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Electrostatics | Physics - Wyatt's Notes

2.1 Coulomb’s Law and the Electric Field

Coulomb’s Law: The force between two point charges q1q_1 and q2q_2 separated by distance rr:

F=14πε0q1q2r2r^\mathbf{F} = \frac{1}{4\pi\varepsilon_0} \frac{q_1 q_2}{r^2} \hat{\mathbf{r}}

The electric field due to a point charge qq at position r\mathbf{r}:

E(r)=14πε0qr2r^\mathbf{E}(\mathbf{r}) = \frac{1}{4\pi\varepsilon_0} \frac{q}{|\mathbf{r}|^2} \hat{\mathbf{r}}

Superposition Principle: The field due to a collection of charges is the vector sum of individual Fields.

2.2 Gauss’s Law Applications

Example: Infinite plane of charge with surface charge density σ\sigma.

Choose a Gaussian “pillbox” of area AA straddling the plane. By symmetry, E\mathbf{E} is Perpendicular to the plane. Gauss’s law:

2EA=σAε0    E=σ2ε02EA = \frac{\sigma A}{\varepsilon_0} \implies E = \frac{\sigma}{2\varepsilon_0}

The field is uniform and perpendicular to the plane, pointing away from positive charge.

Example: Uniformly charged sphere of radius RR with total charge QQ.

For r>Rr \gt R: E=Q4πε0r2r^\mathbf{E} = \frac{Q}{4\pi\varepsilon_0 r^2} \hat{\mathbf{r}} (identical to a point charge).

For r<Rr \lt R: E=Qr4πε0R3E = \frac{Qr}{4\pi\varepsilon_0 R^3} (linear in rr).

2.3 Electric Potential

The electric potential is defined by E=V\mathbf{E} = -\nabla V (for electrostatics, where ×E=0\nabla \times \mathbf{E} = \mathbf{0}).

For a point charge: V(r)=14πε0qrV(\mathbf{r}) = \frac{1}{4\pi\varepsilon_0} \frac{q}{r} (choosing V()=0V(\infty) = 0).

Theorem 2.1. ×E=0\nabla \times \mathbf{E} = \mathbf{0} in electrostatics implies E\mathbf{E} is Conservative, so the line integral ABEdl=V(A)V(B)\int_A^B \mathbf{E} \cdot d\mathbf{l} = V(A) - V(B) is Path-independent.

2.4 Poisson’s and Laplace’s Equations

Substituting E=V\mathbf{E} = -\nabla V into Gauss’s law:

(V)=2V=ρε0\nabla \cdot (-\nabla V) = -\nabla^2 V = \frac{\rho}{\varepsilon_0}

This is Poisson’s equation:

2V=ρε0\nabla^2 V = -\frac{\rho}{\varepsilon_0}

In regions with ρ=0\rho = 0This reduces to Laplace’s equation:

2V=0\nabla^2 V = 0

Theorem 2.2 (Uniqueness --- statement). The solution to Laplace’s (or Poisson’s) equation in a Region is unique given either Dirichlet boundary conditions (VV specified on the boundary) or Neumann boundary conditions (V/n\partial V / \partial n specified on the boundary).

2.5 Worked Example

Problem. Two infinite conducting plates at x=0x = 0 and x=dx = d are held at potentials V=0V = 0 and V=V0V = V_0 respectively. Find the potential and field between them.

Solution. Between the plates, ρ=0\rho = 0 So 2V=0\nabla^2 V = 0. By symmetry, VV depends only on xx:

d2Vdx2=0    V(x)=Ax+B\frac{d^2V}{dx^2} = 0 \implies V(x) = Ax + B

Boundary conditions: V(0)=0    B=0V(0) = 0 \implies B = 0. V(d)=V0    A=V0/dV(d) = V_0 \implies A = V_0/d.

V(x)=V0dx,E=dVdxx^=V0dx^V(x) = \frac{V_0}{d} x, \quad \mathbf{E} = -\frac{dV}{dx}\hat{\mathbf{x}} = -\frac{V_0}{d}\hat{\mathbf{x}}

\blacksquare

2.6 Gauss’s Law: Cylindrical Symmetry

Example: Infinite line charge with linear charge density λ\lambda.

