Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b...

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Electromagnetic (E-M) theory of waves at a dielectric interface i r t n i n t û n x y . z b i k r k t k i E r E t E While it is possible to understand reflection and refraction from Fermat’s principle, we need to use E-M theory in order to understand quantitatively the relationship between the incident, reflected, and transmitted radiant flux densities : We can accomplish this treatment by assuming incident monochromatic light waves which form plane waves with well defined k-vectors as shown in the diagram. The interface is shown with an We will consider E-field polarizations which are (i) in the plane of incidence and (ii) perpendicular to the plane of incidence, as shown below . ) , , ( ), , , ( ), , , ( t t t t r r r r i i i i k E I k E I k E I I i I r I t

Transcript of Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b...

Page 1: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Electromagnetic (E-M) theory of waves at a dielectric interface

i r

t

ni

nt

ûn

x

y

.z

b

ik

rk

tk

iE

rE

tE

While it is possible to understand reflection and refraction from Fermat’s principle, we need to use E-M theory in order to understand quantitatively the relationship between the incident, reflected, and transmitted radiant flux densities:

We can accomplish this treatment by assuming incident monochromatic light waves which form plane waves with well defined k-vectors as shown in the diagram. The interface is shown with an origin and coordinates (x,y,z).

We will consider E-field polarizations which are (i) in the plane of incidence and (ii) perpendicular to the plane of incidence, as shown below.

),,(),,,(),,,( ttttrrrriiii kEIkEIkEI

Ii

Ir

It

Page 2: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

E-field is perpendicular to the plane-of incidence

E-field is parallel to the plane of incidence

Page 3: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Maxwell’s Equations for time-dependent fields in matter

00

BSdB

t

DjHSd

t

DjrdH

t

BESd

t

BrdE

DdVSdD

HBEDEgj

HMMBH

EPPED

mo

eo

1

D – Displacement field

H – Magnetic Intensity

P – Polarization

M – Magnetization

- Magnetic permeability

- Permittivity

e - Dielectric Susceptibility

m - Magnetic Susc.

g – Conductivity

j – Current density

Page 4: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Summary of the boundary conditions for fields at an interface

Boundary

Side 1

Side 2

Maxwell’s equations in integral form allow for the derivation of the boundary conditions for the total fields on both sides of a boundary.

jHHu

uBB

EEu

uDD

n

n

n

n

12

12

12

12

ˆ

ˆ Normal component of D is discontinuous by the free surface charge density

Tangential components of E are continuous

Normal components of B are continuous

Tangential components of H are discontinuous by the free surface current density

Page 5: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

For dielectrics, j = 0. Therefore, the components of E and H that are tangent to the interface must be continuous across it. Since we have Ei, Er, and Et the continuity of E components yield:

i r

t

ni

nt

ûn

x

y

.z

b

ik

rk

tk

iE

rE

tE

i 090

iii EE cossin

tnrin EuEEu

ˆˆ

iiinin EEuEu cossinˆˆ

Note that

Page 6: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

tnrin EuEEu

ˆˆ

tttotn

rrrorniioin

tnrnin

trkEu

trkEutrkEu

EuEuEu

cosˆ

cosˆcosˆ

ˆˆˆ

Consider the expression on the interface (y = b) for all x, z and t. The above relationship must hold at all points and at any instant in time on the interface. Therefore

bytttbyrrrbyii trktrktrk |||

Since then we have tri

byttbyrrbyi rkrkrk |||

Page 7: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Thus, at the interface plane

cos.|ˆ

ˆ||0ˆ|

rconstrkandkkk

ukandkkurkk

byir

nirnrbyri

knu

r

r co

s

ttiitt

ii

ttii

itntbyti

rirriiirn

nncc

kk

kkurkkAlso

kkkku

sinsin,sin1

sin1

sinsin

0ˆ|,

sinsin0ˆ

which is again Snell’s Law

Page 8: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Case 1: E Plane of incidence

