Unit - 4
Electrostatics
LAPLACE’S AND POISSON’S EQUATIONS FOR ELECTROSTATIC POTENTIAL
A useful approach to the calculation of electric potentials is to relate that potential to the charge density which gives rise to it. The electric field is related to the charge density by the divergence relationship
=
E = Electric field
= Charge density
= Permittivity
And the electric field is related to the electric potential by a gradient relationship
E =
Therefore the potential is related to the charge density by Poisson's equation
= 2V =
In a charge-free region of space, this becomes Laplace's equation
2V = 0
This mathematical operation, the divergence of the gradient of a function, is called the Laplacian. Expressing the Laplacian in different coordinate systems to take advantage of the symmetry of a charge distribution helps in the solution for the electric potential V.
For example, if the charge distribution has spherical symmetry, you use the Laplacian in spherical polar coordinates.
Since the potential is a scalar function, this approach has advantages over trying to calculate the electric field directly. Once the potential has been calculated, the electric field can be computed by taking the gradient of the potential.
LAPLACE'S EQUATION IN ONE DIMENSION
In one dimension the electrostatic potential V depends on only one variable x. The electrostatic potential V(x) is a solution of the one-dimensional Laplace equation
=0
The general solution of this equation is
V(x) = sx + b
Where s and b are arbitrary constants. These constants are fixed when the value of the potential is specified at two different positions.
Example
Consider a one-dimensional world with two point conductors located at x = 0 m and at x = 10 m. The conductor at x = 0 m is grounded (V = 0 V) and the conductor at x = 10 m is kept at a constant potential of 200 V. Determine V.
The boundary conditions for V are
V(0) = b = 0V
And
V(10) = 10s +b =200V
The first boundary condition shows that b = 0 V. The second boundary condition shows that s = 20 V/m. The electrostatic potential for this system of conductors is thus
V(x) = 20x
The corresponding electric field can be obtained from the gradient of V
E(x) = = -20 V/m
The boundary conditions used here, can be used to specify the electrostatic potential between x = 0 m and x = 10 m but not in the region x < 0 m and x > 10 m.
If the solution obtained here was the general solution for all x, then V would approach infinity when x approaches infinity and V would approach minus infinity when x approaches minus infinity. The boundary conditions therefore provide the information necessary to uniquely define a solution to Laplace's equation, but they also define the boundary of the region where this solution is valid (in this example 0 m < x < 10 m).
The following properties are true for any solution of the one-dimensional Laplace equation:
Property 1:
V(x) is the average of V(x + R) and V(x - R) for any R as long as x + R and x - R are located in the region between the boundary points. This property is easy to proof:
This property immediately suggests a powerful analytical method to determine the solution of Laplace's equation. If the boundary values of V are
V(x=a) =Va
And
V(x=b) =Vb
Then property 1 can be used to determine the value of the potential at (a + b)/2:
Next we can determine the value of the potential at x = (3 a + b)/4 and at
x = (a + 3 b)/4:
This process can be repeated and V can be calculated in this manner at any point between x = a and x = b (but not in the region x > b and x < a).
Property 2:
The solution of Laplace's equation cannot have local maxima or minima. Extreme values must occur at the end points (the boundaries). This is a direct consequence of property 1.
Property 2 has an important consequence: a charged particle cannot be held in stable equilibrium by electrostatic forces alone (Earnshaw's Theorem). A particle is in a stable equilibrium if it is located at a position where the potential has a minimum value.
A small displacement away from the equilibrium position will increase the electrostatic potential of the particle, and a restoring force will try to move the particle back to its equilibrium position.
There can be no local maxima or minima in the electrostatic potential.
The particle cannot be held in stable equilibrium by just electrostatic forces.
LAPLACE'S EQUATION IN TWO DIMENSIONS
In two dimensions the electrostatic potential depends on two variables x and y. Laplace's equation now becomes
+ =0
This equation does not have a simple analytical solution as the one-dimensional Laplace equation does. However, the properties of solutions of the one-dimensional Laplace equation are also valid for solutions of the two-dimensional Laplace equation:
Property 1:
The value of V at a point (x, y) is equal to the average value of V around this point
Where the path integral is along a circle of arbitrary radius, centered at (x, y) and with radius R.
Property 2:
V has no local maxima or minima; all extremes occur at the boundaries.