By cylindrical symmetry, E\mathbf{E} points radially outward and depends only on rr. Choose a Gaussian cylinder of radius rr and length LL:

EdA=E2πrL=λLε0\oint \mathbf{E} \cdot d\mathbf{A} = E \cdot 2\pi r L = \frac{\lambda L}{\varepsilon_0}

E=λ2πε0rr^\mathbf{E} = \frac{\lambda}{2\pi\varepsilon_0 r}\,\hat{\mathbf{r}}

Example: Coaxial cable. An inner conductor of radius aa carries linear charge density +λ+\lambda And an outer conducting shell of radius bb carries λ-\lambda.

For r<ar \lt a: E=0\mathbf{E} = \mathbf{0} (conductor interior).

For a<r<ba \lt r \lt b: E=λ2πε0rr^\mathbf{E} = \frac{\lambda}{2\pi\varepsilon_0 r}\,\hat{\mathbf{r}}.

For r>br \gt b: E=0\mathbf{E} = \mathbf{0} (total enclosed charge is zero).

The potential difference between the conductors:

V(a)V(b)=abEdl=λ2πε0ln ⁣(ba)V(a) - V(b) = -\int_a^b \mathbf{E} \cdot d\mathbf{l} = \frac{\lambda}{2\pi\varepsilon_0}\ln\!\left(\frac{b}{a}\right)

2.7 The Uniqueness Theorem

Theorem 2.3 (Uniqueness for Dirichlet conditions). The solution to Poisson’s equation 2V=ρ/ε0\nabla^2 V = -\rho/\varepsilon_0 in a volume V\mathcal{V} is unique if VV is specified on the Boundary S\mathcal{S}.

Proof. Suppose V1V_1 and V2V_2 both satisfy Poisson’s equation with the same boundary Conditions. Define U=V1V2U = V_1 - V_2. Then 2U=0\nabla^2 U = 0 in V\mathcal{V} and U=0U = 0 on S\mathcal{S}.

Apply Green’s first identity with ϕ=ψ=U\phi = \psi = U:

V(U2U+U2)dV=SUUndA\int_{\mathcal{V}} \left(U\,\nabla^2 U + \lvert\nabla U\rvert^2\right) dV = \oint_{\mathcal{S}} U\,\frac{\partial U}{\partial n}\, dA

Since 2U=0\nabla^2 U = 0 and U=0U = 0 on S\mathcal{S}:

VU2dV=0\int_{\mathcal{V}} \lvert\nabla U\rvert^2\, dV = 0

Since the integrand is non-negative, U=0\nabla U = \mathbf{0} everywhere in V\mathcal{V} So UU is Constant. With U=0U = 0 on the boundary, U=0U = 0 throughout V\mathcal{V}. Hence V1=V2V_1 = V_2. \blacksquare

Theorem 2.4 (Uniqueness for Neumann conditions). The solution is unique up to an additive Constant when V/n\partial V/\partial n is specified on S\mathcal{S}.

Proof. The same argument applies, but now U/n=0\partial U/\partial n = 0 on S\mathcal{S} and the Right-hand side of Green’s identity vanishes for a different reason. We again conclude U=0\nabla U = \mathbf{0} So UU is constant. \blacksquare

2.8 Method of Images

The method of images replaces a problem with conductors by an equivalent problem with charges only, Exploiting the uniqueness theorem.

Point charge above a grounded plane. A charge qq is placed at distance dd above an Infinite grounded conducting plane (V=0V = 0 at z=0z = 0).

Replace the plane by an image charge q=qq' = -q at z=dz = -d. The potential for z>0z \gt 0 is:

V(x,y,z)=14πε0[qx2+y2+(zd)2qx2+y2+(z+d)2]V(x,y,z) = \frac{1}{4\pi\varepsilon_0}\left[\frac{q}{\sqrt{x^2 + y^2 + (z-d)^2}} - \frac{q}{\sqrt{x^2 + y^2 + (z+d)^2}}\right]

This satisfies 2V=0\nabla^2 V = 0 for z>0z \gt 0 (away from the charge), V=0V = 0 at z=0z = 0 And V0V \to 0 as rr \to \infty. By the uniqueness theorem, this is the correct solution.