Continuity of the tangential components of E and H give

otoroi EEE

Cosines cancel

Using H = -1 B, the tangential components are

otoroitott

tioroi

i

i

tttt

iriii

riri

tttrrriii

tt

tr

i

ri

i

i

EEEandEn

EEn

Ev

EEv

vvand

vEBandvEBvEBSince

BBB

coscos)(

cos1

cos)(1

,

/,/,/

coscoscos

Page 9: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

The last two equations give

coscos

cos2

coscos

coscos

t

ti

i

i

ii

i

oi

ot

t

ti

i

i

tt

ti

i

i

oi

or

nn

n

E

Eand

nn

nn

E

E

The symbol means E Plane of incidence. These are called the Fresnel equations; most often i t o.

Let r = amplitude reflection coefficient and t = amplitude transmission coefficient. Then, the Fresnel equations appear as

ttii

ii

oi

ot

ttii

ttii

oi

or

nn

n

E

Etand

nn

nn

E

Er

coscos

cos2

coscos

coscos

Note that t - r = 1

Page 10: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Case 2: E || Plane of Incidence

Continuity of the tangential components of E:

totrorioi EEE coscoscos

Continuity of the tangential components of -1 B:

it

tt

i

i

ii

i

oi

ot

tt

ti

i

i

ti

ii

t

t

oi

or

riri

ottt

orrr

oiii

nn

n

E

Etand

nn

nn

E

Er

and

Ev

Ev

Ev

coscos

cos2

coscos

coscos

;

111

||

||

||

||

Page 11: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

If both media forming the interface are non-magnetic i t o then the amplitude coefficients become

itti

ii

itti

tiit

nn

ntand

nn

nnr

coscos

cos2

coscos

coscos||||

Using Snell’s law

the Fresnel Equations for dielectric media become

ttii nn sinsin

)cos()sin(

cossin2

)sin(

cossin2

,)tan(

)tan(

)sin(

)sin(

||

||

titi

it

ti

it

ti

ti

ti

ti

tandt

randr

Note that t - r = 1 holds for all i , whereas t|| + r|| = 1 is only true for normal incidence, i.e., i = 0.

Page 12: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Consider limiting cases for nearly normal incidence: i 0.

In which case, we have:

ti

ti

iirr

sin

sin00|| since 1sintan xxx

ittti

tittiti n

n cossincossincossincossinsin

Also, using the following identity with Snell’s law

Therefore, the amplitude reflection coefficient can be written as:

iitt

iitt

iti

t

iti

t

nn

nn

nnnn

ri

coscos

coscos

coscos

coscos

0

Page 13: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

ti

i

it

it

nn

nttand

nn

nnrr

iiii

20||00||0

In the limiting case for normal incidence i=t = 0, we have:

Note that these equalities occur for near normal incidence as a consequence of the fact that the plane of incidence is no longer specified when i t 0.

Consider a specific example of an air-glass interface:

ni = 1

nt = 1.5

ttii nn sinsin

We will consider a particular angle called the Brewster’s angle: p + t = 90 .tan

i

tp n

n

3.56

1

5.1tan 1

p

At the polarization angle p, only the component of light polarized normal to the incident plane and therefore parallel to the surface will be reflected.

i

t

External reflection nt > ni

Internal reflection ni > nt

Page 14: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

External Reflection (nt > ni) Internal Reflection (nt < ni)

n

i

tcttii n

nnn

tci sinsinsin 90

8.415.1/1sin 1c

7.33

5.1

1tan

'

'

p

i

tp n

n

3.56

1

5.1tan 1

p

1

5.1

i

tti n

nnConsider

5.1

1

i

tti n

nnConsider

Page 15: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Concept of Phase Shifts () in E-M waves : trkEE o

cos

0)sin(

)sin(

ti

ti

oi

or

E

Er

Since when nt > ni and t < i

as in the Air Glass interface,

we expect a reversal of sign in the electric field for the Ecase when

.1 forei

We need to define phase shift for two cases:

A. When two fields E or B are to the plane of incidence, they are said to be (i) in-phase (=0) if the two E or B fields are parallel and (ii) out-of-phase ( = ) if the fields are anti-parallel.