LAPLACE'S EQUATION IN THREE DIMENSIONS
In three dimensions the electrostatic potential depends on three variables x, y, and z. Laplace's equation now becomes
+ =0
This equation does not have a simple analytical solution as the one-dimensional Laplace equation does. However, the properties of solutions of the one-dimensional Laplace equation are also valid for solutions of the three-dimensional Laplace equation:
Property 1:
The value of V at a point (x, y, z) is equal to the average value of V around this point
Where the surface integral is across the surface of a sphere of arbitrary radius, centered at (x,y,z) and with radius R.
Figure 1
Proof of property 1
To proof this property of V consider the electrostatic potential generated by a point charge q located on the z axis, a distance r away from the center of a sphere of radius R (see Figure 3.1). The potential at P, generated by charge q, is equal to
Vp=
Where d is the distance between P and q. Using the cosine rule we can express d in terms of r, R and θ
= + -2Rrcosθ
The potential at P due to charge q is therefore equal to
Vp=
The average potential on the surface of the sphere can be obtained by integrating Vp across the surface of the sphere. The average potential is equal to
Which is equal to the potential due to q at the center of the sphere. Applying the principle of superposition it is easy to show that the average potential generated by a collection of point charges is equal to the net potential they produce at the center of the sphere.
Property 2:
The electrostatic potential V has no local maxima or minima; all extremes occur at the boundaries.
Example:
Find the general solution to Laplace's equation in spherical coordinates, for the case where V depends only on r. Then do the same for cylindrical coordinates.
Laplace's equation in spherical coordinates is given by
If V is only a function of r then
=0
And
=0
Therefore, Laplace's equation can be rewritten as
The solution V of this second-order differential equation must satisfy the following first-order differential equation:
This differential equation can be rewritten as
=
The general solution of this first-order differential equation is
V(r) = +b
Where b is a constant. If V = 0 at infinity then b must be equal to zero, and consequently
V(r)=
Laplace's equation in cylindrical coordinates is
If V is only a function of r then
=0
And
=0
Therefore, Laplace's equation can be rewritten as
The solution V of this second-order differential equation must satisfy the following first-order differential equation:
r= a = constant
This differential equation can be rewritten as
=
The general solution of this first-order differential equation is
V(r) = aln(r) +b
Where b is a constant. The constants a and b are determined by the boundary conditions.
Consider a volume (see Figure 3.2) within which the charge density is equal to zero. Suppose that the value of the electrostatic potential is specified at every point on the surface of this volume. The first uniqueness theorem states that in this case the solution of Laplace's equation is uniquely defined.
Figure 2 First Uniqueness Theorem
To proof the first uniqueness theorem we will consider what happens when there are two solutions V1 and V2 of Laplace's equation in the volume shown in Figure. Since V1 and V2 are solutions of Laplace's equation we know that
=0
=0
Since both V1 and V2 are solutions, they must have the same value on the boundary. Thus V1 = V2 on the boundary of the volume. Now consider a third function V3, which is the difference between V1 and V2
=-
The function V3 is also a solution of Laplace's equation. This can be demonstrated easily:
=- =0
The value of the function V3 is equal to zero on the boundary of the volume since V1 = V2 there. However, property 2 of any solution of Laplace's equation states that it can have no local maxima or minima and that the extreme values of the solution must occur at the boundaries. Since V3 is a solution of Laplace's equation and its value is zero everywhere on the boundary of the volume, the maximum and minimum value of V3 must be equal to zero. Therefore, V3 must be equal to zero everywhere. This immediately implies that
V1 = V2
This proves that there can be no two different functions V1 and V2 that are solutions of Laplace's equation and satisfy the same boundary conditions. Therefore, the solution of Laplace's equation is uniquely determined if its value is a specified function on all boundaries of the region. This also indicates that it does not matter how you come by your solution: if (a) it is a solution of Laplace's equation, and (b) it has the correct value on the boundaries, then it is the right and only solution.
Figure 3
The first uniqueness theorem can only be applied in those regions that are free of charge and surrounded by a boundary with a known potential (not necessarily constant). In the laboratory the boundaries are usually conductors connected to batteries to keep them at a fixed potential.
In many other electrostatic problems we do not know the potential at the boundaries of the system. Instead we might know the total charge on the various conductors that make up the system (note: knowing the total charge on a conductor does not imply a knowledge of the charge distribution ρ since it is influenced by the presence of the other conductors).
