interference of two light waves generated by the sources and .


the oscillations of the electromagnetic field generated by this sources in and respectively in . Let us assume that these oscillations will propagate as plane light waves with the finite velocity to the point P, where new oscillations of the electromagnetic field will be generated, having the form:

(24)

and respectively

(25)


where is the phase velocity of light in the given medium and is the refractive index of the medium.

The resultant oscillation of the electromagnetic field in the point P can be derived using the superposition principle:


   (26)

The amplitude of this oscillation will be


(27)

where

(28)

is the phase difference between the two waves at the point P.

Taking into account that , we have


(29)

or

(30)

where is the wavelength in vacuum.

Now, denoting by the difference in optical path, we get


(31)


From relation (31) result that if the optical path difference is equal to an integer number of wavelength in a vacuum:

(32)


then the phase difference is a multiple of , hence . In this case the oscillations generated by the two waves in the point P will be in phase, and in this point a maximum of interference will be observed. The resultant amplitude will be .

If the optical path difference is equal to a half-integral number of wavelength in a vacuum:


(33)


then and In this case the oscillations generated by the two waves in the point P will be in counterphase, and in this point a minimum of interference will be observed. The resultant amplitude will be .

Vector diagram. In order to derive the amplitude of the resultant oscillation, the vector diagram method can be used. Denoting

(34)

and respectively

(35)

the relations (24) and (25) become


(36)

and respectively

(37)


In vector diagram method (Fig. 16), each of above two oscillations is depicted graphically as a vector having the amplitude and respectively, the angle between the direction of this vector and X-axis being equal to and respectively . The resultant oscillation will be depicted graphically too, using the rule of vector addition, as a vector having the amplitude A, making the angle with X-axis, Since the projection of the resultant amplitude, A, on the X-axis and respectively Y-axis, must be equal to the sum of projections of amplitudes and respectively on these axes, on obtain:


(38)

(39)

Fig. 16 The addition of two oscillations using the vector diagram method.


Taking the square of relations (38) and (39) and summing, on obtain:


(40)


Since

(41)

results

(42)


where, in this case, is the phase difference between the two waves. .

In the case when the two waves are not coherent, the phase difference will be a function of time and the time-averaged value of will be zero:


. (43


Therefore, taking the time-average of the relation (42), on obtain


(44)


In the case of a homogeneous medium, the wave's intensity is proportional to the square of amplitude:

(45)


Therefore, in the case of the interference of two incoherent waves, the resultant intensity is equal to the sum of the intensities of the two waves:


(46)


In the case of the interference of two coherent waves, the resultant intensity will be


(47)

The term

(48)


is called the interference term. The interference only exists if this interference term, (48), is other than zero.

The interference of light waves can be classified in interference of waves with non-localized fringes in space and interference of waves with localized fringes in space. In the later case, the interference fringes occur in the all region where the superposition of light waves occurs.

Interference of light waves with non-localized fringes in space An example of such an interference is the Young's double slit-experiment. The Young's device contains a monochromatic light source, S, a first screen with two closely spaced slits and a second screen. The distance between the two screens is denoted by D and the distance between two slits, and placed on the same vertical line, is denoted by l (Fig. 17). When the light wave emitted by the source S, arrives to the two slits localized on first screen, then according to the Huygens's principle, the two slits become coherent secundary light sources, and the two waves emitted will interfere at the point M from the second screen. Obviously, due to the symmetry, at the pointa maximum of interference will be observed. This maximum is called central maximum. Let us denote by d the distance between M and At the point M a maximum of interference will be observed when the path difference between the two light waves is an integer number of wavelength and respectively a minimum when the path difference is an half-integral number of wavelength.

Fig. 17 Interference of light waves with non-localized fringes in space. Young's device.


From Fig. 17, it is easy to see that the path difference between the two light waves has the form :

(49)


For small values of the angle , we can write


(50)

or, since

(51)


result that the path difference has the form:


(52)


The optical path difference will be



At the point M a maximum of interference will be observed if , hence


(53)

or

(54)

where .

Similarly, at the point M a minimum of interference will be observed if , hence

(55)


The distance between two subsequent maxima has the form


(56)


For small values of the angle , as defined by (50), the interference fringes have the form of eqhidistant parallel straight lines, symmetric distributed relative to.

Interference of light waves with localized fringes in space. This type of interference is also called interference of light reflected from thin plates, since it is realized using transparent thin plates, or thin films. In this case the interference fringes are observed in a certain plane from the region where the superposition of light waves is realized. Interference of light reflected from thin plates can be classified in interference with fringes of equal inclination and interference with fringes of equal thickness.

