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PLANE WAVE SOLUTIONS OF MAXWELL'S EQUATIONS
I. CHARACTERISTICS OF PLANE WAVE SOLUTIONS:
For the record, let us once again restate the form of the macroscopic Maxwell's equations
in the time domain which is valid in the high frequency or optical regime.
r rE rr ,t( ) = t
rB rr, t( ) = 0 trH rr , t( ) [I-1a]
r
r
Brr, t( ) = 0
r
r
Hrr , t( ) = 0
r
Jrr,t( ) +
t
r
Prr , t( )
+ 0 0
t
r
Err,t( ) [I-1b]
r
r
Err, t( ) =
1
0rr, t( )
r
r
Prr,t( )[ ] [I-1c]
r
r
B
r
r, t( ) = 0r
r
H
r
r , t( ) = 0 [I-1d]
The most general phenomenological tensorial representation of the linear dielectric response
of a given material which incorporates dissipative and anisotropic effects may be
written in the time domain as
Prr, t( ) = 0 d t
rr, t t( )E
rr, t( )
t
[I-2a]
or in the frequency domain as
Prr, ( ) = 0
rr, ( )E
rr , ( )
[I-2b]
where
rr, ( ) = d t
rr, t t( ) exp j t t( )[ ]
t
= d rr, ( ) exp j [ ]
0
[I-3]
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PLANE WAVE SOLUTIONS OF MAXWELL' S EQUATIONS PAGE 2
R. Victor Jones, October 23, 2002
Neglecting anisotropy, the macroscopic, optical regime Maxwell's equations in the
frequency domain for a linear, isotropic media may be written
r
rE
rr , ( ) =
r
1rr,( )
rDrr , ( ) = j
rB
rr, ( ) = j 0
rH
rr, ( ) [I-4a]
r
rBrr, ( ) = 0
r
rH
rr, ( ) = 0
rJrr , ( ) + j 0
rr, ( )
rErr ,( )
= 0rJrr, ( ) + j 0
rDrr, ( )
[I-4b]
r
rr , ( )
rErr, ( ) =
r
rDrr, ( ) =
rr, ( ) [I-4c]
r
rBrr, ( ) = 0
r
rH
rr, ( ) = 0 [I-4d]
Consider the possibility of a plane wave solution within a uniform medium -- i.e. rr , ( ) ( ) .
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of the form
rE
rr, ( ) =
rE ( ) exp j
rr
rk( ) =
rE ( ) exp j x kx +y ky + zkz( )[ ] [I-5]
so that the spatial partial derivatives simplify to
x
r
Err, ( ) =
r
E ( )
xexp j
rr
r
k( ) =r
E ( ) j kx[ ] exp jrr r
k( ) [I-6a]
y
r
Err, ( ) =
r
E ( )y
exp jrr
r
k( ) =r
E ( ) j ky[ ] exp jrr r
k( ) [I-6b]
z
rE
rr, ( ) =
rE ( )
z
exp jrr
rk( ) =
rE ( ) j kz[ ] exp j
rr
rk( ). [I-6c]
Therefore
r
rE
rr, ( ) =
r
rE ( ) exp j
rr
rk( ) = j
rk
rE
rr, ( ) [I-7a]
r
rE
rr , ( ) =
r
rE ( ) exp j
rr
rk( ) = j
rk
rE
rr , ( ) [I-7b]
and Maxwell's equations in a charge/current free regionbecome
jrk rE rr, ( ) = j 0 rH rr, ( ) [I-8a]
j
rk
rH
rr, ( ) =j ( )
rErr, ( ) [I-8b]
j
rk
rErr, ( ) = 0 [I-8c]
j
r
k r
Hrr , ( ) = 0 [I-8d]
Operate through on both sides of Equation [I-8a] with the operator "rk "
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R. Victor Jones, October 23, 2002
r
k r
k r
Err , ( )[ ] = 0
r
k r
Hrr, ( ) [I-9a]
and using the "bac-cab" rule1and Equation [I-8b] this becomes
rk rk rE rr, ( )[ ] rk rk[ ] rE rr , ( ) =
2 0 ( ) rE rr, ( ) [I-9b]
or finally
r
k r
k[ ]r
Err ,( ) = 2 0 ( )
r
Err, ( ) k2 = 2 0 ( ) [I-9c]
Substituting into Equation [I-8a]
r
H
r
r, ( ) = 0( )
1
k
k
r
E
r
r, ( )[ ] = ( ) 0
k
r
E
r
r , ( )[ ] [I-10]
so that the wave impedance is given by
( ) =
r
Err, ( )
r
Hrr, ( ) = 0 ( ) . [I-11]
Thus, the complete expression for an electromagnetic plane wave propagating in a direction
k is
r
Err, t( ) =
r
E ( ) exp jrr r
k t( )[ ] [I-12a]
rH
rr, t( ) = ( )[ ]
1k
rE
rr, ( )[ ] [I-12b]
1 That is
ra
r
b rc( ) =
r
bra
rc( )
rcra
r
b( ) .
