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Department Of Applied Physics, ACET BE-Second Semester – Advanced Physics Page 1 UNIT-I LASERS AND WAVE OPTICS
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Page 1: azafarahsanacet.files.wordpress.com€¦  · Web viewFig. Absorption Process The no of absorption transition take place is depended on N 1 no of atom in lower energy level E 1 and

Department Of Applied Physics, ACET BE-Second Semester – Advanced Physics Page 1

UNIT-I

LASERS AND WAVE OPTICS

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LASERS

Introduction:

Laser is one of the outstanding inventions of the 20th century. LASER stands for Light Amplification

by Stimulated Emission of Radiation. . It is artificial light sources that differ vastly form the traditional light

source. Laser have widespread applications in our everyday life and in technological devices ranging from CD

players, DVD players, barcode readers in supermarket, laser printers, eye surgery equipments, dental drills,

optical communication system etc.

It is device which produces a highly directional, coherent, monochromatic, polarized and intense beam of

light that depends upon the phenomenon of stimulated emission.

Interaction of light radiation with matter / Three quantum processes:

To understand the working principal of LASER it is required to understand the three quantum processes that

takes place in material when it is exposed to radiation. A material is composed of identical atoms each of which

has characterized by discrete allowed energy levels. Atoms are characterized by many energy levels but for the

sake of simplicity, consider only two energy levels E1 and E2, E1 is lower energy state (ground state) and E2 is

higher energy state (exited state). As the atoms of the material are identical, energy level E1 and E2 are common

to all atoms within material.

The incident radiation may be viewed as a stream of photons, each photon carrying an energy hv. If hv = E 2 - E1,

then interaction of radiation with atom leads to the following three transition. They are absorption, spontaneous

emission and stimulated emission. Transition or Quantum jump is the process of transfer of atom from one

energy state to another energy state.

1. Absorption / Induced Absorption / Stimulated Absorption :

An atom residing in the lower energy level E1 may absorb the incident photon of energy E2 –

E1= hv and jump to the excited state E2 . This transition is known as stimulated absorption or

induced absorption or simply as absorption.

Corresponding to each transition made by an atom one photon is disappears from the incident beam. It

may be represented as

A + hv A*

Where A is an atom in the lower state and A* is atom in excited state.

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Fig. Absorption Process

The no of absorption transition take place is depended on N1 no of atom in lower energy level E1 and

photon density Q.

The number of absorption transitions occurring in the material at any instant will be proportional to the number

of atoms at the energy level E1 and the photon density in incident beam. The number of atoms N ab excited during

time Δt is therefore given by

Nab = B12 N1Q Δt

Where B12 is the constant of proportionality, known as the Einstein coefficient for induced absorption

2. Spontaneous Emission: Excited energy state with higher energy is inherently unstable. To achieve minimum potential energy condition,

atoms are always tends to remain in the lower energy level.

The excited atom in the state E2 may return to lower state E1 on its own out of natural tendency to attain

minimum potential energy condition by releasing excess energy in the form of photon . This type of

process in which photon emission occurs without any external impetus is called spontaneous emission.

We may write the process as

Where hv is energy of incident photon, A is an atom in the lower state and A* is an excited atom.

Fig. Spontaneous Emission process

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The no of spontaneous transition occurring during the time ∆t is depended on N2 number of

atom in excited energy level E2 .

Thus the no of spontaneous transition in time ∆t is given by

Nsp = A21 N2∆t

Where A21 is the constant of proportionality which is known as Einstein coefficient for

Spontaneous Emission.

The important features of this process are:

(1) It cannot be controlled from outside.

(2) The light emitted due to this process is incoherent i.e. the photons have different phases, planes of

polarization and direction of propagations.

(3) The light spreads in all direction around the source. The light intensity goes on decreasing rapidly

with distance from the source

3. Stimulated Emission / Induced Emission :

A photon of energy hv=E2-E1 can induce / trigger the excited atom to make a downward

transition releasing the excess energy in the form of photon. The phenomenon of forced emission

of photon by an excited atom due to the action of an external agency is called stimulated

emission. It is also known as induced emission. It is represented as

The existence of this mechanism was predicted by Einstein in 1916.

Fig. Stimulated Emission process

The no of Stimulated transition occurring in the material in time ∆t is depended on N 2 no of atom in

excited energy level E2 and photon density Q.

Thus the no of Stimulated transition in time ∆t is given by

Nst = B21 N2 Q ∆t

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Where B21 is the constant of proportionality which is known as Einstein coefficient for

Stimulated Emission. The phenomenon of stimulated emission is to be maximized for laser operation because it

produces coherent photons and also multiplies it.

Characteristics of stimulated emission:

1) The photon induced in this process propagates in the same direction as that of incident photon.

2) The induced photon has features identical to that of the incident photon. It has the same frequency, phase and

plane of polarization as that of the incident photon.

3) The outstanding feature of this process is the multiplication of photons. For one photon interacting with an

excited atom, there are two photons emerging. The two photons traveling in the same direction interact with two

more excited atoms and generate two more photons and produce a total of four photons. These four photons in

turn stimulate four excited atoms and generate eight photons, and so on. The number of photons builds up in an

avalanche like manner, as shown in Fig. below.

Fig: Multiplication of stimulated photons into an avalanche.

Distinction between Spontaneous and Stimulated Emission:

Sr. No Spontaneous emission Stimulated emission

1. Spontaneous emission is a random and probabilistic process.

Not a random process.

2. Not controllable from outside. Controllable from outside.

3. Photons are emitted uniformly in all directions from an assembly of atoms. As a result, the light is non-directional.

The photons emitted in the process travel in the same direction as that of incident photon, so light produced by the process is essentially directional.

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4. Photons of slightly different frequencies are generated. As a result, the light is not monochromatic.

The frequency of emitted photon is nearly equal to that of incident photon. As a result the light is nearly monochromatic.

5. The photons emitted by this process have not any correlation in their phases. Therefore, the light produced by this process is incoherent.

The photons emitted by this process are all in phase and therefore, the light is coherent.

6. In this process multiplication of photons does not take place. Hence light amplification does not occur.

In this process multiplication of photons take place. Hence light amplification occurs. (One stimulating photon causes emission of two more photons. These two produce four photons, which in turn generate eight photons and so on. Thus, if there are N excited atoms, 2N photons will be produce.)

