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Wilcox Chapter1R
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Course notes for Chapter 1 (Introduction to Electrostatics) in Gaussian units, apparently from a lecture series by Wilcox. They cover Coulomb's law, Dirac delta functions in curvilinear coordinates, Gauss' law and solid angles, tests for deviations from the inverse square law, surface charge and dipole layers, uniqueness under Dirichlet, Neumann and mixed boundary conditions, and Dirichlet and Neumann Green functions.
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1.1
Chapter 1: Introduction to Electrostatics
1.1 Electric field definition
We begin at a very basic level. Definition of E≥ in terms
of a test charge, q:
F≥ = q E≥. (1.1)
Coulomb's law in the Gaussian system of units:
F≥
12 = q1q2 x≥
1-x≥
2
|x≥
1-x≥
2|3. (1.2)
(force of 2 on 1) Picture:
q2
x2≥>x≥
origin
x≥>x≥qx-x2 >x-x≥≥ ≥ ≥'
'
11
1
E2≥(x≥
1) = q2 x≥1-x≥
2
|x≥
1 - x≥
2|3 or E≥(x≥) = q x≥- x≥'
|x≥ - x≥'|3(1.3)
For a charge density:
E≥(x≥) = ∫ d3x'ρ(x≥') x≥-x≥'
|x≥ - x≥'|3. (1.4)
(Similarly for surface charge or line charge densities.) Of
course, if we choose ρ = q δ (x≥-x≥'), we get back the previous
discrete expression.
1.2
1.2 Dirac delta function properties
One way to define Dirac delta functions:
δ (x-x') ≡ α .0lim 1
α√⎯⎯2π exp[- 1
2α2 (x-x')2],
| < >|~å
x=x~1/ å
'
We get
∫ -∞ ∞
δ(x-x') d(x-x') = 1
α√⎯⎯2π ∫ -∞∞
dx e-1/(2α2)x2 = 1.
(Easy way of seeing the last integral:
I ≡ ∫ -∞∞
dxe-ax2,
I2 = ∫ dx ∫ dx'e-a(x2+x'2) = ∫ rdφdre-ar2,
= 2π∫
0∞
drr e-ar2 = 2π 1
2a = π
a .)
In 3-D space:
δ (x≥-x≥') ≡ α .0lim
⎝⎜⎜⎛
⎠⎟⎟⎞1
α√⎯⎯2π 3 exp[ -1
2α2 [(x-x')2+(y-y')2+(z-z')2]].
1.3
Generalize it to any other orthogonal coordinate system:
old: ds2 = dx2 + dy2 + dz2
new: ds2 = du2
U2 + dv2
V2 + dw2
W2
U,V,W are called "scale factors" (they are intrinsically
positive)
old: d3x = dxdydz
new: d3x = du dv dw
U.V.W
((UVW)-1 is just the Jacobian of the transformation, where U-1
= |∂x≥
∂u|, etc.) General idea:
δ(x≥-x≥') =α .0lim
⎝⎜⎜⎛
⎠⎟⎟⎞1
√⎯⎯2π α 3 exp[-1
2α2(extendedinfinitismal length element)]
δ(x≥-x≥') = α .0lim
⎝⎜⎜⎛
⎠⎟⎟⎞1
√⎯⎯2π α 3 exp[-1
2α2((u-u') 2
U2
+ (v-v') 2
V2 + (w-w') 2
W2)]
=> δ(x≥-x≥') = δ ⎝⎜⎛
⎠⎟⎞u-u'
U δ ⎝⎜⎛
⎠⎟⎞v-v'
V δ ⎝⎜⎛
⎠⎟⎞w-w'
W.
Given (useful in many other situations)
δ(f(x)) = ∑
i 1
|df
dx(xi)| δ (x≥-x≥
i),
so
δ(ax) = 1
a δ(x),
=> δ(x≥-x≥') = U V W δ (u-u') δ (v-v') δ (w-w').
1.4
Makes sense since this now gives
∫ δ(x≥-x≥')d3x = ∫ U V W δ (u-u') δ (v-v') δ (w-w') x dudvdw
U V W,
= 1. √
In particular, can show that the repn of the 3-D delta
function in spherical coord. is
δ(r≥-r≥') = 1
r2 δ ( r-r') δ(cosθ − cosθ ') δ (φ -φ').
These three dimensional delta functions can be "smeared"
or integrated over some dimensions or objects, producing newlower dimensional delta functions. For example, the "linedelta function" seen in the introduction is nothing but a 2dimensional delta function integrated over the line inquestion. Then, an integration across the line producesunity. These delta functions can also be "directed"; that is,the result can depend on the direction of integration. Wewill see these types of objects repeatedly in Chs.5 and 6.
1.3 Gauss' law and solid angles
The integral of the normal component of E≥ due to point
charges is given as follows.
n^
Vcontains charges
q , =1,...,njj
S
1.5
∫o
s da n^.E≥ = ∑
j qj ∫o
s da n^.x≥-x≥
j
|x≥ -xj ≥| 1
|x≥ -xj ≥|2(1.5)
Here
da n^ = ds≥, (1.6)
is the outward directed element of surface area. Then
da n^.x≥-x≥
j
|x≥ -xj ≥| = ds≥.x≥-x≥
j
|x≥ -xj ≥| = ds|| (1.7)
unit vector along( away from)the line from the j th charge
where ds || is the component || to the "line of sight" from the
jth charge:
ds≥= nda^
x-xj≥ ≥
qxj≥x≥
j
Thus, since
ds|| rds
r2Ωd ||=
=> dΩj = da n^ . x≥-x≥
j
|x≥ -xj≥|3 ()+ for charge "inside"
- for charge "outside"(1.8)
1.6
Interpretation: solid angle subtended by ds≥ as seen from
location of jth charge. There are now 2 possible situations:
jV
jV
∫o dΩj= 4π∫ o dΩj= 0
Reason (simple object):
ds≥
jx-xj≥≥
overall
neg.contributionoverall pos.