Interference with fringes of equal inclination. Let us consider a transparent plate with parallel surfaces and let us denote the plate's thickness by h. Also let us denote by n the refractive index of the substance of the plate for a monochromatic radiation whose wavelength is . Let us denote by the refractive index of the medium where the thin plate is placed. On suppose that . An example could be a thin glass plate in air.


Fig. 1 Interference with fringes of equal inclination.


As is know, a monochromatic plane light wave can be considered as a parallel beam of monochromatic light rays. If such a monochromatic light ray is directed on the plate's surface, under a certain angle of incidence, the plate will reflects upward two coherent rays and . The incident ray undergoes both a reflection from the upper surface of the plate and a refraction when enters the plate. The incident ray partly reflected from the upper surface of the plate is denoted by . The remainder of the incident ray after a refraction when enters the plate, undergoes either a second refraction and leaves the plate through the bottom surface or a reflection from the bottom surface and then a refraction when leaves the plate through the upper surface. This second ray is denoted by (Fig. 1). Therefore, the interference can be observed either in the region above the plate, being generated by the reflected rays either in the region below the plate, being generated by the transmitted rays. The rays and fall exactly upon each other, are parallel and interfere at infinity. Using two convergent lenses and , the interference fringes, generated by the two rays and , can be observed at the points and respectively. The optical path difference between the two rays is


(1)


where is the optical path of the ray , and is the optical path of the ray. The term appearing in relation (1) can be justified as follows: in optics, can be show that as often as a light ray undergoes a reflection at the interface of two media of different densities, coming from the less dense medium, a path difference equal to will appear. In the above case the path difference of is introduced by the ray at the point A. Since


(2)

result

(3)

hence

(4)


Since, according to the refraction laws

(5)

result

(6)


hence (7)


All rays falling under the same angle of incidence on the surface of a thin plate will have the same optical path difference and will give a dark or bright fringe. The interference fringes are circles and are called the Haidinger's rings. They can be observed both in reflected light and in transmitted light.

Interference with fringes of equal thickness. This interference can be obtained using a plate having plane surfaces and a variable thickness like is a wedge. In this case the optical path difference between the rays interfering only depends on the plate thickness. An example of such interference is given by the Newton's rings. On a thin glass plate having plane-parallel surfaces, a convergent plane-convex lens is placed, whose refractive index is (Fig. 2). Between the glass plate and the convergent plane-convex lens is a variable thickness air layer. Let us consider two rays and directed perpendicular on the plane surface of the convergent lens. They interfere at the point C, and the interference image can be observed either in reflected light either in transmitted light. Due to the cylindrical symmetry, a dark or bright ring should be seen at the point C. The optical path difference between the two rays will be

(8)

where is the optical path of the ray , and is the optical path of the ray. In this case, since the optical path difference is introduced by the ray at the point B, we get


(9)


In the case of normal incidence, when , on can write


Fig. 2 Fringes of equal thickness. Newton's rings.


(10)


Since for air the refractive index is , result


(11)


The bright rings (maxima of intensity) will be observed when


(12)

hence

(13)


From Fig. 2 can be see that if is the radius of k-th ring, then we can write


(14)


where R is the radius of the sphere (the radius of lens). Since , result


(15)


From (13) and (15) result that the radius of k-th bright ring we can write


(1


The radius of the sphere will be

(17)

Similarly for dark rings (minima of intensity) we get


(18)


and the expression for the radius of the sphere will be


(19)



Diffraction of light Diffraction refers to the phenomenon of light's deviation from the straight line propagation and entrance in the region of geometrical shadow, appearing when the light encounter an obstacle whose dimensions are comparable with the wavelength of the light. This phenomenon can easy be explained using the Huygens-Fresnel principle. According to this principle, each element of a wave surface is a secondary source of spherical waves, their amplitude being proportional to the area of the considered surface element. There are two types of diffraction: Fraunhofer diffraction and Fresnel diffraction. If the rays of the incident beam are parallel, diffraction is called Fraunhofer diffraction. If the rays of the incident beam are divergent, diffraction is called Fresnel diffraction.

Fraunhofer diffraction at a single slit. Let us consider a plane light wave falling on a slit of width b , the surface of the plane wave being parallel to the plane of the slit. Let us assume that this slit is split in a large number of infinitely small slits of equal thickness dx. According to the Huygens-Fresnel principle, each of this elementary slits of thickness dx will become secondary sources of elementary waves. Let us denote by q the diffraction angle. For small values of the diffraction angle on can suppose that the amplitudes of oscillations coming from different elementary slits are equal each other (Fig.1).

Fig.1 Fraunhofer diffraction at a single slit.