7. The net intensity of the generated light is given by

IT.=N I

Where N is the number of atoms emitting photons and I is the intensity of each photon.

As all the photons are in phase, they constructively interfere and produce an intensity

IT =N2 I

8. The planes of polarization of the photons are oriented randomly. Hence, light from the source is unpolarized.

The planes of polarization are identical for all photons. Consequently, light is polarized.

Active Medium

A medium in which light gets amplified is called active medium. The medium may be solid,

liquid or gas.

Active Centers

Out of the different atoms in the medium only small fraction of the atoms are responsible for

stimulated emission and consequent light amplification. They are called active centers. The remaining

bulk of the medium supports the active centers.

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Population and thermal equilibrium

The number of active atoms occupying an energy state is called as population of that state.

Let N1 and N2 be the population of lower energy level E1 and upper energy level E2 . In thermal

equilibrium the population of energy level E1 and E2 is given by Boltzmann factor

N 2

N1=exp [−(E2−E1)

kT ]

The negative exponent in this equation indicates that N2 << N1

at equilibrium. It means more atoms

are in lower energy levels E1. This state is called as “Normal State” or “Thermal Equilibrium state”.

Conditions for Light Amplification: Light amplification requires that stimulated emission occur almost exclusively. In practice, absorption and

spontaneous emission always occur together with stimulated emission. The laser operation is achieved when

stimulated emission exceeds than absorption and spontaneous emission.

1) Condition for Stimulated emission to dominate spontaneous emission process

Stimulated transition spontaneous t ransition

=B21 N 2 QA21 N2

=B21

A21Q

--------------- (1)

Eq. (1) shows that in order to increase stimulated transition the photon density Q is must be larger.

2) Condition for Stimulated emission to dominate Absorption transitions process

Stimulated Transition Absorption Transition

=B21 N2 QB12 N1 Q

=N 2

N 1

---------------(2)

Where B21 = B12 as the probability of Stimulated Emission must be equal to probability of

absorption transition. The eq. (2) indicate that stimulated transition will be larger than absorption, only

when N2>N1

A medium amplifies light only when above two conditions are satisfied.

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Population Inversion / Inverted State / Negative Temperature State :

Population inversion is the condition of the material in which population of upper energy level N2

far exceeds the population of lower energy level N1 , i.e. N2 >> N1.

Therefore, a non equilibrium state is to be produced (required) in which the population of the

upper energy level exceeds to a large extent than the population of lower energy level. When this

situation occurs the population distribution between the energy level E1 and E2 is said to be inverted,

and medium is said to have gone into the state of population inversion.

The condition N2>N 1

is called population inversion. It is also referred to as a condition of negative

temperature as the ratio N2 /N 1

could be larger than unity only if the temperature were negative in the

Department Of Applied Physics, ACET BE-Second Semester – Advanced Physics Page 8

N1

N 2

N1

N2

Normal State N 2 << N1

Thermal Equilibrium State

Inverted State / population inversion N 2 >> N1

Non -Thermal Equilibrium State

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boltzmann’s factor

N 2

N1=exp [−(E2−E1 )

KT ] . Therefore, it is known as negative Temperature State.

In practice population inversion may be obtained at normal temperature also

Metastable state

An atom can be excited to a higher level by supplying energy to it. Normally excited atoms have short

lifetimes and release their energy in 10-8sec or 10-9sec through spontaneous emission. To establish the

condition of population inversion, the excited atoms are required to wait at the upper energy level till a

large number of atoms accumulate at the excited level. Such an opportunity would be provided by

metastable states. Atoms excited to a metastable state remain excited for an appreciable time, which is

of the order of 10-6 to 10-3 s.

Metastable state can be defined as the intermediate state between ground state and excited state where

excited atom can remain for a longer time i.e 10-6 to 10-3 s than life time of normal excited state 10-8sec or

10-9sec.

There could be no population inversion and hence no laser action , if metastable state does not exist.

Pumping / Pump :

The process of supplying energy to the medium to transfer it into the state of population inversion is

known as pumping.

Three types (Techniques/ Methods) of pumping:

1. Optical pumping:

In optical pumping a light source such as flash discharge tube is used to supply energy. Most often this

energy comes in the form of short pulses of light. This mechanism is used in solid state laser e.g. Ruby

lasers.

2. Electric Discharge:

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E1

E2

E3 Metastable

state

Exited state

Lower state

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In this process electric field is used for ionization of gas medium which excites the ground state

atoms to the excited state. This is used in gas lasers especially He-Ne laser.

3. Direct Conversion:

In this process Electrical energy is directly converted into light energy. This is used in semiconductor

diode lasers.

The Principal Pumping Schemes:There are two important pumping schemes . they are known as three level and four level pumping

schemes. Atoms in general are characterized by large number of energy level. Among them only three

or four levels are suitable for pumping process The transition between two level that generates the

stimulated emission is called Lasing transitions. The lower level is called as lower lasing level and

upper level is called upper lasing level. The uppermost level is called as Pumping level.

Upward arrow implies – Pumping Transition

Downward arrow implies – Lasing Transition

1. Three level pumping scheme:Let us consider an atomic system has three energy level as shown in figure . E1 is Ground State. E2 is

Metastable state and E3 is Excited /Pumping State.

When light photon of energy hν= (E3- E1 ) is incident on medium , the atoms in ground state are readily

excited to pumping level E3 . The pumping level E3 is not stable state, thus atoms do not stay at the E3

Level and take a downward transition either to E1 or E2 through non radiative or Spontaneous

transition .The probability of spontaneous transition E3 to E1 is less than E3 to E2. Since E2 is metastable

state, atom get trapped in the state E2 the pumping continuous and after short time there will be a large

accumulation of atoms at the level E2 when more than half of the ground state atoms accumulate at E2 ,

the population inversion condition is achieved between two state E2 and E1. Now the spontaneously

emitted photon of energy hv=E2-E1 can trigger stimulated emission of atom at E2.

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Disadvantages:

1) In this scheme terminal state of laser transition is simultaneously the ground state. To achieve population

inversion more than half of ground state atoms must be pumped to upper state. Therefore a very high

pump power is required in this pumping scheme.