contribution
cancel
Hence
∫o
s da n^.E≥ = ∑
j in V 4π qj. (1.9)
This is a statement about the global behavior of E≥. We need
to get statements about the local behavior of E≥; that is, we
need differential equations (supplemental by BC's). Canalways imagine a charge density as being due to point chargesin infinitismal volumes. Then we may replace
∑
j in V qj .∫
V d3xρ(x≥). (1.10)
Now, our flux statement becomes (by Gauss)
1.7
4π ∫v d3x ρ(x≥) = ∫o
s da n^.E≥ = ∫v d3x ∇≥.E≥
(x≥
). (1.11)
True for an arbitrary volume, V. Result:
∇≥.E≥ = 4πρ(x≥
). (1.12)
We notice that
E≥
(x≥
) = ∫ d3x'ρ(x≥
') x≥-x≥'
|x≥-x≥'|3 = -∇≥Φ (x≥
), (1.13)
where Φ(x≥
) (the "scalar potential") is given by
Φ(x≥
) = ∫ d3x' ρ(x≥')
|x≥-x≥'|. (1.14)
Comparison with the above informs us that
∇2Φ (x≥
) = -4πρ(x≥
), (1.15)
and therefore that
∇2 1
|x≥-x≥'| = -4πδ (x≥-x≥'). (1.16)
(We also see that ∇≥×E≥= 0.) [There are also many direct ways
of showing (1.16).] A more general statement is in fact (x≥'-
x≥ .x≥ for convenience)
∇i∇j 1
r = 3xixj-r2δij
r5 - 4π
3 δijδ (x≥
) (1.17)
(r = | x≥|) This equation will be justified later in the
semester in Ch.5.
1.8
1.4 Deviations from inverse square law
Now that we have an expression for Φ (x≥
), we can talk
about searching for deviations from the inverse square law.
Assume
F≥
12 = q1q2 n^12
r122+δ,from 2 to 1, δ<<1 (1.18)
Regard q 1 as a test charge. Then
E≥
2 (x≥
1) = q2 n^12
r122+δ ,( 1.19)
=> Φ 2 (x≥
1) = q2
(1+δ)r121+δ. (1.20)
Verify last statement:
E≥
2 = -∇ ≥
1Φ2 = - q2
(1+δ) ∇≥
1 1
|x≥
1-x≥
2|1+δ (1.21)
= − q2
(1+δ) {- x≥
1-x≥
2
|x≥-x≥'|3+δ (1+δ)}. (1.22)
Picture:
θ
dsrr'σsphere
radius=R
dΦ = σds
(1+δ)r'1+δ(q = σS, S = 4 πR2) (1.23)
1.9
Imagine
rΦ(r)ab
What one can show is that
Φ(r) = Φin(r) + Φout(r), (1.24)
where
Φin = qa
(1-δ2) 1
2ar [(a+r)1-δ - (a-r)1-δ], (1.25)
Φout = qb
(1-δ2) 1
2br [(r+b)1-δ - (r-b)1-δ]. (1.26)
Now imagine connecting a wire between the spheres:
=> Φ(a) = Φ(b). (1.27)
Can show that this requires
qb ~~ qaδ
2(b-a) [a ln ⎝⎜⎛
⎠⎟⎞a-b
a+b + b ln ⎝⎜⎛
⎠⎟⎞4a2
a2-b2], (1.28)
so that q b vanishes when δ =0 (inverse square law.)
1.5 Surface charge and dipole layers
We learned in the introduction that
(D≥
2-D≥
1).^n21 = 4π σ, (1.29)
(E≥
2-E≥
1)×^n21 = 0. (1.30)
1.10
If both volumes are vacuum, then
(E≥
2-E≥
1).^n21 = 4π σ ( (E2-E1)n = 4π σ), (1.31)
and the potential is
Φ (x≥
) = ∫
s σ(x≥')da'
|x≥-x≥'|. (1.32)
This eqn is consistent with the statement about the
discontinuity in E≥. Can see it as follows. Imagine a flat
surface sheet of charge:
E≥ = -∇≥Φ = -∫
s da'σ (x≥
')∇≥ 1
|x≥-x≥'|, (1.33)
=> En = -∫
s
da'σ (x≥
')n^21.∇≥ 1
|x≥-x≥'|. (1.34)
↑↑↑↑constant vector
But remember
da' ^n21.∇≥ 1
|x≥-x≥'| = ds≥'.(x≥'-x≥)
|x≥-x≥'|3 = dΩ'. (1.35)
Observation position is now from x≥ (field position) rather
than x' (source position as it was before). Picture:
1.11
x'-x≥≥n^
21
≥≥x'
xorigin
can be "inside" or
"outside" relative to n21^.12
Also, remember that d Ω' >0 "inside", d Ω '<0 "outside."
=> En(x≥
) = -∫
s
σ(x≥')dΩ' , flat surfaces (all x≥). (1.36)
Now imagine we are very close to an arbitrary surface. We
can imagine partitioning the surface into an infinitismaldisk and a remainder:
2
1
≥x'
x≥n21^
disk
very close to surface(2-D cutout)
Because the fields are linear
E≥ = E≥
remainder + E≥
disk. (1.37)
But because we are very close to the disk's surface, it is
clear that σ(x≥') and n^21 are nearly constant over the
integration over the disk, so that
(E2,disk)n ≈ 2πσ, (1.38)
(E1,disk)n ≈ -2πσ. (1.39)
1.12
very near the surface. This means there is a discontinuity in
En near the surface given by
(E2-E1)n = 4πσ, (1.40)
as stated above. (The E n due to the remainder is obviously
continuous.) Since the contribution of the remainder toE
1n & E2n is not known, E 1n & E2n are separately unknown.
Another type of surface distribution is the dipole
layer.