In addition to the conductors that make up the system, there might be a charge distribution ρ filling the regions between the conductors. For this type of system the first uniqueness theorem does not apply.
The second uniqueness theorem states that the electric field is uniquely determined if the total charge on each conductor is given and the charge distribution in the regions between the conductors is known.
The proof of the second uniqueness theorem is similar to the proof of the first uniqueness theorem.
Suppose that there are two fields and that are solutions of Poisson's equation in the region between the conductors. Thus
.=
.=
Where ρ is the charge density at the point where the electric field is evaluated. The surface integrals of and , evaluated using a surface that is just outside one of the conductors with charge Qi, are equal to . Thus
=
=
The difference betweenand , So
= -
Satisfies the following equations:
.= . - . - =0
= - = - =0
Consider the surface integral of , integrated over all surfaces (the surface of all conductors and the outer surface). Since the potential on the surface of any conductor is constant, the electrostatic potential associated with and , must also be constant on the surface of each conductor.
Therefore, =- will also be constant on the surface of each conductor.
The surface integral of over the surface of conductor i can be written as
= =0
Since the surface integral of over the surface of conductor i is equal to zero,
The surface integral of over all conductor surfaces will also be equal to zero. The surface integral of over the outer surface will also be equal to zero since on this surface. Thus
=0
The surface integral of can be rewritten using Green's identity as
0 = = - =
= - = - =0
Where the volume integration is over all space between the conductors and the outer surface. Since is always positive, the volume integral of can only be equal to zero if everywhere. This implies immediately that , everywhere, and proves the second uniqueness theorem.
Electric polarization refers to the separation of center of positive charge and the center of negative charge in a material. The separation can be caused by a sufficiently high-electric field.
It occurs when a non-polar substance is placed between two parallel plates with an applied electric field. The electric field tends to attract the negatively charged electron particles or clouds towards the positive plate and the positive charge nucleus towards the negative plate. Therefore, in the presence of an electric field or current, there will be observed an electrical distortion or polarized molecule to form an electrical dipole. In learning chemistry or physics, such type of distortion process in the molecules is called the electric polarization but the polarization disappears as soon as the polarized field is withdrawn and the polarizing molecule comes back to its original state.
The permittivity εo of free space is 8.854×10-12 farads/meter, where
=εo .
The permittivity ε of any material deviates from εo for free space if applied electric fields induce electric dipoles in the medium; such dipoles alter the applied electric field seen by neighbouring atoms.
Electric fields generally distort atoms because pulls on positively charged nuclei (f=q [N]) and repels the surrounding negatively charged electron clouds. The resulting small offset d of each atomic nucleus of charge +q relative to the center of its associated electron cloud produces a tiny electric dipole in each atom, as suggested in Figure: 10(a).
In addition, most asymmetric molecules are permanently polarized, such as H2O or NH3, and can rotate within fluids or gases to align with an applied field. Whether the dipole moments are induced, or permanent and free to rotate, the result is a complete or partial alignment of dipole moments as suggested in Figure: 10(b).
These polarization charges generally cancel inside the medium, as suggested in Figure: 10(b), but the immobile atomic dipoles on the outside surfaces of the medium are not fully cancelled and therefore contribute the surface polarization charge ρsp
Figure 4: Polarized media
Figure:4(c) suggests how two charged plates might provide an electric field that polarizes a dielectric slab having permittivity ε > εo. The electric field is the same in vacuum as it is inside the dielectric (assuming no air gaps) because the path integral of from plate to plate equals their voltage difference V in both cases. The electric displacement vector e =ε and therefore differs.] We associate the difference between o =εo (vacuum) and ε=ε (dielectric) with the electric polarization vector P, where:
= ε =εo + = εo (1+) (8)
The polarization vector is defined by (8) and is normally parallel to in the same direction, as shown in Figure: 4(c); it points from the negative surface polarization charge to the positive surface polarization charge (unlike , which points from positive charges to negative ones).
As suggested in (8), = εo ,
Where χ is defined as the dimensionless susceptibility of the dielectric. Because nuclei are bound rather tightly to their electron clouds, χ is generally less than 3 for most atoms, although some molecules and crystals, particularly in fluid form, can exhibit much higher values.
Electric displacement, also known as dielectric displacement and usually denoted by D, is a vector field in a non-conducting medium, a dielectric.