The secondary wave, emitted by the first elementary slit (the bottommost portion of the slit), propagating along ray, has the equation


(1)


The secondary wave, emitted by the elementary slit placed at distance x from the first elementary slit, propagating along ray, has the equation


(2)


where is the wave's velocity and is the path difference between this two waves.

The equation of the resultant wave owing to the diffraction is obtained by summing the secondary waves generated by each elementary slit and has the form


(3)


since and , equation (3) can be written as:


(4)


Integrating we get:


(5)


since


(6)


equation (5) becomes


 (7)



Therefore the wave's amplitude is


(8)


and the wave intensity will be


(10)


Denoting

(11)


relation (10) becomes

   (12)


where . Maxima of resultant intensity are obtained from condition


(13)

hence

(14)


and

(15)


It is easy to see that u = 0 is a solution of equation (15). In this case on obtain , because for u = 0. This maximum, , is called zeroth order maximum. The remaining maxima, called k-th maxima where , are determined in a first approximation by equation , hence they are obtained for . For example, for , , for , , for , , etc. These maxima of intensity correspond to bright fringes. Dark fringes (minima of intensity) are determined by equation , hence they are obtained for , where . Therefore, as a result of diffraction of light a redistribution of the waves' energy in space is realized, leading again, like in case of the interference, to the emergence of alternating regions of maximum and minimum of intensity, called the dark and bright diffraction fringes.


Fig. 2 Fraunhofer diffraction at a single slit. The diffraction pattern.

In order that the Fraunhofer diffraction at a single slit to be observed, a convergent lens parallel to the plane of slit must be used. In this case the diffraction pattern can be observed on a screen placed at a distance from the lens equal to the focal distance of the lens (Fig. 2).

Fraunhofer diffraction at two slits. Let us consider two slits having the same width , and let us denote by the sum between the width of a slit and the distance between the two slits (Fig. 3). Also, we shall assume that the resultant wave diffracted by the first slit propagates along the ray and the resultant wave diffracted by the second slit propagates along the ray . The path difference between the two waves is .




Fig. 3 Fraunhofer diffraction at two slits.



The equation of the wave diffracted by the first slit, obtained before in the case of Fraunhofer diffraction at a single slit, has the form


(16)

or

(17)

where

(18)

The equation of the wave diffracted by the second slit will be


(19)


According to the superposition principle, the equation of the resultant wave will be


(20)

hence

(21)


Since

(22)


equation (21) becomes


(23)


The intensity of the resultant wave will be

(24)

or

(25)


The expression for the intensity of the resultant wave obtained in the case of Fraunhofer diffraction at two slits is similar to that obtained in the case of Fraunhofer diffraction at a single slit given by de (12), but differs by the factor


(26)


This factor corresponds to the interference between the coherent waves emitted by the two slits. This interference is modulated by the diffraction at a single slit, according to the factor

   

appearing in the expression of the resultant intensity (25).

The interference maxima are given by


(27)

or

(28)


The diffraction minima are given by


(29)

or

(30)


Fraunhofer diffraction at N parallel slits. The diffraction grating. Let us consider a set of N slits having the same width, , and let us denote by the sum between the width of a slit and the distance between the two slits. The quantity is called the grating constant. In this case can be show that the intensity of resultant wave is

   (31)

where

(32)


It is easy to see that for the expression (31) coincides with that given by (25). The factor

   (33)


corresponds to the interference between the coherent waves generated by the N slits. This interference is modulated by the diffraction at a single slit.

The diffraction minima are given by

or


The maxima of interference are given by

(34)

or

(35)


where . The minima of interference are given by


(36)

or

(37)

Since for the values , the relation (30) coincides with relation (28) defining the maxima of interference, result that the minima of interference, given by (30), are obtained for the followings values of (the values must be excluded)

(38)

The maxima of interference given by (28) are called principal maxima. According to (37) and (38), between two principal interference maxima interference minima exist. Between two interference minima a single maximum exist. These maxima are called secondary maxima. Therefore, between two principal maxima there are minima and secondary maxima.

Polarization of light. In wave optics the light is an electromagnetic wave, i.e., an electric and magnetic field propagating in space, the directions of oscillation of these fields laying in two planes perpendicular to the direction of wave's propagation and perpendicular each other. On believe that the sensation of light is given by the electric field vector. Polarization of light refers to the direction of the electric field's oscillations during of propagation of light wave. So, if during the wave propagation, the oscillations of the electric field take place along a single direction in a plane perpendicular to the direction of wave's propagation, then on say that the light is plane-polarized. But, if the oscillations of the electric field rapidly change their direction so that they take place almost simultaneously along many directions in a plane perpendicular to the direction of wave's propagation, on say the light is unpolarized. The plane where the electric field vector oscillates is called the oscillation plane (this is the plane determined by the direction of the electric field and the direction of wave's propagation) and the plane perpendicular on the oscillation plane is called the plane of polarization.