2
1n21^
σ≥(x')
σ-≥d
(x')
Define
D(x≥') = lim
d(x≥') .0 σ(x≥')d(x≥'). (1.41)
One can show (see the derivation preceeding prob. 1.7; the
surface S = S 2)
|not a const.vector
Φ (x≥
) .d .0 ∫
s
D (x≥') n^21.∇≥' 1
|x≥-x≥'| da'
-dΩ(from field
point)'
=> Φ (x≥
) = -∫
s
D (x≥')dΩ'. (1.42)
For constant D this means that the potential is dependent
only on the perimeter of an open surface. (For a closed
1.13
surface see for prob. 1.19(b)). This implies (as before take
a small disk)
Φd
2 = 2πD,Φd
1 = -2πD . (1.43)
Rest is continuous => ( Φ2-Φ1) = 4πD. Really a local statement
at every point on surface. An easier way of seeing this last
result is
12n21^
σ
Previous result:
E1d
n = -2πσ (single layer).
Therefore, we have Etotal
n = -4πσ between the two layers, so
that
ΔΦ = -∫
E≥.d l≥ = 4πσd ⇒
d .0 4πD. (1.44)
1.6 Boundary conditions and uniqueness of solutions
General question: When are the solutions to the eqn s of
electrostatics,
∇≥.E≥ = 4πρ, ∇≥×E≥ = 0,
(or ∇2Φ = -4πρ, E≥ = -∇≥Φ)
unique? An application of Gauss ("Green's first identity"):
∫
v
( ƒ∇2ψ + ∇≥ψ.∇≥ƒ) d3x = ∫o
s da ƒ∂ψ
∂n . (1.45)
1.14
Suppose we have two solutions ( Φ1,2) whose B.C.'s are:
Dirichlet: Φ1|s= Φ2|s = f(x,y,z) (1.46)
Neumann:∂Φ1
∂n|s = ∂Φ2
∂n|s = g(x,y,z) (1.47)
Mixed:
⎭⎪⎪⎬⎪⎪⎫ Φ1|s' = Φ2|s'
∂Φ1
∂n|s" = ∂Φ2
∂n|s" S'U S" = S (1.48)
↑"union" ↑whole surface
(no overlap)
Let U = Φ1-Φ2. Then ∇2U = 0 in V and
U|s = 0 , Dirichlet (1.49)
∂U
∂n|s = 0 , Neumann (1.50)
U|s' = 0, ∂U
∂n|s" = 0, Mixed. (1.51)
Let ψ = ƒ = U in Green's first identity. Result:
∫
v
(U∇2U + (∇≥.U)2) d3x = ∫o
s daU ∂U
∂n |s . (1.52)
For all three cases, we have the rhs vanishing.
=>∫
v
d3x(∇≥U)2 = 0, (1.53)
=> ∇≥U = 0 in V,
=> U = const.
(For Dirichlet & Mixed cases we know that U| s = 0, so that the
constant is zero there.)
1.7 Dirichlet and Neumann Green functions
Rather than trying to solve for each charge distribution
as a special case, there is a more powerful method whichallows us to solve a class of problems with a given set of
1.15
BC's. Called Green functions. Let us say we are trying to
solve
∇' 2Φ (x≥') = -4 πρ (x≥'), (1.54)
in V. (Can have boundaries at infinity or in finite regions.)
The trick is first to solve
∇' 2G (x≥,x≥') = -4 πδ (x≥-x≥'), (1.55)
for the same volume. G (x≥,x≥') is then the potential of a point
charge at x≥, the BC of which are as yet totally unspecified.
(I probably should have introduced (1.55) as ∇2G (x≥
',x≥) = -4πδ
(x≥-x≥') to conform with the usage that x≥' is regarded as the
source and x≥ as the field coordinate. In any case you can
regard the coordinates inside as G(source, field).) We willuse this freedom of choice of BC to simplify our expressions.
"Green's second identity":
∫
v
d3x'( ƒ∇' 2ψ - ψ ∇' 2 ƒ) = ∫o
s da'[ ƒ∂ψ
∂n' - ψ ∂ ƒ
∂n']. (1.56)
Let ƒ = G (x≥,x≥'), ψ = Φ(x≥'). Then
=> ∫ d3x'[G(x≥,x≥') ∇' 2Φ(x≥') - Φ(x≥')∇' 2G(x≥,x≥')]
= ∫o
s da'[G(x≥,x≥') ∂Φ
∂n' - Φ(x≥') ∂G(x≥,x≥')
∂n'], (1.57)
LHS = -4 π∫ d3x'G (x≥,x≥')ρ (x≥') + 4πΦ (x≥). (1.58)
(n^ = outward normal) We now use the freedom of choice of BC
for G (x≥,x≥') to specifiy
GD(x≥,x≥
') = 0, x≥
' on S (Dirichlet). (1.59)
1.16
Then
Φ(x≥
) = ∫ d3x' GD(x≥,x≥') ρ (x≥') - 1
4π ∫o
s da'Φ(x≥') ∂ GD(x≥,x≥')
∂ n'. (1.60)
Physically, this Green function is the solution for the
potential of a +unit point charge at x≥
' in the presence of
grounded conductors.
For Neumann BC, we must be more careful. One must
realize that since
∇' 2GN(x≥,x≥') = -4 πδ (x≥-x≥'), (1.61)
=> ∫
v
d3x' ∇≥'.∇≥'GN(x≥,x≥') = -4 π, (1.62)
=> ∫o
s da'∂ GN(x≥,x≥')
∂ n' = -4π. (1.63)
One can not take ∂GN
∂n' = 0 on S in general. Easiest thing to do:
∂GN
∂n' = - 4π
S for x≥' on S. (1.64)
S = total surface area. Then
Φ(x≥
) = 1
S ∫s da'Φ(x≥') + ∫ d3x' GN(x≥,x'≥
)ρ (x≥')
≡ <Φ>s+ 1
4π ∫o da'GN(x≥,x≥')∂Φ
∂n'. (1.65)
A possible situation is to find the fields outside of:
("exterior problem")
1.17
take to ∞n^'
imaginary thin
"Neumann" tuben^'
n^'BC's specified
If we add the imaginary surfaces shown, then we have a
single surface, S, which has infinite area as we take theouter part to
∞. Clearly, we then have
<Φ>s = 0, (1.66)
and we may consistently take
∂GN
∂n' = 0, (1.67)
on the finite volumes. (Doesn't contradict ∫o
s ∂GN
∂n' da' = -4 π.)
