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...@@ -39,7 +39,7 @@ while the third and fourth ...@@ -39,7 +39,7 @@ while the third and fourth
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will give information on the tangential components of $`\overrightarrow{E}`$ and $`\overrightarrow{H}`$. will give information on the tangential components of $`\overrightarrow{E}`$ and $`\overrightarrow{H}`$.
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To obtain the boundary conditions we consider a surface separating two To obtain the boundary conditions we consider a surface separating two
Linear Homogeneous and Isotropic (LHI) media whose properties such as that Linear Homogeneous and Isotropic (LHI) media whose properties such as that
the permittivity and permeability are different. We denote as the permittivity and permeability are different. We denote as
...@@ -47,159 +47,152 @@ $`\overrightarrow{E}_1\,,\overrightarrow{B}_1\,,\overrightarrow{D}_1`$ and $`\ov ...@@ -47,159 +47,152 @@ $`\overrightarrow{E}_1\,,\overrightarrow{B}_1\,,\overrightarrow{D}_1`$ and $`\ov
material 1 close to its surface. Likewise an index 2 will be used for material 1 close to its surface. Likewise an index 2 will be used for
the fields in the second material. the fields in the second material.
Figure 3.1: []{#_bookmark59 .anchor}Scheme for deriving boundary ![](electromag-in-media-reflexion-transmission-fig-31.jpg)
conditions for perpendicular field components. S~1~, S~2~ and S^t^ _Figure 3.1 : Scheme for deriving boundary conditions for perpendicular field components._
represent respectively the surface at the top, bot- tom and interface. _$`S_1\,, S_2`$ and $`S'`$ represent respectively the surface at the top, bot- tom and interface._
> >
__**Normal components**__ ##### Normal components
__D vector__ __D vector__
Let's apply Maxwell equation (i) to the small cylinder showed in Let's apply Maxwell equation (i) to the small cylinder showed in
figure [3.1](#_bookmark59) which extends from one side to the other on figure [3.1] which extends from one side to the other on
the separation surface. This box has a base surface A and an the separation surface. This box has a base surface A and an
infinitesimally small thickness *δ*. We get: infinitesimally small thickness $`\delta`$. We get:
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tS $`\overrightarrow{D}`$ · d**a** = {S
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$`\overrightarrow{D}`$~1~ · d**a**~1~ + {S
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$`\overrightarrow{D}`$~2~ · d**a**~2~ + {S
side @@@@@@@@@@@@@@@@@@@@@@@@@
$`\overrightarrow{D}`$ · d**a** = {*V* If we now let $`\delta\longrightarrow 0`$ symmetrically with respect to the separation
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*ρ~c~* d*V.*
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If we now let *δ* 0 symmetrically with respect to the separation
surface such that the cylinder gets "pressed" onto the surface: surface such that the cylinder gets "pressed" onto the surface:
- The third term on the left hand side of the previous equation will * The third term on the left hand side of the previous equation will
be negligible as the flux of the vector $`\overrightarrow{D}`$, which is a finite be negligible as the flux of the vector $`\overrightarrow{D}`$, which is a finite
quantity, through an infinitesimally small surface will approach quantity, through an infinitesimally small surface will approach
0. 0.
- The volume charge will be reduced to a surface charge at the * The volume charge will be reduced to a surface charge at the
interface only as the volume will approach 0. The volume charge interface only as the volume will approach 0. The volume charge
density is re- placed by a surface charge density *σ~s~* and the density is replaced by a surface charge density $`\sigma`$ and the
volume integral is replaced by surface integral over the middle volume integral is replaced by surface integral over the middle
surface S^t^. surface $`S'`$.