Let us assume that the xy-plane is the oscillation plane and let us denote byand the components of the electric field. Because, these components can oscillate independently at a definite frequency, the resultant electric field will be determined by the superposition of and oscillations. If these oscillations are in phase then the electric field oscillates on a straight line and light is linearly-polarized, but if these oscillations are out of phase then the electric field vector moves around an ellipse or a circle in a plane perpendicular on the direction of wave's propagation which propagates along with the wave. In this case, the light is elliptically-polarized or, respectively, circular-polarized and the polarization can be dextrogyrate or levogyrate, depending if the rotation of the electric field take place to the right or the left. Therefore, a plane-polarized light can be a linearly-polarized light or an elliptically-polarized light, respectively, a circular-polarized light.

The light coming from the sun or from a neon light bulb in the room is seen by us as unpolarized light although in the moment of emission it is linear polarized. The explanation is a simple one. Let us consider the simplest atom, the hydrogen atom, in the fundamental state (state of the minimum energy). Let us assume that after a collision, the atom jumps to an excited state, i.e. the electron jumps to an orbit more distanced from the nucleus. In this state the electron will remains only a short time interval, about s, then he will return to a stationary orbit more close to nucleus, and the difference of energy between the two states will be liberated in form of a quantum of radiation, i.e., by emission of a photon. Obviously, the emitted photon is polarized. Let us assume that to each emitted polarized photon a linearly-polarized elementary electromagnetic wave corresponds, whose electric field oscillates on a given direction. If a large number of atoms exist, each s another linearly-polarized elementary wave will be emitted, the direction of the electric field being different each time. The maintenance interval of an image on the human eye retina is about 0.01 seconds. In this time interval, on the retina arrive and remain "images" of many polarized photons having different polarization. Therefore the light will be perceived as unpolarized. We are unable to detect the rapid variations of elementary waves' polarization, whose polarization change every s. We have assumed that in the case of linearly-polarized wave the wave's polarization refers to the direction of oscillation of the electric field.

How the polarized light can be obtained? There are many methods to obtain total or partly polarized light. A first method uses the refraction and the reflection of light. If on the interface between two dielectric media, an unpolarized light ray is directed under a certain angle, other than zero, then the reflected and refracted rays will be partly polarized, i.e., in the reflected ray the oscillations of the electric field component perpendicular to the incidence plane will predominate while in refracted ray the oscillations of the electric field component parallel to the incidence plane will prevail. For example in the reflected ray 90% of electric field oscillations could be perpendicular to the incidence plane and 10% parallel. As is known, the incidence plane is the plane determined by the incident ray and the normal to the interface between two media (Fig. 1). For a value of the incidence angle, given by relation , the reflected ray is completely polarized and the degree of polarization of the refracted ray reaches is its maximum value. The angle is called Brewster's angle.

A second method refers to the existence of substances that polarize the light, known as polaroids or polaroid filters. An example of polaroid is the cellophane. Polaroids are made from complex long molecules parallel placed on the direction of their long axes. These molecules transmit only the light waves whose polarization direction is parallel to their long axes but strongly absorb the light waves whose polarization direction is perpendicular on the direction of their long axes. Therefore it is an absorption polarization. When an unpolarized light wave passes through such a polaroid, the transmitted light wave will be linearly-polarized, its oscillation plane being parallel to the direction of long axes of molecules (Fig. 2), while its polarization plane is perpendicular to this direction. In other words only light waves whose electric field oscillates parallel to direction defined by the long axes of molecules will pass. The polaroids can be used to analyse if the light emitted by different sources is polarized or unpolarized. If the incident light is polarized then the tramsmitted light intensity will vary when the polaroid is rotated. Because the reflected light from nonmetal surfaces is often partly polarized, the sun glass having polaroid lenses have the polarization axis on vertical direction.

Fig. 1 The use of the refraction and the reflection of light to obtain a polarized light



Fig. 2 The use of substances that polarize the light, known as polaroids or polaroid filters to obtain a polarized light.