2) The three level schemes produce, light only in Pulses. Once stimulated emission commences, the

metastable state is quickly emptied and the population of ground state increases rapidly ; as a result

population inversion ends, one has to wait till the population inversion is reestablished. Thus the three

level laser operates in pulsed mode.

2. Four level Pumping Scheme: Let us consider an atomic system has four energy level as shown in figure . E1 is Ground State.

E3 is Metastable state and E2 and E4 are the Excited State.

Pumping frequency lifts the active center (active atoms) from ground state E1 to uppermost level E4.

From pumping level E4 , atom rapidly fall to the metastable state E3 . The population at this state grows

rapidly while the level E2 is virtually empty. Therefore population inversion is achieved between the

state E2 and E3. A photon of energy hv= (E3-E2) can start a chain of stimulated emission , bringing the

atom into the the state E2 . Atoms from E2 undergo non radiative transition subsequently to the ground

state E1 and will be available once again to participate in the process.

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The lower lasing level E2 is virtually empty. Therefore less pump power is sufficient to achieve

population inversion. Four level lasers operate in continuous wave (CW) mode.

3. Two level Pumping Scheme:

Two level pumping scheme is not suitable for obtaining population inversion . the time span ∆t for

which atom have to stay at the upper level E2 must be longer for achieving population inversion

condition. According to Heisenberg Uncertainty Principle,

∆E. ∆t ≥ h/2π

∆t will be longer , if ∆E is smaller that is E2 is narrow. If ∆E is smaller the pumping efficiency is

smaller as a consequence of which less number of atoms are excited. Through a sharp energy level

supports the population inversion , enough population cannot be excited to level E2 in view of small

energy ∆E. The result is that upward transition would be accompanied by premature downward

stimulated transition and population in level E2 would not accumulate to the required extent.

Optical Resonator or Cavity Resonator or Optical resonant cavity or Fabry

perot resonator : A pair of optically plane parallel mirrors enclosing active medium in between them is called as

optical resonator. One of the mirrors is 100% reflecting while the other is made semitransparent. The

mirrors are set normal to the optic axis of the active material. This structure is also known as Fabry-

Perot resonator

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Action Optical Resonator/ Lasing action:

Fig 1 shows the active medium enclosed in optical resonator. The resulting laser action which is

shown in fig (2) consists of following steps,

Step 1: Pumping: Let us assume that the active centers are initially in the ground state. Through the

suitable pumping mechanism the material is taken into a state of population inversion as shown in fig.

2(a)

Step 2: Population inversion: The life time of atom at the excited state is extremely small of the order

of 10-9 Sec. Therefore the atom drop spontaneously from the excited state to the metastable state. As the

life time of metastable state is comparatively longer (10-3 to 10-6 Sec), the atoms go on accumulating at

the metastable state. As soon as the number of atoms in metastable state exceeds that of ground state,

the medium goes into the state of population inversion.

Step 3: Spontaneous emission / stimulated emission: Some of the excited atoms at the metastable

state may emit photon can trigger many stimulated transitions. The photon emitted in a direction other

than the axial direction which will pass through the sides of the medium and all lost forever.

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Fig (2): Action Optical Resonator

Step 4: Optical feedback and Light amplification: A majority of photons traveling along the axis

cause stimulated emission and are reflected back on reaching the end mirror. They travel towards the

opposite mirror and on their way stimulated more and more atoms and build up the photon strength fig

2(d). The photon that strike the opposite mirror are reflected once more into the medium [fig 2(e)]. as

the photon are reflected back and forth between the mirrors stimulated emission sharply increases and

provide positive feedback of light into the medium so that stimulated emission acts as sustained and the

medium operates as an oscillator.

Step 5: Light Oscillations: At each reflection at the front end mirror, light is partially transmitted

through it. The transmitted component constitutes a loss of energy from the resonator. when the losses

at the mirror and within the medium balance the gain; a steady and strong laser beam will emerge from

the front end mirror fig.2(f)

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Role of Optical resonator1. The primary function of optical resonator is to provide positive feedback of photons into the medium

so that stimulated emission is sustained and laser acts as a generator of light.

2. In order to make the stimulated emission dominate spontaneous emission, a high photon density is

required to be present in the active medium. The optical resonator builds up the photon density to a

very high value through repeated reflections of photons and confines them within the medium

3. The optical resonator selects the direction in which the light is to be amplified; the direction being the

optical axis of the pair of mirror. Thus optical cavity makes the laser beam highly directional.

4. Optical cavity selects and amplifies only certain frequencies causing the laser output to be highly

monochromatic.

Condition of steady state Oscillation / condition of resonance:

The wave propagation within the cavity resonator should take on standing wave pattern so that a

continuous increase in the wave amplitude occurs the condition for forming standing wave within the

resonator is that the optical path length traveled by a wave between the consecutive reflection should be

an integral multiple of wavelength, thus

2L = m λ (m= 1, 2, 3……..) L = m λ/2Where L is distance between mirrors, λ is wavelength of light within the material.

Because of its relative length as compared to the wavelength of light ,the resonator may simultaneously

support several standing wave of slightly different wavelength. They are called as longitudinal cavity

mode. Each mode has distinct frequency given by

νm = mc / 2L

Where m is called as mode number , νm are the frequency which are sustained in the cavity and hence

the emerging beam is restricted as invisible border having wide range of frequency.

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Types of Laser:

The lasers are normally classified on the basis of material (Active Medium ) used are as follows

1) Solid state laser:

E.g. Ruby Laser, Nd: YAG Laser

2) Gas laser:

He-Ne Laser, CO2 Laser

3) Liquid Dye laser:

E.g. Liquid dye laser an organic dissolved in liquid such as alcohol; benzene etc. acts the active centre

4) Solid state Diode laser:

E.g. Semiconductor diode laser

On the basis of nature of output, lasers can be operated in

1. Continuous Wave Mode (CW)2. Pulsed Mode (PM)

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RUBY LASER:

Historically the first working laser was the Ruby laser. It belongs to the class of solid-state lasers. Ruby is

basically Al203 crystal containing about 0.05% of chromium atoms. Cr3 ions are the actual active centers,

while aluminum and oxygen atoms are host medium. Chromium ions have absorption bands in the blue and

green regions

Construction:

Ruby is taken in the form of cylindrical rod of about 4 cm long and 1cm in diameter. Its end faces are

made perfectly flat and parallel to each other. One of them is completely silvered to achieve 100 % reflection and

other one is partially silvered to make it semitransparent. Thus, two silvered faces constitutes the mirrors of

fabry perot resonator.