We obtain: We obtain:
{S1 {S {Sl @@@@@@@@
$`\overrightarrow{D}`$~1~ · d**a**~1~ + $`\overrightarrow{D}`$~2~ · d**a**~2~ = *σ~s~* d*a.* (3.7) Now, considering that $`d\overrightarrow{a_2}=-d\overrightarrow{a_1}`$ we can write:
>
Now, considering that d**a**~2~ = −d**a**~1~ we can write:
{S ($`\overrightarrow{D}`$~1~ − $`\overrightarrow{D}`$~2~) · d**a**~1~ = {Sl *σ~s~* d*a.* (3.8) @@@@@@@@@@@@@
Finally, as S~1~ = S^t^ and d**a**~1~ = **nˆ**~2→1~d*a*~1~ we can Finally, as $`S_1=S'`$ and $`d\overrightarrow{a_2}=\overrightarrow{n}_{2\rightarrow 1}\,da_1`$ we can
write: write:
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**nˆ**~2→1~ · ($`\overrightarrow{D}`$~1~ − $`\overrightarrow{D}`$~2~) = *σ~s~* (3.9) @@@@@@@@@
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or or
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*D*~1*n*~ − *D*~2*n*~ = *σ~s~* (3.10) @@@@@@@@@@@
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The normal component of the vector $`\overrightarrow{D}`$ is in general discontinuous. The normal component of the vector $`\overrightarrow{D}`$ is in general discontinuous.
It is continuos only if there are no conduction charges at the It is continuos only if there are no conduction charges at the
separation surface. separation surface.
__chap5 B vector__ __B vector__
The situation is identical for the vector $`\overrightarrow{B}`$, the only difference The situation is identical for the vector $`\overrightarrow{B}`$, the only difference
being that the right hand side of the equation is always 0. We being that the right hand side of the equation is always 0. We
conclude that: conclude that:
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**nˆ**~2→1~ · ($`\overrightarrow{B}`$~1~ − $`\overrightarrow{B}`$~2~) = 0 (3.11) @@@@@@@@@
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or or
>
*B*~1*n*~ − *B*~2*n*~ = 0 (3.12) @@@@@@@@@
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The normal component of $`\overrightarrow{B}`$ is always conserved. The normal component of $`\overrightarrow{B}`$ is always conserved.
__**Tangential components**__
![](media/image171.jpeg) ##### Tangential components
Figure 3.2: []{#_bookmark60 .anchor}Contour for deriving boundary ![](electromag-in-media-reflexion-transmission-fig-32.jpg)
conditions for parallel field com- ponents. _Figure 3.2 : Contour for deriving boundary conditions for parallel field components._
__chap5 E vector__ __chap5 E vector__
We integrate the third Maxwell equation around the rectangular contour We integrate the third Maxwell equation around the rectangular contour
C that straddles the boundary of width W and thickness *δ* as shown in C that straddles the boundary of width W and thickness $`\delta`$ as shown in
figure [3.2.](#_bookmark60) We chose to integrate the line integral figure [3.2.]. We chose to integrate the line integral
following the right-hand sense relative to the surface normal following the right-hand sense relative to the surface normal
**nˆ***~a~*. By letting *δ* → 0, we get $`\overrightarrow{n_a}`$. By letting $`\delta\right 0`$, we get
>
t $`\overrightarrow{E}`$ · *d***l** = $`\overrightarrow{E}`$~1~ · *A_B* + $`\overrightarrow{E}`$~2~ · *C_D* = − @@@@@@@@@@@
[d]{.underline} { $`\overrightarrow{B}`$ · *d*$`\overrightarrow{S}`$ → 0 (3.13)
>
as the line integral along the sides goes to zero and the flux of the as the line integral along the sides goes to zero and the flux of the
induction field $`\overrightarrow{B}`$, which is a finite quantity, approaches 0. induction field $`\overrightarrow{B}`$, which is a finite quantity, approaches 0.