Thus, G N(x≥,x≥') is the potential for a point charge for zero
normal electric field on the boundaries for the exterior
problem.
Can think of Dirichlet as (conductor has surface charge
density which excludes E≥ norm.)
1.18
conductor .∞ε()x'≥
x≥
Φ(x≥,x≥') = GD(x≥,x≥')
Can think of Neumann as ("Neumann conductor" has dipole
density which excludes E≥ tang. Has properties of a "dual
superconductor".)
x'≥
x≥
(dual superconductor)ε .0 "Neumann conductor" ( )
Φ(x≥,x≥') = GN(x≥,x≥')
For electrostatics then, Neumann is not as physical as
Dirchlet. It makes more sense, however, in fluid flow
problems. Note the ε .∞,0 remarks above. ε is the "dielectric
constant" to be introduced in Ch.4. I am saying that the ε .∞
limit of a point charge near a dielectric gives you the
correct Dirichlet Green's function for this geometry (except
that the conductor will be uncharged) and the ε . 0 limit in
the same situation gives the correct Neumann one. Note that
the inside fields in these cases may or may not be physical.
An important aspect of Green functions is the symmetry
property, G (x≥,x≥') = G (x≥',x≥
). We can show it as follows:
∫v d3x( ƒ∇2ψ - ψ∇2 ƒ) = ∫o
s da[ ƒ∂ψ
∂n - ψ∂ ƒ
∂n ]. (1.68)
Choose (Dirichlet case)
1.19
ƒ = GD(x≥",x≥
) , ψ = GD(x≥',x≥
)
=> ∫ d3x [G(x≥",x≥
) ∇2G(x≥',x≥
) - G (x≥',x≥
) ∇2G(x≥",x≥
)]
= ∫o da[G(x≥",x≥
) ∂
∂n G (x≥',x≥
) - G (x≥',x≥
) ∂
∂n G (x≥",x≥
)]. (1.69)
But of course since G D(x≥',x≥) = 0 for x≥
on S, we have
GD(x≥",x≥') = GD(x≥',x≥"). (1.70)
If we do the same thing for Neumann, the RHS does not
automatically vanish, and we get:
(GN(x≥",x≥') - GN(x≥',x≥")) = <GN(x≥",x≥
) - GN(x≥',x≥
)>s(x≥)(1.71)
However, each of these terms vanishes separately if S
includes the surface at infinity since
<GN(x≥',x≥
)>s(x≥) = 1
S ∫o
sda GN(x≥',x≥
) .R . ∞0 (1.72)
GN(x≥',x≥
) ~ 1
R (|x≥
| >> |x≥'| )
da ~ R2dΩ
S = 4πR2
(If we choose G N = const. on the surface at infinity, the RHS
of (1.71) still vanishes.) Therefore, G N(x≥",x≥') = GN(x≥',x≥")
also for the exterior Neumann problem. Is not necessarily
true for interior Neumann problems. Let's look at this insome more detail.
Have shown (G ≡ G
N ; x' ≡ x≥')
G(x", x') - G (x', x") = <G(x",x) - G(x',x) >s(x)(1.73)
1.20
=><G(x",x')-G(x',x") >s(x')=<G(x",x)>s(x )-<G(x',x)>s(x),s(x')
source | | field
=><G(x', x")>s(x') ≡ const. (1.74)
Note that (1.74) implies
∂
∂n' <G(x, x')>s(x) = <∂
∂n' G(x, x')>s(x) = 0. (1.75)
But we also have that
∂
∂n' G(x, x') = -4π
S, (1.76)
for x' on S. Therefore, it would seem from (1.76) that
<∂
∂n' G(x, x')>s(x) = -4π
S, (1.77)
contradicting (1.75) above. We can clear this up with the
hypothesis that there is a surface delta function lurking in
(1.76). The hypothesis is that
∂
∂n' G(x, x') = -4π
S +4πδ(s)(x-x'). (1.78)
[What the last statement really means is
lim
x' .s ∂
∂n' G(x, x') |x on s = -4π
S + 4πδ(s)(x-x'). ]
This is now consistent with (1.75) since
∂
∂n' <G(x, x')>s(x) = <∂
∂n' G(x, x')>s(x) = -4π
S + 4π
S = 0.(1.79)
We can confirm this hypothesis from our earlier expression
for Φ:
1.21
Φ(x≥
) = <Φ>s + ∫ d3x' G(x,x') ρ(x') + 1
4π ∫o
s da'G(x,x') ∂Φ
∂n',(1.80)
which implies ∂Φ
∂n
|s =∫ d3x' ∂
∂n G(x,x') ρ(x') + 1
4π ∫o
s da' ∂
∂n G(x,x') ∂Φ
∂n' .
(1.81)
(Note an indescretion here: the normal derivatives are on the
first, not second arguments of G(x,x'). We will clear this upin prob. 1.7.3.) This must reduce to an identity:
∂Φ
∂n|s = ∫ d3x'{-4π
S + 4πδ (s)(x-x')}ρ(x')
+ 1
4π ∫o
s da'{-4π
S + 4πδ (s)(x-x')}∂Φ
∂n', (1.82)
=> ∂Φ
∂n|s = -4πQ
S + 4π ∫ d3x'δ(s)(x-x') ρ(x') - 1
S ∫o
s da'∂Φ
∂n' + ∂Φ
∂n|s.
(1.83)
But
-1
S ∫o
s da' ∂Φ
∂n' = -1
S ∫ d3x'∇' 2Φ(x') = 4πQ
S. (1.84)
-4ρx'()π
Therefore
∂Φ
∂n|s = ∂Φ
∂n|s + 4π∫ d3x'δ(s)(x-x') ρ(x'), (1.85)
and consistency is maintained as long as we take
∫ d3x'δ(s)(x-x')f(x') = 0, (1.86)
for any f(x'). (This last fact can be seen from other, more
mathematical, points of view as well. So the surface is notcontained in the volume!)