Ruby rod is surrounded by a helical photographic flash lamp filled with xenon. It produces flashes of

white light , whenever activated by the power supply. The system is cooled with help of coolant around the ruby

rod.

Working: The energy levels of the chromium ions in the crystal are as shown in the figure.

Ruby Laser uses three level pumping scheme. Cr3+ ions are the active centers while aluminium and oxygen

atoms are inert. The xenon flash lamp generates an intense of white light lasting for few milliseconds.

The Cr3+ ions are excited to the energy bands E3 and E3’ by the green and blue components of white light. The

normal excited level E3 is highly unstable, the life time of E3 is 10-9sec . From there the Cr 3+ ions undergo

non-radiative transitions and quickly drop to the metastable level E2. .

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E2 is metastable state having life time of the order of 10-3 sec to 10-6 sec. The metastable state E2

has a lifetime of approximately 1000 times more than the lifetime of E3 level. Therefore Cr 3+ ions accumulate at

E2 level. When more than half of the Cr 3+ ion population accumulates at E2 level, the population inversion is

established between E2 and E1 levels. A chance photon emitted spontaneously by a Cr 3+ ion initiates a chain of

stimulated emissions by other Cr 3+ ions in the metastable state. Red photons of wavelength 6943 AO travelling

along the axis of the ruby rod are repeatedly reflected at the end mirrors and light amplification takes place. A

strong intense beam of red light (λ=6943AO) emerges out of the front-end mirror.

Disadvantages:

The xenon flash lamp lasts for few milliseconds. However laser does not operate throughout this

period. Once stimulated emission starts, the mestastable state E2 gets depopulated very rapidly and

lasing ceases. The laser becomes inactive till the population inversion is once again established.

Therefore the output of the laser is not continuous but occurs in the form of pulses of micro seconds

duration.

It requires high pumping power as more than half the active atoms are to be lifted to excited state from

the ground state to achieve population inversion.

The efficiency of ruby laser is less as only the green and blue component of the white light is utilized

while the rest of the components of incident light are unused.

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He-Ne Laser:

He-Ne laser was first successful gas laser built by Ali javan, W.Bennett and D.Herriot in 1961. , Neon atoms are the active centers while Helium atoms helps in exciting Neon atoms.

Construction:

The He-Ne laser consists of a long and narrow discharge tube having length about 50cm and

diameter 1 cm. The tube is filled with the mixture of He and Ne in the ratio 10:1 respectively. Electrodes are provided in the discharge tube to produce discharge in the gas. They are connected to a high

voltage power supply. The tube is hermetically sealed by inclined windows arranged at its two ends. On the axis

of tube, two mirrors are arranged externally which forms the optical resonator. Out of which, one mirror is

completely reflecting and the other mirror is partially reflecting. The distance between the two mirrors is adjusted

such that mλ/2 and supports the standing wave pattern.

Working:

Helium neon laser employs a four level pumping scheme. When the power is switched on, the electric

field ionizes some of the atoms in the mixture of helium and neon gas. Due to electric field the

electrons and ions are accelerated towards the anode and cathode respectively. Since the electrons have

a smaller mass, they acquire a higher velocity. The energetic electrons excites helium atoms through

atomic collisions to the excited state F2 and F3 which lie at at 19.81 eV and 20.61 eV above the ground

level respectively . These two state are metastable states and hence the helium atoms excited to these

levels spend a sufficient long amount of time before getting de-excited. With the passage of current

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through the discharge tube more and more helium atoms are accumulated in the excited state . These

excited helium atom can return to the ground state by transferring their energy to the Neon atom

through collision. Such an energy transfer can take place when the two colliding atoms have identical

energy state. Such an energy transfer is called as resonant energy transfer.

Fig.b) Energy level of Helium and Neon atom and transition between the levels

The E6

level which is at 20.66 eV and E4 level which is at 18.7 eV of neon atom nearly coincide in

energy with the F3

and F2

levels of helium atom. Therefore resonant transfer of energy can occur

easily. The kinetic energy of Helium atoms provide the additional 0.05 eV for exciting the neon atoms

to E6

level. This is the main pumping mechanism in He-Ne laser. Neon atoms are the active

centers and role of He atoms is to excite neon atoms and cause population inversion. This results

in the excitation of neon atoms to the levels E4

and E6

and de-excitation of the helium atoms to the

ground level. Thus, discharge through the gas mixture continuously populates the neon excited energy

levels E4

andE6

. This helps to create a state of population inversion between the levels E6 and E5,

E6 and E3 ,E4 and E3. Consequently three laser transitions can occurs.

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1.15 μm

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i) E6 E3 Transitions: this transition generates a laser beam of red colour of wavelength 6328A0.

ii) E6 E5 Transitions: It produces far infrared laser beam at a wavelength of 33900 A0 (3.39μm)

iii) E4 E3 Transitions: It produces infrared laser beam at a wavelength of 11500 A0. (1.15μm)

From the level E3 the neon atoms drop to E2 level spontaneously. The E2 level is a metastable state and

neon atoms tends to accumulate in this level. This disturbs the condition of population inversion.

Hence, to drop the neon atoms from E2, they are made to collide with wall of tube and get de-excited to

ground state. Thus to increase the probability of atomic collision with the walls, the discharge tube is

made narrow.

Semiconductor Diode Laser:

A semiconductor diode laser is a specially fabricated pn junction device that emits coherent light when it is

forward biased. R N Hall and his coworkers made the first semiconductor laser in 1962.

Construction: A schematic diagram of semiconductor diode laser is shown in fig. The diode is extremely small

in size with sides of the order of 1mm. the junction lies in a horizontal plane through the center. The top and

bottom faces are metalized and two electrodes are provided to pass current through the diode. The front and rear

faces are polished parallel to each other and perpendicular to the plane of the junction. The polished faces

constitute the Fabry-Perot resonator. The other two opposite faces are roughened to prevent lasing action in that

direction. The active region consists of a layer of about 1µm thickness.