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II. ELECTROMAGNETIC INTERFACIAL CONTINUITY CONDITIONS:
The previous section gives a completeplane wave solution within a particularuniform,
linear, isotropic medium. The key remaining problem is to find how that solution may be
extended into a second uniform, linear, isotropic medium. The conditions for extendingthe solution across an interface between two materials are give by consideration of the
appropriate integral forms of Maxwell's equations -- viz.
rE
rr, t( ) d
rl = t
rBrr, t( ) d
rA [II-1a]
rH
rr, t( ) d
rl =
rJrr, t( ) d
rA + t
rD
rr , t( ) d
rA [II-1b]
Applying these equations to the smallthought loopthat spans the interfacial surface, as
illustrated below
Medium 1
Medium 2
Interface1, 1, 1[ ]
2 , 2 , 2[ ]L
l"Thought"loop
r
r
it is seen that Equation [II-1a] yields
rE
rr, t( ) d
rl
rE2
rr, t( )
rE1
rr , t( ){ }
r L 0 [II-2]
unlessrBrr, t( ) is pathologically large over the loop. Similarly, it is seen that Equation
[II-1b] yields
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R. Victor Jones, October 23, 2002
r
Hrr, t( ) d
r
l r
H2rr , t( )
r
H1rr, t( ){ }
r L 0 [II-3]
unlessr
Jrr, t( ) and/or
r
Drr, t( ) are pathologically large over the loop.
In words and in general, the tangential component of the electric
field strengthrE
rr, t( ) and the magnetic field strength
rH
rr, t( )are
continuous across an interfacial surface between two materials
unless electric current densityrJrr, t( ) , the magnetic flux density
r
Brr, t( ) , or the electric flux density
r
Drr, t( ) are pathologically
large near that interfacial surface.
III. THE FRESNEL EQUATIONS:Consider then a plane wave incident on a planar interfacial surface.
The Spatial Configuration:2
2
Note: In this figure we have taken the plane of reflect ionto be identical to the plane of incidence. Whileassumed here for simplicity, this important identity is establish in the analysis below.
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The Mathematical Representation of F ields :
In abstract vector form, the incident field is given by3
rE inc =
rE
inc 1 kinc
rH||
inc{ } exp jk1 k incrr( )
rH
inc = rH ||inc + 1
1k
inc rEinc{ } exp j k1 k inc rr( ) [III-1a]
the reflected field is given by
rE ref =
rE
ref 1 kref
rH||
ref{ } exp j k1 k refrr( )
r
Href =
r
H ||ref + 1
1k
ref r
Eref{ } exp j k1 kref
rr( )
[III-2]
and the transmitted field is given by
rE tran =
rE
tran 2 ktran
rH||
tran{ } exp j k2 ktranrr( )
rH
tran =rH||
tran + 21
ktran
rE
tran{ } exp j k2 ktranrr( )
[III-3]
In coordinate form these equations become:
rE inc = E
incy 1 cosinc x + sin inc z[ ] H||incy[ ]{ } exp j k1 x cos inc +zsin inc( )[ ]
rHinc = H ||
incy + 11 cos inc x + sininc z[ ] E
incy[ ]{ } exp j k1 x cos inc + zsin inc( )[ ][III-1b]
r
E ref = Erefy 1 cos ref x + sin ref z[ ] H ||
refy[ ]{ } exp j k1 xcos ref +zsin ref( )[ ]rH ref = H||
refy + 11 cos ref x + sin ref z[ ] E
refy[ ]{ } exp j k1 x cosref +zsin ref( )[ ][III-2b]
3 A note on notation: The subscripts and || refer to the polariztion of the electric field taken with respect to the
plane of incidence. The field components are also called transverse electricor TE components and the||
field components are called transverse magnetic or TM components.