1.22
Actually, surface delta functions appear using Dirichlet
B.C. as well. Remember
Φ(x) = ∫ d3x' G(x,x') ρ(x') - 1
4π ∫o
s da'Φ(x')∂G
∂n' . (1.87)
Take x≥ on S. Then
Φ|s = - 1
4π ∫o
s da'Φ(x') ∂G
∂n', (1.88)
which means that
- 1
4π ∂G
∂n' |s = δ(s)(x-x'). (1.89)
[This really means
lim
x .s - 1
4π ∂G
∂n' (x,x')|x'on S = δ(s)(x-x').]
We will illustrate the presence of surface delta functions in
some explicit problems later.
I claimed earlier that G N(x',x") is not necessarily
symmetric in it's arguments for interior BC's. Can see thisas follows. First, we will show that, in general, theDirichlet Green function is unique, while the Neumann one isnot. Both cases at once:
∇
2 G1(x',x) = -4 πδ(x-x')
∇2 G2(x',x) = -4 πδ(x-x')either Dirichlet
or Neumann (1.90)
Form
U(x',x) = G 1(x',x) - G 2(x',x), (1.91)
1.23
=>∇2U(x',x) = 0. (1.92)
Then
U(x',x)|s(x) = 0 Dirichlet (1.93)
∂
∂n U(x',x)|s(x) = 0 Neumann (1.94)
As before, look at Green's first identity:
∫v d3x(U(x',x) ∇2 U(x',x) + [ ∇≥U(x',x)]2)
= ∫o
s da U(x',x) ∂
∂n U(x',x), (1.95)
vanishes in either case
=> ∫v d3x(∇≥U(x',x))2 = 0, (1.96)
=> ∇≥U(x',x) = 0 in V. (1.97)
In the Dirichlet case, we proved that G D(x',x") = G D(x",x')
Combined with U |s = 0, we have that
U(x',x) = 0, (1.98)
and GD(x',x") is unique. On the other hand, we have proven
the symmetry G N(x',x") = G N(x",x') only for the exterior
problem (in which case G N(x',x") is unique up to a constant.)
Thus, in general for the interior problem we only have that
∇≥U(x',x) = 0 implies
U(x',x) = F(x'), (1.99)
where F(x') is some function of x'. It is also easy to see
that the most general solution is then
G N(x',x) = G Nsym(x',x) + F(x') (1.100)
1.24
where
GNsym(x',x) = G Nsym(x,x'). (1.101)
It is easy to see that ∇2F(x) = 0 and that G Nsym(x',x) is
unique up to a constant. We can get a physical interpretation
of F(x') from anti-symmetrizing (1.100). We can write
F(x') - F(x") = G N(x',x") - G N(x",x'). (1.102)
We now compare to our earlier (1.73):
<GN(x',x) - G N(x",x)>s(x) = GN(x',x") - G N(x",x').
Averaging over the s(x) surface there gives
F(x') = <GN(x',x)>s(x) + Const. (1.103)
Thus, the arbitrary function F(x') represents the average
potential of the surfaces (which vanishes when the surface at
∞ is included) up to a constant. The fact that this
potential can take an arbitrary value for each source
position is due to the fact that the system is isolated. The
sensible thing to do would be to refer it to a constantoutside potential (via a thin wire, say), which would thenremove the arbitrariness. Thus, we can always
require the
Neumann Green function, in any case, to be symmetric in itsarguments.
1.8 Electrostatic energy
Enough of this! Let's investigate some aspects of
electrostatic energy. Imagine sources in infinite space.Work done on a test charge:
1.25
Wi = qiΦ(x≥
i) (brought in from ∞ ) (1.104)
If Φ is due to point charges, [(n-1) of them ]
Φ(x≥
i) = ∑
j=1n-1 qj
|x≥
i - x≥
j|. (1.105)
Total energy: (now n of them)
W = ∑
i=1n ∑
j<i qiqj
|x≥
i - x≥
j|, (1.106)
or
W = 1
2 ∑
i≠j qiqj
|x≥
i - x≥
j|. (1.107)
Continuous distributions (now has self-energy contributions):
W = 1
2 ∫ ∫ ρ(x≥
) ρ(x≥')
|x≥ - x≥'| d3xd3x'. (1.108)
In contrast to the discrete sum, this expression is in
general finite (because of the d3x, d3x'elements) when self-
energies are included as long as ρ(x'≥
) is not too singular.
Another expression:
W = 1
2 ∫ ρ(x≥
)Φ(x≥
) d3x. (1.109)
But now
ρ(x≥
) = -1
4π ∇2Φ (x≥
), (1.110)
=> W = 1
8π ∫ d3x [∇2Φ]Φ, (1.111)
1.26
= -1
8π ∫ d3x [∇≥.(Φ∇≥
Φ) - ∇≥
Φ .∇≥
Φ], (1.112)
= -1
8π ∫o
s da Φ ∂
∂n Φ + 1
8π ∫ d3x |E≥|2(1.113)
because da ~ R2dΩ, Φ ~ 1
R => ∂
∂n Φ ~ 1
R2
=> W = ∫ d3x w, w = 1
8π |E≥|2. (1.114)
“w” is energy density. What if we try to calculate self-
energy of a stationary point charge:
|E≥|2 = q2
|x≥ - x≥'|4. (1.115)
Then (take x≥' = 0; x ≡ 1
r )
W self = q2 ∫ d3x
r4 = 4πq2 ∫
.0∞
dr
r2 ~ 4π q2∫ 0.∞
dx. (1.116)
Divergence is at small distances, which means high energies.
Called a linear divergence. Actually, divergent in the
quantum theory also, but only logarithmically. This permits
renormalization to take place. (Ask me what this means.)