Working:

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Fig. (a) Heavily doped pn junction without bias and (b) Heavily doped pn junction forward biased above threshold

value .

The energy band diagram is shown in figure. The donor and acceptor levels get broaden due to heavy

doping. Hence the Fermi levels in p and n regions get shifted in valence band and conduction band

respectively. At thermal equilibrium, the Fermi levels in conduction band and valence band are at same

level. The electrons remain accumulated below Fermi level in conduction band and holes above the

Fermi level in valence band as shown in figure.

When the junction is forward biased, the energy levels shift and electron and holes are injected into

the depletion region. Due to this, the width of region decreases. At low forward biased voltage, the

electron-hole concentration is low and diode works as LED.

However at larger forward biased voltage, the carrier concentration reaches to very high value. In

upper levels, electron concentration is more and lower levels, hole concentration is also large. Thus, the

condition of population inversion is achieved in semiconductor diode.

At this state, the few recombination of electrons with holes result in spontaneous emission. The

photons that propagate in the junction plane induce stimulated recombination of electron hole pair and

intense laser beam of wavelength 9000 A0 is emitted

Advantages:

The semiconductor diode laser is simple, compact and highly efficient

It requires very little power and little auxiliary equipment.

Limitations:

This laser gives more divergent beam having an angular spread of the order of 50 to 150.

They are less monochromatic

Highly temperature sensitive

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Characteristics of Laser: 1. Coherence: A conventional light source such as incandescent lamp or natural source such as sun

produces incoherent light since they emit random wavelength light waves with no common phase

relationship.

On other hand the wave emitted by a laser source will be in phase and are of same frequency.

Therefore light generated by a laser is highly coherent. The coherence length is determined by the

relation.

lcoh=λ2

μΔλ

Is typically of the order of a few kilometers. in case of laser whereas the coherence length of light

radiation by conventional monochromatic source is of the order of few millimeters or centimeters.

2. Directionality:

Conventional light source emits light in all direction but laser emits (spreads) light in one directional as

the photons traveling along the optical axis of the system are only selected and augmented with the help

of optical resonator. The width of laser beam is very narrow and can travel to long distance without

spreading Hence it can be focused sharply.

3. Divergence:

Light from conventional sources spread out in the form of spherical wave front and hence it is highly

divergent on the other hand light from a laser propagates in the form of plane waves. The small

divergence that exist is due to the diffraction of the beam of the exit mirror.

4. Intensity:

The intensity of light from the conventional sources decreases rapidly with distance as it spreads in the

form of spherical waves. Laser emits light in the form of a narrow beam which propagates in the form

of plane waves. As the energy is concentrated in a very narrow region and stays constant with distance.

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5. Monochromaticity:

A light source is said to be monochromatic , if it emits light of single frequency or single wavelength.

The light from normal monochromatic sources spreads over a wavelength of the order 100 A0 to 1000

A0 . The laser light is highly monochromatic. The spread is of the order of a few angstrom units

(<10A0) only. That is the line width associated with laser beams is extremely narrow.

Coherence :

Coherence is an important property of light. Coherent light means that the light waves maintain

constant phase difference over a period of time. It refers to the constant phase difference between

a wave or waves at a point or different points in space with time.

Types of Coherence:

1. Temporal Coherence: i) If the wave maintains constant phase difference at a given time and certain time later then the waves are

said to be temporally coherent.

ii) It refers to the continuity and uniformity of a wave along (parallel to) the direction of propagation of

wave.

iii) It is the characteristic of one wave.

iv)It is related to finite bandwidth of the source.

v) It is also called longitudinal coherence.

2. Spatial coherence: i) A wave exhibits spatial coherence, if the phase difference between any two fixed points , in a plane

perpendicular to the wave propagation does not vary with time.

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P1

P2

P3Source

S

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ii) It refers to the continuity and uniformity of a wave in a direction perpendicular to the direction of

propagation of wave.

iii) It is the characteristic of more than one waves travelling along different paths.

iv) It is related to finite size of the disturbance.

v) It is also called transverse coherence or lateral coherence.

Coherence length :Let us consider the wave train generated by an atom at a particular instant. The middle of the wave train

appears fairly sinusoidal for some number of oscillations whereas at its end occur abrupt change of

frequency and phase.

Defn : The length of wave train over which it may be assumed to have a fairly sinusoidal character

and predictable phase is known as coherence length.

It is denoted by lcoh.

The coherence length may also be defined as the product of number of waves contained in the wave

train N and wavelength λ. Thus,

lcoh = Nλ

Coherence time: The time interval over which the phase of the wave train can be predicted reliably is called

coherence time.

It is denoted by tcoh or τ

lcoh = c ∆t

As tcoh = ∆t

lcoh = c tcoh --------------(1)

Relation between Coherence length and frequency band width: According to Fourier analysis, the frequency bandwidth is given by

Δν= 1Δt

−−−(2 )

Where ∆t is the average lifetime of the excited state of atom

In eqn (2) ∆t is the time during which a wave train is emitted by atom and corresponds to the coherence

time tcoh.

Δν= 1Δt

= 1t coh

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Using eqn(1) in eqn (2)

Δν=clcoh

lcoh=cΔν

−−−−(3 )

Relation between Coherence length and wavelength band width:The frequency and wavelength of light wave is given by

v= cλ ------- (4)

Where λ is wavelength. On Differentiating eqn (4) on both side

Δν=−cΔλλ2

clcoh

=−cΔλλ2

lcoh=λ2

Δλ (Using Eq. (3))

Where ∆λ is called as natural line width or band width.

Application of Lasers:

A] Engineering Application:1) Welding: Welding is the joining of two or more pieces into a single unit. The laser beam heats the

edges of two plates to their melting point and causes them to fuse together where they are in contact.

The main advantage of laser welding is that it is a contact less process and hence no possibility of

introduction of impurities into the joint.

2) Drilling: the principal underlying drilling is the vaporization of the material at the focus of the

beam. With laser, one can drill holes as small as 10 mm in diameter.

3) Surveying : Civil engineers use laser for surveying process

4) Laser beam can be used for cutting, molding the metals.

5) Electronics Industry: electronics industry used lasers in the manufacture of electronic component

and integrated circuits.

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6) Laser beam can be used in fiber optics communication.