A third method is known double refraction or birefringence. Double refraction appears in anisotropic crystals, where the velocity of the light propagation, hence the refractive index too, depend on the direction of propagation in crystal. In any anisotropic crystal, one or two directions exist, called the optical axes of the crystal. Along these axes the phenomenon of double refraction does not exist. An example is the anisotropic crystal of Iceland calcite (). This crystal has the property that if an unpolarized light ray is send perpendicular to the plane surface of a thin plate of this crystal, along a direction which differs from the direction of optical axis of the crystal, it will split into two plane-polarized rays, one that is not deviated from the normal, called ordinary ray and another that is deviated from the normal, called extraordinary ray. This phenomenon is called double refraction or birefringence and was discovered by Erasmus Bartholinus in 1669. While, in the ordinary ray, the oscillations of the electric field vector are perendicular to the principal plane of the crystal, in the extraordinary ray, the oscillations of the electric field vector are in principal plane of the crystal (the principal plane of the crystal is the plane determined by direction of the incident ray and direction of the


Fig. 3 Double refraction or birefringence


optical axis of crystal). If the incident beam is narrow enough and the crystal is thick enough, the two emergent rays, the ordinary ray and the extraordinary ray, will be parallel (Fig. 3). While, the ordinary ray propagates through crystal with the same speed in all directions, the extraordinary ray travels with different speeds in different directions. The two emergent rays transmitted by the crystal, the ordinary ray and the extraordinary ray, are very close each other. In order to separate these rays, hence to obtain polarized light, a Nicol prism can be used. Let us consider an anisotropic crystal of Iceland calcite This is a rhombohedron crystal, its longitudinal right section being a parallelogram, whose length is about three times greater than his width. This crystal is cut in half along his small diagonal, and the two halves are cemented together with a material called Canada balsam (Fig. 4). When on his surface an unpolarized light ray is send, it will split into two plane-polarized rays, one that is not deviated from the normal, called ordinary ray and another that is deviated from the normal, called extraordinary ray. Because for the crystal of Iceland calcite, the values of the refractive index are for the ordinary ray and for the extraordinary ray, and the refractive index of the Canada balsam is , result that , hence, the ordinary ray will be totally internally reflected, and the crystal will transmit only the extraordinary ray, which is a plane-polarized ray. Therefore, an unpolarized light ray is sending on the surface of crystal and the light emerging from the crystal is polarized. This device is called a Nicole


Fig. 4 Nicol prism


prism. This device is also called a polarizer, i.e., a device used to obtain a plane-polarized light wave. A device used to analyze a polarized light is called analyzer, for example a rotating Nicole prism can be used as an analyzer. In order to understand the how the polarizer and analyzer work, let us consider a mental experiment. Let us assume that a cord oscillates in the vertical plane and let us suppose that perpendicular to the direction of oscillations' propagation is placed a plane having a vertical oriented rectangular opening, placed on the direction of cord's oscillations, whose high is greater than the cord's oscillations amplitude. Obviously, the cord's oscillations will pass through this opening beyond the plane. But if perpendicular to the direction of oscillations' propagation is placed, at a certain distance, a second plane having a horizontal oriented rectangular opening, the cord's oscillations will not pass. But if this second plane is rotated with 90 degrees, the rectangular opening will be again in vertical plane and oscillations will pass through this opening. The first plane having a vertical oriented rectangular opening can be use as a polarizer. The second plane having a horizontal oriented rectangular opening can be used as an analyzer. If we image that many cords exist, oscillating in different planes, after the first plane only the vertical oriented cord's oscillations will pass, after the second plane no oscillation will pass, but if this second plane is rotated with 90 degrees oscillations will pass beyond the plane. An example of a pair of polarizer and analyzer consisting of polaroid filters is illustrated in Fig. 5.


Fig. 5. A pair of polarizer and analyzer consisting of polaroid filters


Rotation of the plane of polarization. There are certain substances, called optically active substances, having the property of turning of the plane of polarization of a light wave as it travels through them. This phenomenon was discovered by Arago in 1811 in case of quartz crystals and is known as natural rotatory polarization, since the presence of an external magnetic field is not required. In 1815, Biot shown that the liquid solutions of certain substances are optically active too. An example of an optically active substance is the sugar solution. A possible application of the polarization of light could be the determination of the concentration of a sugar solution. When a linear polarized light ray pass through a tube filled with a sugar solution, the oscillating plane of the electric field will be rotated with an angle a. This angle can be determined using an analyzer, hence the concentration will be given by relation , where is the specific rotation power () and l is the length of the tube filled with sugar solution.

Magnetic rotation of the plane of polarization. In 1846 Faraday discovered that even a substance that is not optically active, but is under the action of an external magnetic field, will rotate the oscillating plane of the electric field of a linearly-polarized light ray, if the linearly- polarized light ray travel the substance along a direction that coincide with the direction of the external magnetic field. The rotation angle of the oscillating plane of the electric field is determined by relation:

(39)


where R is called the Verdet's constant or the rotatory magnetic power, l is the length of the layer of substance traveled and B is magnetic induction in substance. Magnetic rotation of the plane of polarization is also known as Faraday effect.