In a dielectric material, the presence of an electric field E causes the bound positive and negative charges in the material to slightly separate, inducing a local electric dipole moment. The electric displacement field "D" is defined as
D= 𝜺0E+P
E = External electric field in which the dielectric is placed
𝜺0 = the permittivity of the free space
P = Polarization Density
In S.I. System, Unit of Electric displacement is C/m2.
D = 𝜺0E+P
D= 𝜺E and P = XeE
Key Takeaways
- The permittivity εo of free space is 8.854×10-12 farads/meter
- The electric displacement vector e =ε and therefore differs.] We associate the difference between o =εo (vacuum) and ε=ε (dielectric) with the electric polarization vector P , where: = ε =εo + = εo (1+)
- The electric displacement field "D" is defined as D= 𝜺0E+P
Besides the bound charges due to polarization, a dielectric material may also contain some extra charges which just happen to be there. For a lack of a better term, such extra charges are called free charges, just to contrast them from the bound charged due to polarization. Anyway, the net macroscopic electric field does not care for the origin of the electric charges or how we call them but only
net(r) =free(r) + bound(r); net(r) = free(r) + bound(r); ………(1)
In particular, the Gauss Law in differential form says
0.E(r) = net(r) + net (coordinate ⟂ surface) + more function terms due to linear and point charges ………(2)
For simplicity, let's ignore for a moment the surface, line, and point charges and focus on just the volume charge density. This gives us
0.E(r) = net(r) = free(r) + bound(r) = free(r) −∇ ·P
Which we may rewrite as
∇.(ε0E+P) = free ………(3)
In light of this formula, the combination
D(r) =ε0E(r) +P(r) ………(4)
Called the electric displacement field obeys the Gauss Law involving only the free charges but not the bound charges,
∇.D(r) = free
Boundary Conditions
Outside the dielectric there is no polarization, so we simply set
D(r) =ε0E(r) ……(1)
Consequently, at the dielectric’s boundary, the D field has two sources of discontinuity:
(1) The abrupt disappearance of the P term, and
(2) Discontinuity of the E field due to the net surface charge density.
If we focus on the component of the D vector ⊥ to the boundary, we get
Disc (D⊥) =−Pinside⊥+ ε0disc(E⊥) =−P·n + σnet=−σbound + σnet=σfree ……(2)
Again, only the free surface charge affects this discontinuity, the bound surface charge cancels out between the P and the ε0E terms. In terms of the D field's divergence, the discontinuity of ∇.(ε0E+P) = free becomes
()singular = disc (D⊥)(coordinate ⟂ surface) = σfree(coordinate ⟂ surface) ……(3)
Similar -function terms would obtain at free surface charges stuck inside the dielectric or outside it, and if we also allow for line or point free charges, there would also be (2) and (3)on the RHS. Altogether, for a most general geometry of free charges the complete Gauss Law for the D field becomes
∇.D(r) = free(r) + σfree(coordinate ⟂ surface) + more -function terms due to free linear and point charges,
But only the free charges appear on the RHS here. All contributions of the bound charges cancel against the ∇.P term hiding inside the ∇.E on the LHS. Therefore, the integral form of the Gauss Law for the D field is
=Qfree [surrounded by S] ……(4)
Where the RHS includes all possible configurations of free charges surrounded by the surface S, but only the free charges. By the way, the surface S in this formula can be any complete surface | it can lie completely inside the dielectric, or completely outside it, or even cross the dielectric's surface | but the Gauss Law will work in any case, as long as we properly account for the net free charge enclosed within S.
For highly symmetric cases, we may calculate the D field just from the Gauss Law; more general geometries do not allow such shortcuts.
In fact, in general D(r) (anything) as in case of E(r) = (r) ……(5)
Indeed, while the electrostatic tension field (Electric Field) always obeys ∇E = 0, for the displacement field we have
∇D = ε0∇ E + ∇P which does not need to vanish ……(6)
This issue becomes particularly acute at the dielectric's boundary. We know that despite the surface charge density of the bound charges, the potential and the tangential components of the electric tension field must be continuous across the boundary.
V(just outside) =V(just inside) ……(7)
E∥(just outside) =E∥(just inside) ……(8)
On the other hand, the polarization field P abruptly drops to zero at the boundary, so if P just inside the dielectric is directed at some general angle to the surface, then both its tangential and normal components suffer discontinuities.