B] Scientific Applications:

1] The distance between the earth and moon has been precisely measured by using laser beam.

2] It is used for tracking of the satellites and space craft tracking means the determination of a path of

a moving object.

C] Medical Applications:-

1] In medicine it is used for diagnosis as in endoscopy in which inner parts of the body are examined

with the help of laser using an optical probe.

2] Affected part of the body can be burnt out by irradiating with laser Hence it is used in treatment

of cancer and ulcers.

3] Laser is useful in painless surgery specially that of an eye.

4] Dentists use the laser beam to destroy germs in tooth cavities without pain It is also used to seal

cracks in the enamel of the tooth.

D] Military Applications:-

1] Laser can serve as a user weapon since laser beam is highly directional and energetic.

2] It can be used as death ray which could destroy anything near or far.

E] Miscellaneous Applications:-

1] The most exciting application of laser is in holography in which three dimensional view of the

object is obtained.

2] Holography is also used for data storage in computers.

3] Laser is used for recording audio and video information on discs. It also used in laser printers.

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WAVE OPTICS

Interference: The phenomenon of redistribution of light due to superposition of light waves from two or more coherent sources is known as Interference.

Types of Interference

Constructive Interference (Maxima)If the optical difference between two rays is integral number of wavelength, then the rays meet each other in phase then the reflected waves interfere constructively at the point of their meeting.Optical Path difference, ∆ = n λ ( n = 0,1,2,3,……)

Destructive Interference (Minima)If the optical difference between two rays is odd integral number of wavelength, then the rays meet each other in out of phase then the reflected waves interfere destructively at the point of their meeting.Optical Path difference = ∆ = (2n + 1) λ /2 ( n = 0,1,2,3……)

Geometrical path:

The shortest distance L between two points is known as the geometrical path. It is independent of the medium.

Optical path:

The distance experienced by light waves in a medium is releted to the R. I. of the medium. It is called optical path ∆. It is related to the geometric path L through the relation

∆ = µ x geometric path relation ∆ = µ L

Thin Film:

A film is said to be thin when its thickness is of the order of one wavelength of visible light which is taken to be 5500 A0. Thus a film of thickness in the range of 0.5µ to 10 µm may be considered as a thin film. A thin film may be a thin sheet of transparent material such as glass, mica, an air film enclosed between two transparent plates or a soap bubble.

1) Interference due to reflected light (Plane parallel film)

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Consider a plane parallel of uniform thickness ‘t’ as shown in the figure. Let ‘µ’ be the refractive index of the material of the film. The film is surrounded by air on both sides. Let a plane parallel monochromatic light beam is incident on the upper surface of the film. Let ray AB be incident on the upper surface of the thin film at an angle of incidence ‘i’.

The ray AB is partially reflected along BC and is partially transmitted into the film along BF. The transmitted ray BF makes an angle ‘r’ with the normal and meets the lower bounding surface. At F, it is

partly reflected back into the film along DF, while a major portion refracts into the outer medium along FK. The reflected ray FD refracts at the outer surface and emerges out along DE which is parallel to ray BC. Both the rays BC and BFDE are travelling along the same direction and are obtained from the same incident ray

AB. Therefore they are coherent and produces interference. The condition for interference depends on the optical path difference between the rays BC and BFDE.

Actual path difference :∆a = 2µ t cos r

Correction on account of phase change at reflection : When a ray is reflected at the rarer medium, a path change of λ/2 ( or a phase change of π) occurs for the ray BC due to abrupt change of π rad in the phase of wave BC. By including the change in path difference due to reflection, the true path difference is

∆t = 2μtcosr− λ2

i) Condition for Maxima (Brightness)When the optical difference between two rays is integral number of wavelength, then the rays meet each other in phase then the reflected waves interfere constructively.

∆ = n λ ( n = 0,1,2,3,……)

2μtcosr− λ2 = n λ

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2μtcosr = n λ+ λ2 ∴ 2μtcosr = (2n+1¿ λ

2

ii) Condition for Minima (Darkness)When the optical difference between two rays is odd integral number of wavelength, then the rays meet each other in out of phase then the reflected waves interfere destructively.

∆ = (2n + 1) λ2 ( n = 0,1,2,3……)

2μtcosr− λ2 = (2n + 1)

λ2

2μtcosr = (2n + 1) λ2

+ λ2

∴ 2μtcosr = (n +1) λ = n λ ( n +1 is replaced by n for simplicity of expression)

In both the expressions n is called as order of interference. Since the rays reflected from the surface of thin film are parallel to each other they do not intersect at finite distances.

2) Variable thickness or wedge shaped thin film:

A thin film having zero thickness at one end and progressively increasing to particular thickness at the other end is called a wedge / or wedge shape thin film.

Thin wedge of air film is formed by two glass slides resting on each other at one end and separated by a thin spacer at the other end. Arrangement for observing the interference pattern in a wedge shaped film is as shown in fig.

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Microscope Slides

Glass Plate

Microscope

Sodium Lamp

Thin Sheet / Spacer

450

S

Air Wedge

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Fig. Experimental arrangement

Fig. Ray diagram

When a monochromatic ray of light AB be incident on the wedge from above, it gets reflected from glass to air boundary i.e. at top surface of the air film along BC. Part of incident light AB is transmitted through the air film and gets reflected partly at the air to glass boundary along DE. Thus two rays BC and DE are coherent because they are derived from same ray AB through division of amplitude. These rays interfere if the thickness of the film (t) is of the order of wavelength of light (t ≈ λ). So for small thickness ray BC & DE interfere & produce darkness depending on the phase difference.

Optical Path difference between two ray BC & DE is

Δ=2 μt cos r− λ2 ……… (1)

λ2 be the gain of half wave due to abrupt jump of π-radian of the wave reflected from bottom boundary

i.e. air to glass.

Condition of Maxima (Brightness):

2 μt cosr− λ2=nλ

So 2 μt cosr=(2n+1) λ2

The waves interfere constructively.

Condition of Maxima (Darkness):

2 μt cosr− λ2=(2 n+1) λ

2

So, 2μt cosr=nλ

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Glass to air boundary

Air to Glass boundary

A

D

F

B

E

C

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The fringes are bright and dark when monochromatic light is incident; otherwise coloured fringes are observed with white light.

a) Expression for fringe width in wedge shaped thin film:-

When a monochromatic light is incident on the wedge shaped thin film alternate dark and bright fringes are observed.