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rE tran = E
trany 2 cos tran x + sin tran z[ ] H ||trany[ ]{ } exp j k2 x costran +zsin tran( )[ ]
rH tran = H||
trany + 21 cos tran x + sin tran z[ ] E
tran y[ ]{ } exp j k2 x cos tran +z sintran( )[ ][III-3b]
Or expanding out the cross-products:
rE
inc = Einc
y + 1 H ||inc( ) cos inc z + sininc x[ ]{ } exp j k1 xcos inc +zsin inc( )[ ]
rH inc = H ||
incy 11 E
inc( ) cos inc z + sininc x[ ]{ } exp j k1 xcosinc +zsin inc( )[ ][III-1c]
rE
ref = Eref
y + 1 H||ref( ) cos ref z + sin ref x[ ]{ } exp j k1 xcos ref +zsin ref( )[ ]
rH ref = H||
refy 11 E
ref( ) cosref z+ sinref x[ ]{ } exp j k1 x cosref +zsin ref( )[ ][III-2c]
r
E tran = Etrany + 2 H||
tran( ) costran z + sin tran x[ ]{ } exp j k2 x cos tran +zsin tran( )[ ]rHtran = H||
trany 21 E
tran( ) cos tran z +sin tran x[ ]{ } exp j k2 xcos tran +zsin tran( )[ ][III-3c]
Applying any kind of continuity conditions at the interface requires that
ref = inc Law of Sinus [III-4a]
k2 sin tran = k1 sininc Law of Snell [III-4b]
Applying, in particular, the continuity conditions discussed in the previous section -- viz.
rE
1[ ]tang
=rE
2[ ]tang
andrH
1[ ]tang
=rH
2[ ]tang
[III-5]
at the interface, requires that
Einc + E
ref = Etran
1
1cos
inc
E
inc E
ref
[ ]=
2
1cos
tran
E
tran
[ ]
[III-6]
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and that
H||inc + H ||
ref = H||tran
1 cos inc H||inc H||
ref[ ] = 2 costran H ||
tran[ ]
[III-7]
These two sets of equations yield the Fresnel Reflection Equations
E ref
Einc =
11cos inc 2
1 cos tran1
1cosinc +2
1cos tran
[III-8a]
and
H||ref
H||inc =
1 cosinc 2 costran1 cosinc +2 costran
[III-9a]
Since 11
sin inc = 21
sin tran
E ref
Einc =
cos inc sintran cos tran sin inccos inc sin tran + cos tran sin inc
=sin tran inc( )sin tran + inc( )
[III-8b]
and
H||ref
H||inc =
cos inc sininc cos tran sin trancos inc sin inc + cos tran sintran
=tan inc tran( )tan inc + tran( )
[III-9b]
These equations taken together with first equations from Equations [III-6] and [III-7] yield
the Fresnel Transmission Equations -- i.e.
Etran
Einc =
2 cosinc sintrancosinc sintran + cos tran sininc
[III-10]
and
H||tran
H||inc =
2 cos inc sininccos incsin inc + costran sin tran
[III-11]
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FAMOUS FRE SNEL REFLECTION CURVES ( n2 n1 = 1 n2 = 2 1 =1.5 )
The minimum (zero) in H ||ref
H||inc
occurs at the Brewster angle where
tan incBrewster + tran
Brewster( ) [III-12a]
or tranBrewster = 2 inc
Brewster[III-12b]
or (from Snell's equation)
tan incBrewster = 1 2 = n2 n1 = 2 1 . [III-12c]
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Total Internal Reflection
Reconsider Equation [III-3c] and use Snell's law to write the exponential factors in the
form
rE
tran = Etran
y + 2 H||tran( ) costran z + sin tran x[ ]{ } exp j x k2
2 k12
sin2 inc[ ] exp j z k1sin inc[ ] [III-13]
When sininc > k2 k1 = n2 n1 sin inccrit
,rE
tran, the solution in medium 2, is
attenuated!
incident
beam
attenuated
f ie ld
Reconsideration of Equation [III-8a] and [III-9a] shows that the magnitude of the
reflection coefficients are onewhen sininc > sininccrit
-- viz.