Thermal radiation

1. What is the thermal radiation?

The emission of electromagnetic waves by any body at a temperature greater than zero Kelvin is called thermal radiation. Obviously, the intensity of thermal radiation will depend on the temperature of the emitting body, being higher at high temperatures. At the room temperature the thermal radiation is emitted by the bodies in the invisible part of the spectrum, beyond the infrared radiation. When a metal is heated at high temperatures, a thermal radiation is emitted in the visible part of the spectrum, the light color varying from red to white, corresponding to the metal's temperature. For example, incandescent lamps emit yellow light when heated up to 3000. The thermal radiation is also emitted at low temperatures, lower than the room temperature, but the thermal energy carried by this radiation is very small.

2. What is the physical mechanism of the thermal radiation's emission?

The emission of the thermal radiation can be explained as follows: When the temperature of a body is increassed, the kinetic energy of thermal (chaotic) motion of the atoms of the body, will increasse too. Therefore, a transition of the atoms in excited states of higher energies can be realized. The thermal radiation is emitted when the atoms of the body return from these excited states to other lower energies states. Also, when the atoms of a body are thermally agitated, their motion will be accelerated. These atoms contain charges that are therefore thermally accelerated. Hence the thermal radiation is also emitted by the charged particles, like positive ions or negative electrons of the body, having an accelerated motion.

3. The spectrum of the thermal radiation.

Any body is a source of thermal radiation and also absorbs thermal radiation from the neighbour bodies, so that at equilibrium the energy of emitted radiation will be equal with that of absorbed radiation. Such a radiation is called the equilibrium thermal radiation. The spectrum of equilibrium thermal radiation is a continuum spectrum. The dependence of the spectral emitted power on the wavelength has a single maximum, whose position and value depend on the temperature (Fig 1)

Fig. 1

where is spectral emissive power of a blackbody, is the wavelength of the thermal radiation and is the temperature of blackbody.

The emission and the absorption of the equilibrium thermal radiation are characterized by the spectral emissive power and respectively by the spectral absorption power. The energy of the emitted thermal radiation per unit time per unit area of radiating surface of a body, at temperature T, in all directions, in the frequency interval from n to n+dn is called spectral emissive power .This is given by

(1)


where dW is the energy of the emitted thermal radiation per unit time per unit area of radiating surface in the frequency interval from n to n+dn.

The energy of the emitted thermal radiation per unit time per unit area of radiating surface of a body, at temperature T, in all directions, in the frequency interval from 0 to , that is for all the frequencies, is called total emissive power . It is denoted by is defined as follows

(2)


The quantity describing the capacity of a body to absorb the incident radiation at a given frequency is called spectral absorption power. It is denoted by, and is defined as follows:

(3)


Therefore, the spectral absorption power represents the fraction of the energy dWinc, delivered in unit time to unit area of the body surface by incident electromagnetic waves with frequencies from n to n+dn, that is absorbed by the body.

The fraction of the energy dWinc, delivered in unit time to unit area of the body surface by incident electromagnetic waves with frequencies from 0 to , that is for all the frequencies, that is absorbed by the body is called total absorption power . It is denoted by AT and is defined as follows

(4)


The blackbody is an ideal body that can absorb all the radiations falling on him. By example, a small orifice on the surface of a sphere covered on interior with soot black, can be considered, in a first approximation, as a blackbody. When a ray of light goes into the sphere through this orifice, it is reflected many times and also partly absorbed by the walls of the sphere, so that the probability to go out is very close to zero.

If is spectral emissive power of a blackbody, then total emissive power of a black body, eT, will be

(5)

Because

, (6)


and taking into account that spectral emissive power of a blackbody is also denoted by, then total emissive power of a blackbody, eT, can also be written as


(7)



Laws of the blackbody radiation

1. Kirchhoff Law

The Kirchhoff's law of the thermal radiation, established by Kirchhoff in 1859, states that the ratio between the spectral absorption power and spectral emissive power, at the same temperature and for the same frequency of the thermal radiation, is the same for all bodies, being an universal function of temperature and radiation's frequency. This ratio is equal to the spectral emissive power of a blackbody at that same temperature. The the spectral absorption power of a blackbody being equal to the unity.

The Kirchhoff radiation law may be written as


(1)



Since for the real bodies , result that . Therefore the spectral emissive power, of a blackbody is greater than of any bodie at the same temperature, T.