The equation W i = qiΦ (x≥
i) also allows a physical
interpretation of the fact that we may always choose G(x',x")
= G(x",x') for Green functions. We learned that G(x',x")represents the potential of a (+) unit charge in given BC's.Because of this connection between interaction energy andpotential, we see that the Dirichlet or Neumann Greenfunction can also be considered the
interaction energy of two
positive (or two negative) point charges (at x',x") with
given BC's. Since the two charges are equivalent, the Greenfunction must be symmetric in its arguments. This argumentfails in the case of interior Neumann boundary conditions,
1.27
again because one can imagine defining the zero of potential
for each new source position. This is not possible in theDirichlet case since the potentials are specified by theBC's.
1.9 Capacitance
Let’s talk about capacitance. To emphasize the fact that
the Green function contains all the information to solve anelectrostatic problem in a given geometry, let’s connect thisto the Green function. I learned the following formulas fromSchwinger. Adopting Dirichlet BC's, the potential is
Φ (x
≥) = ∫ d3x GD(x≥
,x≥')ρ(x≥') - 1
4π ∫o
s da'Φ (x≥')∂GD(x≥
,x≥')
∂n'. (1.117)
Let us apply this to a volume, V, bounded by a number of
conducting surfaces. Let's let
ρ(x≥') = 0 (1.118)
in V, and
Φ (x≥')|si .Vi (const.) (1.119)
on the ith surface. Then, using superposition, the potential
in the volume V is
Φ (x≥) = -1
4π ∑
j Vj ∫o
sjdaj'∂GD(x≥
,x≥')
∂n'j. (1.120)
Therefore, the surface charge density, given by the
discontinuity of the normal electric field, is (n^i is an
outward normal to V on the ith conductor, not necessarily to
the conductor volume)
σi (x≥) = 1
4π n^i.∇≥
Φ (x≥) = 1
4π ∂
∂ni Φ, (1.121)
1.28
= − 1
16π2 ∑
j Vj ∫o
sj da'j∂
∂ni ∂
∂n'j GD(x≥
,x≥'). (1.122)
The total charge on the ith surface is therefore
Qi = ∫o
si dai ßi = -1
16π2 ∑
j Vj ∫o
si,sj dai da'j ∂
∂ni ∂
∂n'j GD(x≥
,x≥'). (1.123)
We can write this more simply as
Qi = ∑
j Cij Vj, (1.124)
where the capacitances (C ii) or coefficients of induction
(Cij,i≠j) are given by
Cij = - 1
16π2 ∫o
si,sj dai da'j ∂
∂ni ∂
∂n'j GD(x≥
,x≥'). (1.125)
The capacitance of a conductor is therefore the charge on the
conductor when it is maintained at unit potential, all otherconductors being grounded . A similar statement holds for the
coefficients of capacitance, except the total charge ismeasured on a conductor other than the one being held at unitpotential. The coefficients are symmetric in their indices,
C
ij = Cji. (1.126)
because G D(x≥
,x≥') = G D(x≥',x≥) . Given the energy expression,
W = 1
2 ∫ d3xd3x' ®(x≥) ®(x≥')
|x≥ - x≥'| .1
2 ∫ dada' ß(x≥) ß(x≥')
|x≥ - x≥'|, (1.127)
=> W = 1
2 ∫ da Φ(x≥) ß(x≥), (1.128)
we have, in this case
1.29
W = 1
2 ∑
i Vi ∫o
si dai ßi(x≥) = 1
2 ∑
i ViQi (1.129)
or
W = 1
2 ∑
ij Cij ViVj (gives diff. perspective (1.130)
on the C ii's.)
We have to be careful when the surface at ∞ is included in
our analysis since it's capacitance and coeff.'s of induction
can only be defined in a limiting sense in a given problem.With this understanding then, we can now show that
∑
i Cij = 0, (1.131)
for an interior or “exterior” problem as follows:
∑
i Cij = -1
16π2 ∫o
sj da'j ∂
∂n'j (∑
i ∫o
si dai ∂
∂ni GD(x≥',x≥)). (1.132)
But
1
4π ∑
i ∫o
si dai ∂
∂ni GD(x≥',x≥) = 1
4π ∫ d3x ∇2 GD(x≥',x≥) = -1. (1.133)
Since ∂
∂n'j (const.) = 0, the top line says ∑
i Cij = 0. This
means that
Q ≡ ∑
i Qi = ∑
ij CijVj = 0, (1.134)
as it must since we are imagining a closed system with no
volume charge. (Can you see why this line of reasoning failsin the exterior problem, when the surface at infinity is notincluded?) In addition, only relative values of thepotential have significance here. We can see this from
∑
j Cij(Vj + const.) = ∑
j CijVj. (1.135)
Simple example: parallel conductor geometry
1.30
aVS S2 1
Since the C ij are symmetric in i & j and must sum to zero on
one index, this means
C11 = -C21 = -C12 = C22 ≡ C. (1.136)
Also Q 1 = -Q2 = C(V 1-V2) = C ΔV. (1.137)
The energy is
E = 1
2 ∑
i,j CijViVj = 1
2 C ΔV2. (1.138)
These are the usual expressions for a parallel plate
capacitor. C can be shown from Gauss' law to be,
C ≈ A
4πa. (finite surface, A. Can be directly evaluated; see prob. 2.4.)
(1.139)
Note: Usually it is difficult to get exact solutions for
the Green function for a given geometry, so approximationmethods must be used in computing the C
ij.
1.31
Problems
1.1.1 (a) A vector field is defined by
E≥ = -∇≥Φ,
with
Φ = d≥.r≥
r3 . (d≥ = constant vector)
Derive an expression for E≥.
(b) Prove that E≥ in part (a) can be written as follows:
E≥ = ∇≥×A≥,
with
A≥ = d≥×r≥
r3.
(c) Calculate ∇≥.E≥ and ∇≥×E≥.
[Note: This problem neglects certain subtleties that occur at
r≥= 0. Adapted from DiBartolo's "Classical Theory of
Electromagnetism".]