E ref
Einc =
cos inc j sin2 inc k2 k1( )
2
cos inc + j sin2 inc k2 k1( )
2
= exp j 2 tan1sin2 inc k2 k1( )
2
cos inc
[III-14a]
and
H||ref
H||inc =
cos inc j k1 k2( )2
sin2 inc 1
cos inc + j k1 k2( )2
sin2 inc 1
= exp j 2 tan1k1 k2( )
2sin2 inc 1
cos inc
. [III-14b]
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IV. A DIFFERENT "TAKE" ON THE FRESNEL EQUATIONS:
Equations [III-1c] through [III-3c] may be rewritten in the following form:
rE inc = E
inc y + H||inc 1 cosinc( ) z + H||
inc 1 sin inc( ) x} exp jk1 x cosinc +z sininc( )[ ]rH inc = H||
incy Einc 1
1 cosinc( ) z Einc 1
1 sin inc( ) x{ } exp j k1 x cosinc +zsin inc( )[ ] [IV-1a]
r
E ref = Erefy H||
ref 1 cos ref( ) z + H||ref 1 sin ref( ) x{ } exp j k1 x cos ref +z sinref( )[ ]
rH ref = H ||
refy + Eref 1
1 cosref( ) z Eref 1
1 sin ref( ) x{ } exp j k1 x cos ref +zsin ref( )[ ][IV-1b]
r
E tran = Etrany + H ||
tran 2 cos tran( ) z + H ||tran 2 sin tran( ) x{ } exp j k2 x costran +zsin tran( )[ ]
rHtran = H||
trany Etran 2
1 cos tran( ) z Etran 2
1 sin tran( ) x{ } exp j k2 xcos tran +zsin tran( )[ ][IV-1c]
Notice: If = cos is interpreted as the
characteristic impedance of a wave polarized perpendicular to
the plane of incidence (TE wave) which is propagating at an
angle with respect to the normal of an interfacial plane and
if || = cos is interpreted as the characteristic
impedance of a wave polarized parallel to the plane ofincidence (TM wave) which is propagating at an angle with
respect to the normal of an interfacial plane, then the whole
analysis of specular reflection fits neatly into transmission line
theory .
In particular, a re-interpretation the famous transmission line equation for the
voltage reflection coefficient
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V z,( ) =Z z,( ) Zc ( )Z z,( ) + Zc ( )
[IV-2]
yields an equation for the electric field strength reflection coefficient at the interfacial plane
for TE waves
=
tran inc
tran +
inc =2 costran 1 cosinc2 cos tran + 1 cosinc
[IV-3]
which is in precise agreement with Equation [III-8a] -- i.e.
E ref
Einc =
11cos inc 2
1 cos tran1
1cosinc +2
1cos tran
.
Similarly, a re-interpretation the equally famous transmission line equation for the current
reflection coefficient
I z ,( ) =Y z ,( ) Yc ( )Y z,( ) + Yc ( )
[IV-4]
yields an equation for the magnetic field strength reflection coeficient at the interfacial plane
for TM waves
|| =1 ||
tran 1 ||inc
1 ||tran +1 ||
inc =1 2 costran 1 1 cosinc1 2 cos tran +1 1 cosinc
[IV-5]
which is in precise agreement with Equation [III-9a] -- i.e.
H||ref
H||inc =
1 cosinc 2 costran1 cosinc +2 costran
.
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V. PARALLEL PLATE WAVEGUIDE:
Consider the propagation of a plane wave between two parallel perfectly conducting planes.