2. Stefan-Boltzmann Law

In 1879, Josef Stefan, physicist professor at Viena University, has studied experimentally the dependence of the energy of the thermal radiation emitted by a heated body on temperature. He finds that the total thermal energy emitted per unit time per unit area of radiating surface of a body is proportional to the four power of its absolute temperature. The empirical law discovered by Stefan was not confirmed by the subsequent measurements. The Stefan empirical law was corrected by Boltzmann, a former student of Stefan. In 1884 Boltzmann, using the laws of thermodynamics, has theoretically demonstrated that total thermal energy emitted per unit time per unit area of radiating surface of a blackbody is proportional to the four power of its absolute temperature. Therefore, the empiric law discovered by Stefan was not valid for all bodies but only for the blackbody. Mathematically, the Stefan-Boltzmann law, has the form

(2)


where s, is a constant, called the universal Stefan-Boltzmann constant. For a blackbody, the experimentally established value of this constant is


. (3)

3. Wien's Displacement Law

Before 1880, it was known, on the evidence of the experimentally obtained curves of the blackbody radiation of Fig. 2, that the dependence of the spectral emitted power on the wavelength has a single maximum, whose position and value depend on the temperature.

In 1893, using the principles of thermodynamics, Wien established a law, known today as Wien's Displacement law. He has found that as the temperature of any blackbody increases, the curve retains its general shape, but the maximum of the curve increases and the maximum of the curve shifts to smaller wavelengths. Mathematically, this law has the form

(4)

where T is the temperature, is the wavlength corresponding to the maximum of the spectral emitted power and b is a constant whose value is b=2.898 10-3 m K.

Wien's Displacement law can be used to determine the absolute temperature of a blackbody. For example, the sun has a spectral distribution of the thermal radiation is very close to that of a blackbody, the maximum of the spectral curve having the wavelength equal to 470 nm. Using Wien's Displacement law on obtain for the absolute temperature at the surfacee of the sun a value approximative equal to 6200 K.

4. Wien Law

It was known that the radiation spectrum of a blackbody is a continuum spectrum. The form of this spectrum was also known but the analytical dependence of the spectral emitted power,, on the wavelength and on temperature was unknown. This analytical dependence was investigated first in 1887 by the Russian physicist V. Michelson. Then in 1896, the German physicist Wilhelm Wien, found, using both the experimental data concerning the form of this spectrum and also the laws of thermodynamics and electromagnetism, that spectral emissive power of a blackbody can be written as follows:


(6)


where l is the wavelength, T is the absolute temperature, e is the base of the natural logarithms and and are two adjustment constants. Wien Law is an empirical law, i.e. for certain values of the constants and , and in the range of small wavelengths, this law offers a rather good fit to the experimental data.



Fig. 2 The energy distribution in the radiation spectrum of a blackbody. The dependence of the spectral emitted power on the wavelength and on the temperature.

Wien Law can be written also


(7)


from (5) and (7) result


, (8)


or

. (9)

or

(10)


Taking into account that

(11)

and

(12)

on obtain

. (13)


Substituting (13) into (10) result

(14)


Substituting (6) into (14) and using (11), on obtain


.


Therefore, the Wien law can be written as


(15)


where b1 and b2 are two constant.

It is easy to show that spectral emissive power, , has the form


(16)


where is the spectral energy density of thermal radiation, also denoted by . Energy density of the thermal radiation is

From (15) and (16) result that Wien law can also be written as


(17)


where and are two constants.

5. Rayleigh-Jeans Law

In 1900 the British physicist Lord Rayleigh (its true name is John William Strutt), starting from a theorem of statistical mechanics concerning the law of uniform distribution of the kinetic energy among degrees of freedom, theoretically established an expression for the dependence of spectral emissive power of a blackbody on wavelength and temperature. Rayleigh found that, in the range of long wavelengths, the expression leads to a rather good agreement with the experimental data. Later in 1905, James Jeans has derived the expresions for the constants of proportionality appearing in Rayleigh's formula. Therefore the Rayleigh-Jeans law has the form


(18)


Rayleigh-Jeans law can also be written as

(19)


Substituting (18) into (14) and using (11), on obtain


. (20)


Hence, Rayleigh-Jeans law can be written as


. (21)


Taking intoo acount that

(22)


and using (21) and (22) result that Rayleigh-Jeans law can be written as


(23)


This is another form of Rayleigh-Jeans law. While this law fits well the experimental data in the range of long wavelengths, in the range of short wavelengths this law leads to disagreement with the experimental data. This disagreement is known as ultraviolet catastrophe, since at short wavelengths or high frequencies both and increase toward infinity.

Both Wien laws and Rayleigh-Jeans law were just attempts to derive on the basis of classical physics the analytical dependence of the spectral emitted power of a blackbody on wavelength and temperature. Since these attempts are only partly successful show that in classical physics a good description of the spectral distribution of a blackbody's thermal radiation can not be obtained.