Let nth dark fringe occurs at A. For the dark fringe condition

2µt1 cos r = nλ …………………………………(1)

If normal incidence light is considered cos r = 1

And thickness of the wedge at A is considered to be t1.

Then equation (1) becomes 2µt1 = nλ ………………………………….(2)

Let the next dark fringe occurs at C where the thickness of wedge is t2.

Then at the C 2µt2 = (n+1) λ ………………………………………….(3)

Subtracting, equan. (3) From (2), we get

2µ (t2 - t1) = λ ………………………………………….(4)

In ∆ ABC, BC = t2−¿t1, A = θ, AB = β

Using BC = t2−¿t1, in eq. (4), we get

2µ BC = λ …………………………………………………………...……(5)

Also in ∆ ABC, BC = AB tan θ

BC = β θ tan θ …………………………….…(6) ( since AB = β )

Using eq. (6) in (5),

2µ (β tan θ) =λ

∴β= λ2 μ tan θ

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Since θ is very very small, tan θ = θ

∴β= λ2 μθ …………………………………… (7)

Above equation represent the expression for fringe width in wedge shaped thin film.

In this equation µ, λ and θ all are constant hence β is constant for a given wedge angle θ. So the interference fringes are equidistant from one another. As wedge angle θ increases fringes get closer because β decreases. When θ decreases β increases.

b) Fringe at apex is dark:-

At the apex thickness of air film is very small i.e. t<< λ or t=0

Therefore at the apex, optical path difference ∆=2 μt cosr− λ2=0− λ

2

∆=−λ2

It implies that the interfering ray will be 1800 out of phase and interfere destructively at the apex. Hence wedge fringe pattern always begin with dark fringe.

c) Fringes are straight and parallel:

Each of the fringes is produced by the interference of ray reflected from section of wedge having the same thickness. The locus of point having the same thickness lie along lines parallel to the apex line of the wedge. Therefore the fringes are straight and parallel.

d) Fringes are of equal thickness:

As each maxima and minima is a locus of point of same thickness, the fringes are called as fringes of equal thickness.

e) Fringes are localized:

Fringes are said to be localized as they are located at the top surface of film.

f) Determination of wedge angle θ:

Experimentally wedge angle θ can be determined with help of travelling microscope. Position of dark fringes at two distant point say Q &R located at distances x1 and x2 respectively from the apex are noted. Let t1 and t2 be the thickness of the wedge at Q & R respectively.

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Condition for dark fringe at Q is,

2µt1cos r = nλ

For normal incidence cos r =1

But tanθt1

x1

t 1=x1tanθ=x1θ for very small θ

2µ x1θ=nλ -------------------------------- (1)

Similarly for dark fringe at R,

2µt 2=(n+N )λ

2µ x2θ=(n+N )λ ------------------------------- (2)

Where, N is the no. of dark fringes between Q & R

Subtracting equa. (1) From equ. (2) We get

2 µ( x2−x¿¿1)θ=Nλ ¿

θ= Nλ2 µ(x2−x¿¿1)¿

If the film is of air, µ=1.

θ= Nλ2(x2−x¿¿1)¿

g) Spacer thickness: Let the spacer thickness t be used to from the air wedge, kept at distance l from

apex O

tanθ= tl

t=l tanθ≈ lθ

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tt1

t2

OQ

R

x1 x1

l

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l = length of the air wedge

∴ t=l Nλ

2(x2−x¿¿1)¿

Newton ring:

Newton’s ring is observed in the air film enclosed in between the curved surface of convex lens and flat glass plate.

Newton’s ring is example of fringes of equal thickness. They are formed when light is reflected from a plano-convex lens of long focal length placed in contact with a glass plate. Thin film of air is formed in between the plate and the lens. The thickness of the air film varies from zero at the point of contact to some value t.

If the lens plate system is illuminated with a monochromatic light falling at normal to the plane surface of the lens, concentric bight and dark interference rings are observed in reflected light. These circular fringes are called Newton’s rings. When a ray AB is incident on the system it gets partially reflected at the bottom curved surface of the lens (ray 1) and part of the transmitted ray is partially reflected (ray2)from the top surface of the plane glass sheet. The ray1 and ray2 are derived from the same incident ray by division of amplitude, and are the thus coherent.

Ray 1 undergoes no π change (because reflection from glass to air boundary), but ray 2 acquires phase change of π upon reflection air to glass boundary. The conditions of brightness or darkness depend on the path

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difference between two reflected rays which in turn depends upon thickness of thin film. The conditions for interference of the rays are identical on circumference with radius OJ.

The fringes are bright and dark when monochromatic light is incident, colored fringes are formed when white light is incident. Interference does not take place between the ray reflected from the surfaces of lens and glass plate owing to their thickness.

Conditions:-

1) For constructive interference / Bright rings:

2µt cos r −¿

= nλ

2µt cos r = (2n+1) --------(for bright ring)2) For destructive interference / dark rings:

Simillary, we get2µt cos r = n λ --------(for dark ring)

For normal incidence, cos r = 1

2t = (2n+1) --------(for bright ring) 2t = n λ --------(for dark ring)

Properties/ Main features:-

1) Central spot is dark:

Newton’s rings are formed as result of interference between light waves reflected from the top and bottom surface of a thin air film enclosed between a plano-convex lens and a plane glass plate.

The occurrence of brightness or darkness depends on the optical path difference arising between the reflected rays. The optical path difference is given by ∆=2t-λ/2At the point of contact O of the lens and glass plate as shown in figure, the thickness of air film is

negligibly small compared to a wavelength of light.

t≈0 ∆=λ/2

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The wave reflected from the lower surface of the air film suffers a phase change of rad while the wave reflected from the upper surface of the film does not suffer such change. Thus the superposing waves are out of step λ/2 which is equivalent to a phase difference of 1800 (or π rad ). Thus, the two interfering waves at the centre are opposite in phase and produce a dark spot.

2) Fringes are of equal thickness:

Maxima and minima depends on thickness of air film. Reflected light wave have maximum intensity for those thickness for which path difference is ∆ = n λ and minimum intensity for those thickness for which ∆=

(2n+1) . Thus each maxima and minima is a locus of points of contact film thickness. Hence fringes are known as fringes of equal thickness.