Perspective view Side view
Combining Equations [III-1c] and [III-2c], the electric field strength of the TE wave in the
region between the plates may be written
rE = y E
incexp j x k1 cosinc( ) + E
refexp j x k1 cosinc( )[ ] exp j z k1 sin inc( ) [V-1]
At x = 0 the field parallel to the surface of a perfect conductor must be zero so thatE
ref = Einc
and, therefore,
r
E = y E inc exp j x k1 cos inc( ) exp j x k1 cos inc( )[ ] exp j z k1 sininc( )= y 2j E
inc sin x k1 cos inc( ) exp j z ( )[V-2]
where = k1 sininc . At the upper surface -- i.e. x = d-- the field parallel to the surface of
a perfect conductor must also be zero so that
d k1 cos inc = n where n = 1,2,3,K [V-3]
and, therefore,
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TE n = k1 sin inc = k1
2 k12
cos2 inc = k1
2 n d( )2
where n =1, 2,3, K [V-4]
which is the dispersion relationship for TE waves in a parallel plate
waveguide with "cutoff" frequencies at
n
cutoff = n d( ) 0 1( )1
where n = 1,2,3,K [V-5]
Again combining Equations [III-1c] and [III-2c], the electric field strength of the TM wave
in the region between the plates may be written
rE|| = z 1 cos inc( ) H||
incexp j x k1 cos inc( ) H||
refexp j x k1 cos inc( ){ } exp j z k1 sininc( )
+ x 1 sin inc( ) H ||inc exp j x k1 cosinc( ) + H||
ref exp j x k1 cos inc( ){ } exp j z k1 sin inc( )[V-6]
At x = 0 the field parallel to the surface of a perfect conductor must be zero so thatH||
ref = H ||inc
and, therefore,
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rE|| = z 2j H ||
inc 1 cosinc( ) sin x k1 cosinc( ) exp j z ( )
+x 2 H||inc 1 sin inc( ) cos x k1 cos inc( ) exp j z ( )
[V-5]
where = k1
sininc
. At the upper surface -- i.e. x = d-- again the field parallel to the
surface of a perfect conductor must also be zero so that
d k1 cos inc = n where n = 0,1, 2,3,K [V-7]
and, therefore,
TM n = k1 sin inc = k1
2 k12
cos2 inc = k1
2 n d( )2
where n = 0,1,2,3,K [V-8]
which is the dispersion relationship for TM waves in a parallel platewaveguide.
Note that the TM0 mode is a bona fide mode of propagation which does not
have a "cutoff" frequency!
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VI. DIELECTRIC SLAB WAVEGUIDE:
Consider the propagation of waves "trap in" or "guided by" a dielectric slab of thickness d.
In its full generality this is moderately complicated problem, but a rather simple ray optics
model of the propagation is sufficient to yield dispersion relationships for the various
possible modes of propagation. To obtain such relationships, consider the total internal
reflection of a sequence of plane waves as illustrated below.
x
z
k inc
d
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In order for the multiple reflected wave to be self-consistence the following, relatively
obvious, phase condition must hold:4
x =d + x =0 + 2 k1 dcos inc = m 2 where m = 0,1,2, 3,K [VI-1]
where x =d and x =0 are, respectively, the phase shifts associated with the reflections at
the upper and lower dielectric boundaries.
For TE-modes of propagationEquation [III-14a] gives the phase shift at the boundary
(called in the trade the TE Goos-Hnchen shift) and Equation [VI-1] becomes
2 tan1sin2 inc sin
2 inccrit
cos inc
+ k1 dcosinc = m [VI-2]
where sininccrit k2 k1 = n2 n1 = 2 1 . Therefore, the self-consistence relationship
for TE is given by
sin2 inc sin2 inc
crit
cos inc= tan
n1 k0 dcos inc2
m2
[VI-3]
where k0 = c = 2 0 . This is a transcendental equation in the single variable cosinc .
Its solutions yield the allowed bounce angles, inc( )m , of possible modes and, hence, theallowed propagation constants since = k1 sininc The left and right sides of this equationmay be plot as a function of cosinc with n1 k0 d= n1 2 d 0( ) and sininc
crit = n2 n1 as a
parameters. The intersections of such curves yield the allowed bounce angles as illustrated
below
4 This equation is a direct generalization of Equations [V-3] and [V-7] which figure in our analysis of parallel
plane waveguides.
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LHS and RHS of Equation [VI-3] LHS and RHS of Equation [VI-3]
for n1 d 0( ) = 0.5 and cosinccrit = 0.5 for n1 d 0( ) = 1.0 and cosinccrit = 0.5
LHS and RHS of Equation [VI-3] LHS and RHS of Equation [VI-3]
for n1 d 0( ) = 1.5 and cosinccrit = 0.5 for n1 d 0( ) = 2.0 and cosinc
crit = 0.5