6. Planck's Formula

In 1900, German physicist Max Planck found the exact analytical dependence of the spectral energy density of thermal radiation, , on wavelength and temperature. Planck advanced the hypothesis that the emission of the electromagnetic waves is quantized. Therefore the radiation is not emitted in continous amounts but in discrete packets of energy, now called quanta or photons. Each cuanta has the energy

(25)


where h is a constant, called today Planck's constant. Its value, determined experimentally is

(26)


There are many way to derive the Planck's formula. We shall present here the one given by Einstein in 1917. Since the absorption and emission of the electromagnetic waves is quantized result that in atoms discrete levels of energy must exist. According to the quantum physics, the radiation is emitted by atoms when they return from higher energy states, called excited states, to other lower energies states.

Let us assume that an atomic system is placed in an isolated region of space, maintained at a constant temperature T. Also we shall suppose that this region is filled with an equilibrium thermal radiation whose spectral energy density is . We shall consider only the transitions occurring between two atomic levels. Let bus denote by and the energiy of higher and respectively of lower level. Then


(27)


where n is the frequency of the transitions between levels. Let us denote by and the number of atoms placed in the states m and respectively n. According to Boltzmann's distribution law, on can write

(28)

and

(29)


The equilibrium between the atomic system and radiation implies that the number of atoms that jump in unit time from the state m to the state n must to be equal with the number of atoms that jump in unit time from the state n to the state m . Since , result that the transitions n m can occur only by absorption of a radiation (these transitions are called stimulated transitions), while the transitions m n can occur both under stimulation and spontaneously. Hence,

, (30)

and    (31


Let us denote by the probability of a spontaneous transition of an atom from the state m to the state n . Then the number of the atom that perform a spontaneus transition m n in unit time is given by

(32)


The equilibrium condition is

(33)


Let us assume that is the probability of a stimulated transition of an atom in unit time from the energy level to the level , and let us assume that is the probability of the reverse transition. The probability of stimulated transitions is proportional to the spectral density of energy of the electromagnetic field inducing the transition. Hence, we can write

(34)

and

(35)


where the coefficients and are known as Einstein's coefficients.

Therefore, the number of the atoms that perform in unit time a stimulated transition m n is given by

(36)


the number of the atoms that perform in unit time a stimulated transition n m is


(37)


Substituting (32), (36) and (37) into (2.33) on obtain (Fig. 3)


(38)


Nm Wm


AmnNm BmnrnTNm BnmrnTNn

Nn Wn


Fig. 3

or

(39)


Since, for T we have rnT , result that =. Hence, the relation (39) becomes


   (40)


Taking into account (28) and (29) the relation (40) becomes


(41)


The coefficient , will be determined from condition that the expression (41), at low frequencies, must coincide with Rayleigh-James formula. For small frequencies, when

  (42)

we can write

(43)


Substituting (43) into (41), on obtain

(44)


On the other side, according to Rayleigh-James law, we have


(45)


since (44) and (45) must coincide, we get

(46)


Substituting the coefficient given by (46) into (41) on obtain Planck's formula


(47)



Applications.

a) It is easy to see that Wien law can be obtained from Planck's formula, in the particular case of high frequencies. In this case


(48)


hence, we can approximately write

(49)


Substituting (49) into (47) we get Wien law:


(50)


b) Stefan-Boltzmann law can be derived from Planck's formula. Let us start from relation


(51)


Substituting (47) into (51) on obtain

or

(52)


The total emissive power will be


(53)


Denoting

(54)

we can write

(55)

and

(56)


Substituting (55) and (56) into (53) result


(57)

Since

(58)


on obtain

(59)

or

(60)


Therefore, the Stefan-Boltzmann law was derived


(61)

where

(62)


is the Stefan-Boltzmann's constant.



c) Wien's displacement law can be derived from Planck's formula. Let us start from the total emissive power of a blackbody


(63)

Using (63) we can write

(64)

or

(65)


Taking into account that


(66)


then substituting (66) into (65) on obtain


(67)


Substituting given by Planck's formula (47) into (67) on can write


or

(68)


The wavelength corresponding to the maximum of the function , is determined from condition


(69)


Denoting

(70)


on can write

(71)


then, substituting (71) into (68) on obtain


(72)

Hence, the condition

(73)

can be written as

(74)

or

(75)

hence, weget the equation

(76)


whose approximative solution is

(77)


Using (70) on obtain

(78)


Therefore, Wien's displacement law can be written as


(79)


where

(80)

is Wien's constant.


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