1.2.1 Given the scale factor definitions,
U-1 ≠ |∂x≥
∂u|, V-1 ≠ |∂x≥
∂v|, W-1 ≠ |∂x≥
∂w|,
and
δ(x≥-x≥') = δ(u-u')δ(v-v')δ(w-w')UVW,
find the form of the delta function for:
1.32
(a) cylindrical coordinates
x= ρ cos φ,
y= ρ sin φ,
where u= ρ, v=φ, w=z;
(b) spherical coordinates
x = r sin θ cos φ,
y = r sin θ sin φ,
z = r cos θ,
where u=r, v=cos θ, w=φ.
1.2.2 Find the form of the Dirac delta function in oblate
spheriodal coordinates. Use
(x) x1 = R√⎯⎯⎯⎯Z2+1sinθ cosφ,
(y) x2 = R√⎯⎯⎯⎯Z2+1sinθ sinφ,
(z) x3 = RZ cos θ.
Take u=Z, v=cos θ, w=φ as the new coordinates. (The θ and φ
corrdinates correspond to the usual polar and azimuthal
angles, respectively, in spherical coordinates.]
1.3.1 (a) Given in two spatial dimensions the form
E≥(x≥) = ∫ da'σ(x≥') x≥-x≥'
|x≥ - x≥'|2,
for the electric field, argue as in the notes that one has
∫o
c d l n^.E≥ = ∑
j in S 2πqj,
for enclosed charge within an surface area S bounded by C, and
∇≥.E≥ = 2πσ(x≥
),
for the electric field due to charge density σ(x≥
).
1.33
(b) For a positive point charge in two dimensions, show that
(a) gives
∇2 ln|x≥-x≥'|
K = 2πδ (2)(x≥-x≥'),
where K is an arbitrary positive constant.
(c) Confirm this delta function representation by puttingx≥'=0 and integrating both sides of (b) about an arbitrary
area surrounding the origin. [Note: This identifies the
potenial of a point charge in 2 dimensions as - ln|x≥-x≥'|
K
.
However, the potential of a line charge in 3 dimensions with
unit line density of charge is - 2 ln|x≥-x≥'|
K. Do you know where
the extra 2 comes from?]
1.3.2 (a) Find the potential everywhere for a straight
uniform line charge density, λ, which makes a X-figure at the
origin in the xy plane extending from L to -L on both axes
(no conductors present):
y
xλλ
L -L
-LL
Get the exact Φ(x,y,z), then show for L >> |x|,|y|,|z| that
Φ(x,y,z) ~~ - λ ln ⎝⎜⎛
⎠⎟⎞ (x2+z2)(y2+z2)
16L4.
1.34
Why is this answer obvious? For the opposite extreme, L <<
|x|,|y|,|z| show that you get the expected answer for aneffective point charge.(b)
y
xλλ
-L
L
The straight uniform line charges in the xy plane are now
given by one line charge, λ, situated along the y-axis from
the origin to L, and another, - λ, situated along the x-axis.
Again, get the exact expression, then show for L >>
|x|,|y|,|z| that
Φ(x,y,z) ~~ - λ ln ⎝⎜⎛
⎠⎟⎞r-y
r-x,
where r = √⎯⎯⎯⎯⎯⎯⎯x2+y2+z2.
1.4.1 (a) For a potential of the form ( δ<<1)
φ = q
(1+δ)r121+δ ,
where r 12 is the distance between source and field points,
show that the potential difference between two concentricspheres with uniform surface charge (radii a and b with b<a)is given by
φ(r) = φ
in(r) + φout(r)
where
1.35
φin(r) = qa
1-δ2 1
2ar [(a+r)1-δ -(a-r)1-δ] ,
φ out(r) = qb
1-δ2 1
2br [(r+b)1-δ − (r-b)1-δ].
(b) After the spheres are connected by a wire, show that the
charge on the inner sphere is given by
qb ≈ qaδ
2(b-a) [a ln ⎝⎜⎛
⎠⎟⎞a-b
a+b + b ln ⎝⎜⎛
⎠⎟⎞4a2
a2-b2].
1.5.1 In deriving Eq.(1.42) of the text, consider two close
surfaces, 1 and 2, with associated surface charge densities
σ1(x≥') and σ(x≥"), respectively; see the figure on p. 1.12. The
separation between the surfaces is such that the points at
which the charge densities are equal and opposite areseparated a uniform distance, d, along the common
perpendicular; ie, σ
1(x≥'-n^21d) = - σ(x≥'). We may characterize
the potential in the limit of close separation of the two
surfaces as,
Φ(x≥) = ∫
S2
σ(x≥')
|x≥-x≥'| da' - ∫
S1
σ1(x≥")
|x≥-x≥"| da".
With the connection
x≥" = x≥' - n^21d,
and the expansion, to lowest order in a≥,
1
|x≥-a≥| = 1
|x≥| + a≥.∇≥
⎝⎜⎜⎛
⎠⎟⎟⎞ 1
|x≥|,
one may derive Eq.(1.42) of the text.
Now consider the similar situation:
1.36
21n21^
σ≥(x')σ-≥d
+xsurface 2
surface 1(x'+dx)^
Two regions in free space (3 dimensions) are separated by a
type of dipole surface. The dipole surface is constucted byplacing equal and opposite surface charge densities oncomplementary surfaces which are then brought together suchthat a small constant separation, d, measured along one axis,remains (these are open surfaces).
(a) Show that the potential can be written as
Φ
d(x≥) = dx^.E≥2(x≥),
where x^ is a unit vector in the separation direction and E≥2 is
the electric field due to surface 2.
(b) Show that the discontinuity of the potential in the normal
direction (to surface 2) across the surfaces is given by
Φd2 − Φd1 = 4π D(x≥) x^.n^21,
where D(x≥) ≡ σ(x≥)d.
1.5.2 (a) A hemisphere of radius "a" has a constant dipole
surface density, D. D is defined relative to the unit vector,n^, pointing "out" as shown. Using the coordinates shown with
the origin O at the hemisphere's enter, find the E≥ field
everywhere along the z-axis (- ∞ <_ z <_ ∞), Then, using
spherical coordinates, find the electric field components, E
r
and E θ, far from the region of the sphere, r>>R.