B. When two fields E or B are parallel to the plane of incidence, the fields are (i) in-phase if the y-components of the field are parallel and (ii) out-of-phase if the y-components of the field are anti-parallel.

Page 16: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Examples of Phase shifts for two particular cases:

,,

,

0,,

,

phaseofoutBB

EE

phaseinEE

BB

ri

ri

ti

ti

)a( )b(

0,,

,,

phaseinallBBB

EEE

tri

tri

Page 17: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Glass (n = 1.5) Air (n = 1)

Air (n = 1) Glass (n = 1.5)

Analogy between a wave on a string and an E-M wave traversing the air-glass interface.

= 0 = 0

= = 0

Compare with the case of .0 ior forE

Page 18: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Examples of phase-shifts using our air-glass interface:

In order to understand these phase shifts, it’s important to understand the definition of .

Page 19: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Reflected E-field orientations at various angles for the case of External Reflection (ni < nt). It is worth checking and comparing with the various plots for the phase shift on the previous slides.

Page 20: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Reflected E-field orientations at various angles for the case of Internal Reflection (ni > nt). It is worth checking and comparing with the various plots for the phase shift on the previous slides.

Page 21: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Reflectance and Transmittance

Remember that the power/area crossing a surface in vacuum (whose normal is parallel to the Poynting vector) is given by .2 BEcS o

The radiant flux density or irradiance (W/m2) is

TToo

TEcEvE

cSI 222

2

/1vPhase velocity

From the geometry and total area A of the beam at the interface, the power (P) for the (i) incident, (ii) reflected and (ii) transmitted beams are:

ttt

rrr

iii

AIPiii

AIPii

AIPi

cos)(

cos)(

cos)(

Page 22: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Define Reflectance and Transmittance:

2

2

2

2

2

2

cos

cos

cos

cos

cos

cos

2/

2/

cos

cos

tn

n

E

E

n

n

AI

AI

P

PT

RrE

E

Ev

Ev

I

I

AI

AI

P

PR

ii

tt

oi

ot

ii

tt

ii

tt

i

t

oi

or

oiii

orrr

i

r

ii

rr

i

r

Note that

2

2222

22

,

1

2

11

2

1

2

1

2

1

2

1

o

oo

oo

oo

oo

oo

EnITherefore

Ec

nEc

c

vEEvEI

Conservation of Energy at the interface yields:

riritottrorrioii

ttrrii

nnEnEnEn

AIAIAI

,222 ;coscoscos

coscoscos

Page 23: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

Therefore, TRE

E

n

n

E

E

oi

ot

ii

tt

oi

or

22

cos

cos1

We can write this expression in the form of componets and:||

2||||

22||||

2

cos

cos

cos

cos, t

n

nTandt

n

nTrRandrR

ii

tt

ii

tt

11, |||| TRandTRTherefore

1

5.1

i

tti n

nnConsider

We must use the previously calculated values for ttrr ,,, ||||

Page 24: Electromagnetic (E-M) theory of waves at a dielectric interface ii rr tt nini ntnt ûnûn x y. z b While it is possible to understand reflection and.

1

42

4

,0

2

22

2||

2

||

it

itiitt

it

it

it

iti

nn

nnnnnnTR

nn

nnTTTand

nn

nnRRRWhen

It’s possible to verify for the special case of normal incidence:

Consider the case of Total Internal Reflection (TIR):

ttii nn sinsin

5.1

1

i

tti n

nnConsider

t

i

nt = 1

ni = 1.5

8.41

5.1

1sin,90

c

i

tit n

nWhen

c