Considering that *C_D* = Considering that $`\overrightarrow{CD}-\overrightarrow{AB}=d\overrightarrow{l}`$, we get:
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*A_B* = d**l**, we get: @@@@@@@@@@
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($`\overrightarrow{E}`$~1~ − $`\overrightarrow{E}`$~2~) · d**l** = 0 ∀d**l** /I to the separation
surface (3.14)
>
or again or again
*E*~1*T*~ − *E*~2*T*~ = 0 (3.15) @@@@@@@@@@@@
i.e. the tangential components of the electric field are always i.e. the tangential components of the electric field are always
conserved at the interface. This condition can also be written: conserved at the interface. This condition can also be written:
>
**nˆ**~2→1~ ***×*** ($`\overrightarrow{E}`$~1~ − $`\overrightarrow{E}`$~2~) = 0*.* (3.16)
__chap5 H vector__ @@@@@@@@@@ $`\quad equ. 3.16)`$
Following the same reasoning as for the $`\overrightarrow{E}`$ vector we write for the __H vector__
left hand
>
side when *δ* → 0: $`\overrightarrow{H}`$
C Following the same reasoning as for the $`\overrightarrow{E}`$ vector we write for the
left hand side when $`\delta\right 0`$ :
· *d***l** = $`\overrightarrow{H}`$ $`\overrightarrow{H}`$
~1~ · *A_B* @@@@@@@@@@@@@ $`\quad equ. 3.17)`$
\+ $`\overrightarrow{H}`$~2~ · *C_D.*
>
(3.17)
>
The right hand side needs more attention. The flux of the vector $`\overrightarrow{D}`$ The right hand side needs more attention. The flux of the vector $`\overrightarrow{D}`$
approaches approaches 0. However the flux of the vector $`\overrightarrow{J}`$ over an infinitesimal surface
>
0\. However the flux of the vector $`\overrightarrow{j}`$ over an infinitesimal surface
can give a finite value: the surface integral reduces to an integral can give a finite value: the surface integral reduces to an integral
over the line of width W equal to the side of the rectangle. No volume over the line of width W equal to the side of the rectangle. No volume
current can contribute, however a surface current $`\overrightarrow{j}`$*~s~* (i.e. a current can contribute, however a surface current $`\overrightarrow{J}_S`$ (i.e. a
current flowing on the separation surface with dimensions \[*A/m*\] current flowing on the separation surface with dimensions $`[A/m]`$
not \[*A/m*^2^\] as $`\overrightarrow{j}`$) can. This is typically the case of a not $`[A/m*^2]`$ as $`\overrightarrow{J}`$) can. This is typically the case of a
perfect conductor where a finite current can flow through a perfect conductor where a finite current can flow through a
infinitesimally small area. We get: infinitesimally small area. We get:
>
@@@@@@@@ $`\quad equ. 3.18)`$
or again or again
>
($`\overrightarrow{H}`$~1~ − $`\overrightarrow{H}`$~2~) · d**l** = *J~s~* (3.18) @@@@@@@@ $`\quad equ. 3.19)`$
>
*H*~1*T*~ − *H*~2*T*~ = *J~s~* (3.19)
>
i.e. the tangential components of the magnetic field $`\overrightarrow{H}`$ is i.e. the tangential components of the magnetic field $`\overrightarrow{H}`$ is
discontinuous unless no surface currents exist. As for the electric discontinuous unless no surface currents exist. As for the electric
field, this condition can also be written: field, this condition can also be written:
>
**nˆ**~2→1~ ***×*** ($`\overrightarrow{H}`$~1~ − $`\overrightarrow{H}`$~2~) = $`\overrightarrow{j}`$*~s~* (3.20) @@@@@@@@ $`\quad equ. 3.20)`$
!! *Summary*
!!
! *Remarks*
!
! * If medium 1 & 2 are perfect dielectrics then there are no charges
! nor surface currents at the interface, and so the tangential component
! of $`\overrightarrow{H}`$ and the normal component of $`\overrightarrow{D}`$ are both continuous.
!
! * If medium 1 is a perfect dielectric and medium 2 is a perfect metal,
! there are charges and surface currents at the interface, and so the
! tangential component of $`\overrightarrow{H}`$ and the normal component of $`\overrightarrow{D}`$ are
! not continuous.
!
! * In case of linear media, the 4 relations can be expressed in terms
! of $`\overrightarrow{E}`$ and $`\overrightarrow{B}`$ alone using the constitutive relations
! $`\overrightarrow{D}=\epsilon\,$`\overrightarrow{E}`$ and $`\overrightarrow{B}=\mu\,$`\overrightarrow{H}`$.
&&&&&&&&&&&&&&&&&&&&&&&&&
#### chap2 Reflection and transmission at normal incidence #### chap2 Reflection and transmission at normal incidence
......
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