1.37
+z On^
constant D
(b) A sphere of radius "a" is given a constant dipole surface
charge density, D. D is defined relative to the sphere's outernormal, n ^.
n^
D=constant
Find the electric field both inside and outside the sphere.
1.5.3 A thin isolated metallic disk of radius R is charged
until it has aquired a potential V.
R
V
The solution for the electrostatic potential is found most
easily in oblate spheroidal coordinates, Ζ and ξ, given by
1.38
z = R Ζ ξ,
ρ = R[(1+ Ζ2)(1-ξ2)]1/2,
(ρ2 = x2 + y2 where x, y and z are the usual Cartesian
coordinates) and is given by
Φ = A tan-1
⎝⎜⎛
⎠⎟⎞1
Ζ,
where A is an unknown constant. (The third coordinate is the
usual azimuthal angle φ; take your the origin of coordinates
at the center of the disk and the z azis | _ to the plane of
the disk.)(a) Change variables to show that the potential may be
written as (r
2 = ρ2 + z2)
Φ = A tan-1
⎝⎜⎜⎜⎛
⎠⎟⎟⎟⎞ √⎯2R √⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯(r2 - R2)+√⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯⎯(r2 - R2)2 + 4R2z2
(b) By considering the limit z § 0 when r < R, argue from
consistency that
A = 2V
π.
(c) Show that the surface charge density on the disk, σ(ρ),
is given by
σ(ρ) = V
π2 1
√⎯⎯⎯⎯⎯⎯R2 - ρ2.
[Note: d
dxtan-1 y = 1
1+y2 dy
dx.]
1.6.1 (a) Prove Green's reciprocation theorem: For two
problems with the exact same geometry including conductingsurfaces, one has
1.39
∫ da σ Φ' + ∫ d3x ρ Φ' = ∫ da σ 'Φ + ∫ d3x ρ 'Φ,
where Φ, ρ and σ are the potential, volume charge density and
surface charge density of problem 1, while Φ', ρ' and σ' are
similar quantities for problem 2.
(b) A point charge, q, is located somewhere between twogrounded concentric spherical conducting shells (a < r < b) asshown.
a
br
q0V0V
Find the charge induced on the inner or outer conducting
shells by use of the theorem of (a).
1.7.1 Given a certain geometry, show that the Neumann and
Dirichlet Green functions are related by
GN(x≥",x≥) = GD(x≥,x≥") - 1
4π ∫o
Sda' GN(x≥",x≥')∂GD(x≥,x≥')
∂n'.
1.7.2 Show that a solution to the Poisson equation with both
Φ and ∂Φ
∂n specified arbitrarily on a closed boundary (Cauchy
boundary conditions) does not exist. [Hint: Show that if one
is known, the other is determined .]
1.7.3 The Neumann Green's function in 3 dimensions satisfies
∇2GN(x≥',x≥) = -4πδ(x≥ - x≥').
1.40
Assume that the normal derivative is
∂GN(x≥',x≥)
∂n|x≥on S = - 4π
S
where S is the total surface area. We saw that according to
(1.100),
G N(x≥',x≥) = Gsym(x≥',x≥) + F(x≥').
Considering the interior problem, show that F(x≥') gives no
contribution to the potential, Φ(x≥). When considering the
normal derivative, ∂Φ
∂n|s, show that the general form for
GN(x≥',x≥) above and Eq.(1.78) remove the "indescretion" in
Eq.(1.81).
1.8.1 Prove a simplified Thompson's theorem for a single
closed surface: If a surface is fixed in position and a giventotal charge is placed on it, then the electrostatic energy inthe region bounded by the surface and infinity is an absoluteminimum when the charges are placed so that the surface is anequipotential.
1.8.2 Prove the following theorem: If a number of conducting
surfaces are fixed in position with a given total charge oneach, the introduction of an uncharged, insulated conductorinto the region bounded by the surfaces lowers theelectrostatic energy.
1.8.3 Investigate the self-energy of a one-dimensional
straight
string of charge with linear charge density λ = Q
a and
length a. Is this quantity divergent, and if so, is it
guadratically, linearly or logarithmically divergent?
1.41
1.8.4 Consider an infinitely thin circular disk of radius R
with constant surface charge density σ. (This is not a
conductor!) Give an argument that the self-energy is finite.
[Hint: The origins of the primed and unprimed coordinatesystems do not have to coincide. I used cylindricalcoordinates and got an upper limit.]
1.9.1 Two conductors, A and B, form an isolated system. Show,
based upon the positivity of the field energy W, that thecoefficient of capacitance, C
AB = CBA, and the two
capacitances, C AA and C BB, obey the inequality,
CAB2 < CAACBB.
1.9.2 (a) Use Green's reciprocity theorem (above) to prove
Cij = Cji.
(b) Show the same result from (1.125) of the script.
(c) Show C ii > 0 from first principles.
1.9.3 Using Q i = ∑
jCijVj and the definition of the C ij,
find the six independent coefficients of capacitance for three
co-centered spherical conducting shells having radii a,b and c(a<b<c). [ Call these C
aa, Cbb, Ccc, Cab, Cac and Cbc.]
1.9.4 Given a system of two
conductors of arbitraryshape, with conductor Bbeing hollow and containingan interior conductor A,show that the capitancessatisfy
AB
1.42
CBB ≥ CAA.
1.9.5 Consider two arbitrary, closed conductors, labelled "a"
and "b" in free space, with total charge Q and -Q present.Define,
C ≠ Q
V
a - Vb,
where V a and V b are the potentials of conductors A and B. Show
that
C = det()Caa Cab
Cab Cbb
∑
i,jCij.
1.9.6 Consider an isolated conductor, a, with capacitance Ca1.
Show that the introduction of a second conductor, b, raises
the capacitance of the first conductor: Ca2 > Ca1.