P∥(just inside) P∥(outside) = 0 ……(9)
P⟂ (just inside) P⟂(outside) = 0 ……(10)
Figure 5
Combining equations (9) and (10), we find that in general the tangential components of the displacement field are discontinuous across the dielectric's boundary,
D∥(just outside) D∥(just inside) ……(11)
As to the normal components of the tension and the displacement fields, the E⟂ is generally discontinuous across the boundary due to surface bound charges, but as we saw in eq. (2),
In the absence of free charges
D⟂ (just outside) =D⟂ (just inside) ……….(12)
In the middle of a dielectric or outside it:
∇.D=free ……….(13)
∇E= 0 ………(14)
On the other hand,
∇.E= (1/ε0)net which is often unknown ………(15)
∇D= unknown ………(16)
At the outer boundary of a dielectric, or at the boundary between two different dielectrics
- V, E∥, and D⟂ are continuous
- E⟂ and D∥ are discontinuous
To complete this equation system, we need a relation between the E and the D fields at the same point r, and that relation depends very much on the dielectric material in question. For some material, such relation can be rather complicated, or even history-dependent. Fortunately, for most common dielectrics the relation between the E and the D fields is linear (unless the fields become too strong). So in this class, we shall hence forth focus on such linear dielectrics.
At far distances from the sphere, the field is uniform and is equal to
= ……….(1)
Which corresponds to a potential of
out = ……….(2)
As before we can expand the potential inside and outside in terms of Legendre polynomials. Since the distant potential only has Legendre polynomial of order 1, we need to include only up to this order. Outside the sphere, the field is given by the potential.
……….(3)
Inside the sphere, the origin is included. Thus, inside the sphere, the potential cannot have a singularity at the origin and is given by
……….(4)
Comparing with the asymptotic limit at long distances, A1 =
The potential itself is continuous at r=R
……….(5)
Since there are no free charges on the surface, the normal component of the displacement vector is continuous across the surface. The normal component being the radial direction, we have,
……….(6)
Solving, we get,
……….(7)
……….(8)
So that
……….(9)
And the electric field inside the dielectric is
……….(10)
It is seen that the due to the presence of dielectric the electric field inside is reduced by
……….(11)
We observe that if a dipole is kept at the origin of a sphere of radius R, since the radius of the sphere can be considered very large compared with the dimensions of the dipole, the field is given by
……….(12)
Thus the effect of dielectric is the same as that of replacing the dielectric with a dipole of moment
……….(13)
The polarization of the sphere is then obtained by dividing this by the volume of the sphere, i.e., /3 by
……….(14)
Thus the field due to the dielectric can be written as
……….(15)
Note that the polarization in the medium is uniform and is directed along the direction of the external field. The field lines approach the sphere from the left (negative z direction) and leave from the right, making the left face of the sphere negatively charged.
Figure 6
Reduction in the electric field due to the presence of a dielectric
Consider a point charge in an isotropic dielectric with permittivity . Taking the position of the charge at the origin, the field must be radial. The displacement field can be found from the Gauss’s law,
……….(16)
So that
……….(17)
Since the dielectric is uniform,
……….(18)
Thus in the presence of a dielectric the electric field is reduced by a factor =k. The dielectric constant is a measure of the factor by which the electric field gets reduced in a linear dielectric medium. The polarization vector is given by
……….(19)
Consider a Gaussian sphere of radius r. We can calculate the volume charge density inside the volume by the negative divergence of the polarization vector
……….(20)
However, there is a bound surface charge density. Since the dielectric is inside the sphere, the surface direction is inward =.
……….(21)
Thus there exists a net negative bound charge. The total charge is obtained by multiplying the above with the surface area, which gives qb=
As the total charge bound to the surface. The effective charge seen by a test charge is the sum of the original charge as reduced by this amount, i.e
……….(22)
.i.e., the test charge experiences the electric field due to an effective charge screened by a factor equal to the dielectric constant of the medium.
References:
1. Fundamentals of Physics Electricity and Magnetism, Halliday and Resnick, tenth edition (published 2013).
2. Electricity, magnetism and light, W. Saslow, 1st edition
3. Electromagnetic Theory, Singh and Prasad, I. K. International Publication, 1/e
4. Electricity, Magnetism & Electromagnetic Theory, S. Mahajan and Choudhury, 2012, Tata McGraw
5. Elements of Electromagnetics, M.N.O. Sadiku, 2010, Oxford University Press.