3) Circular Fringes :In Newton’s ring arrangement, a thin air film is enclosed between plano- convex lens and a glass plate. The thickness of the air film at the point of contact is zero and gradually increases as we move outward. The locus of points where the air film has the same thickness then fall on circle whose center is the point of contact. Thus the thickness of air film is constant at point at points on any circle having the point of lens-glass plate contact as the center. The fringes are therefore circular.

4) Fringes are localized in the film: When the film is illuminated with a parallel light beam, the reflected rays are not parallel. They interfere nearer to the top surface of the air film and appear to diverge from these when viewed from the top. The fringes are seen near the upper surface of film and hence are said to be localized in the film.

5) Radii of the dark rings: Let R be the radius of curvature of the lens.Let a dark fringes be located at point QThe thickness of air film at Q is tLet the radius of nth dark fringe at Q is rn

In ∆ NEP, (PN)2 = (PE)2 + (EN)2

R2 = rn2 + (R – t)2

rn2 = 2Rt – t2

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N

R

P

Q Ot

rn

R

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As R >> t, 2Rt >> t2

rn2 = 2Rt

But, condition for dark fringes at point Q is

2µt cos r = nλ

Since cos r = 1 and for air µ=1

2 t = nλ

rn2 = nλR

rn=√nλR -----------------------------for dark ring

The diameter of the dark ring is given by

Dn = 2 rn = 2√nλR

Radii of the different dark ring can be found by substituting n= 0,1,2,3,…….

r0 = 0, r1=√λR,r2=√2 λR

Radii (diameter) of the dark ring are proportional to the square root of the natural numbers.

6) Radii of bright fringes/ rings : The radius of 0th dark ring is given by rn

2 = 2Rt = 2t.R

rn2 = (2n+1) R (since for bright ring 2t= (2n+1) )

rn=√(2 n+1)R

Dn=2√(2 n+1)R

Radii of the different bright ring can be found by substituting n= 0,1,2,,…….

r0=√Rr1=√3 R

Radii (diameter) of the bright ring are proportional to the square root of the odd natural numbers.

7) Lens of larger radius of curvature is used:

The radius of nth dark ring is given by

rn=√nλR

From above equation it is seen that the radius of dark ring is proportional to square root of radius of curvature of the lens.

i.e. rnα√ R

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It implies that greater the radius of curvature of the lens, the larger would be the diameter of the ring. Therefore less error in measurement of diameter

8) Rings gets closer away from the centre: It is observed that two consecutive fringes away from the centre are closer to each other and hence crowded. The diameter of dark ring is proportional to the square root of the natural numbers while the diameter of bright ring is proportional to the square root of the odd numbers.

From equa. Dn=2√nλR is observed that the order of rings (n) increases; the diameter does not increases in a same proportion with the result that the rings gets closer and closer away from the centre.

9) Transmitted light : The rings are exactly complementary to the reflected ring system so that central spot is bright. Contrast of the fringes is less.

10) White light : Produced rings are colored near the point of contact.

APPLICATIONS OF INTERFERENCE:

1. Determination of wave length of light.

λ=D n+ p2 −D n

2

4 pR

where, λ is incident monochromatic light p is no. of rings R is Radius of curvature of plano convex lens Dm+p is the diameter for (m+p)th ring Dm is the diameter for (m)th ring

2. For measuring refractive indices of liquids and gases.

Determination of Refractive Index of Liquid using Newton’s Ring:

µ=[ Dn+ p

2 ]Air−[ Dn2 ]Air

[ Dn+ p2 ]Liq−[ Dn

2 ]Liq

3. For measuring small displacements.4. Testing of lens surface.5. Testing of Flatness/ Smoothness of Surface:

Department Of Applied Physics, ACET BE-Second Semester – Advanced Physics Page 39

Page 40: azafarahsanacet.files.wordpress.com€¦  · Web viewFig. Absorption Process The no of absorption transition take place is depended on N 1 no of atom in lower energy level E 1 and

The smoothness of a surface can be quickly inspected visually by keeping an optical flat on the component at an angle and illuminating it with a monochromatic light. The air wedge formed between the component and optical flat produces straight and equidistant fringes if the component surface is smooth. If the fringes are curved towards the contact edge, the surface is concave and if the fringes curve away, it is convex as shown in fig.

6. Anti-Reflection Coating:

A thin transparent coatings of optical thickness of one quarter wavelength given on a surface in order to suppress the reflection from the surface is called as Anti–reflection film coating.

Principle:

A thin film coating can act as an AR coating if the waves reflected from its top and bottom surface are exactly 180° out of phase and the waves have equal amplitudes.

Conditions for antireflection coating:i. Amplitude condition : The reflected waves will have equal amplitudes, if the refractive index of the

coating material is nearly equal to the sqyare root of the refractive index of the substrate material, thusµfilm ≈√µsubstrate

ii. Phase condition: The waves reflected from the top & bottom surface (ray1 & ray2) of the thin film should be 180º out of phase with each other.

Department Of Applied Physics, ACET BE-Second Semester – Advanced Physics Page 40

Page 41: azafarahsanacet.files.wordpress.com€¦  · Web viewFig. Absorption Process The no of absorption transition take place is depended on N 1 no of atom in lower energy level E 1 and

The minimum thickness of the thin film coating required for the purpose can be obtained from the phase condition.From the above fig., the optical path difference between the reflected wave is

∆=2 µf tcosr− λ2− λ

2

∆=2 µf tcosr

The first λ2 corressponds to phase change at the top surface and the second

λ2 corresponds to change which

occurs at the bottom surface because μf <¿ μ¿ ¿. The two waves interfere destructively if

∆ = (2n + 1) λ2

2 µ f tcosr = (2n+1¿ λ2

For normal incidence cos r = 1

2 µf t = (2n+1¿ λ2

When m=0 the thickness of the film will be minimum

2 µ f tmin = λ2

µf tmin = λ4

Thus the optical thickness (µf tmin) of the AR coating should be of one quarter wavelength.

tmin = λ

4 µf

This is expression for minimum thickness of antireflection coating.

Department Of Applied Physics, ACET BE-Second Semester – Advanced Physics Page 41


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