The force on qq is the force due to the image charge:

F=q24πε0(2d)2z^\mathbf{F} = -\frac{q^2}{4\pi\varepsilon_0 (2d)^2}\,\hat{\mathbf{z}}

The induced surface charge density on the plane:

σ(x,y)=ε0Vzz=0=qd2π(x2+y2+d2)3/2\sigma(x,y) = -\varepsilon_0 \left.\frac{\partial V}{\partial z}\right|_{z=0} = -\frac{qd}{2\pi(x^2+y^2+d^2)^{3/2}}

Example: Point charge inside a grounded sphere. A charge qq is at distance aa from the centre Of a grounded conducting sphere of radius RR (a<Ra \lt R).

The image charge is q=qR/aq' = -qR/a located at distance b=R2/ab = R^2/a from the centre, along the same Radial line.

Solution: Verifying the image charge

We must verify that V=0V = 0 on the sphere. Place qq at distance aa from the origin along the zz-axis and qq' at distance bb along the zz-axis. At any point on the sphere at distance RR From the origin, the distances to qq and qq' are d1d_1 and d2d_2 where:

d12=R2+a22Racosθ,d22=R2+b22Rbcosθd_1^2 = R^2 + a^2 - 2Ra\cos\theta, \quad d_2^2 = R^2 + b^2 - 2Rb\cos\theta

For V=0V = 0 on the sphere, we need q/d1=q/d2q/d_1 = -q'/d_2 for all θ\theta. This requires the ratio d2/d1d_2/d_1 to be constant. Setting b=R2/ab = R^2/a:

d22d12=R2+R4/a22R3cosθ/aR2+a22Racosθ=R2a2\frac{d_2^2}{d_1^2} = \frac{R^2 + R^4/a^2 - 2R^3\cos\theta/a}{R^2 + a^2 - 2Ra\cos\theta} = \frac{R^2}{a^2}

The ratio is indeed constant. Choosing q=qR/aq' = -qR/a gives q/d1+q/d2=0q/d_1 + q'/d_2 = 0 on the sphere. \blacksquare

2.9 Multipole Expansion

For a localized charge distribution ρ(r)\rho(\mathbf{r}')The potential at large distance r=rr=rr = \lvert\mathbf{r}\rvert \gg r' = \lvert\mathbf{r}'\rvert is expanded using 1rr=n=0rnrn+1Pn(cosα)\frac{1}{\lvert\mathbf{r}-\mathbf{r}'\rvert} = \sum_{n=0}^{\infty} \frac{r'^n}{r^{n+1}} P_n(\cos\alpha) Where α\alpha is the angle between r\mathbf{r} and r\mathbf{r}':

V(r)=14πε0n=01rn+1rnPn(cosα)ρ(r)d3rV(\mathbf{r}) = \frac{1}{4\pi\varepsilon_0}\sum_{n=0}^{\infty}\frac{1}{r^{n+1}}\int r'^n P_n(\cos\alpha)\,\rho(\mathbf{r}')\,d^3\mathbf{r}'

Monopole term (n=0n = 0):

V0=14πε0Qr,Q=ρ(r)d3rV_0 = \frac{1}{4\pi\varepsilon_0}\frac{Q}{r}, \quad Q = \int \rho(\mathbf{r}')\,d^3\mathbf{r}'

This is the potential of a point charge at the origin.

Dipole term (n=1n = 1):

V1=14πε0pr^r2,p=rρ(r)d3rV_1 = \frac{1}{4\pi\varepsilon_0}\frac{\mathbf{p} \cdot \hat{\mathbf{r}}}{r^2}, \quad \mathbf{p} = \int \mathbf{r}'\,\rho(\mathbf{r}')\,d^3\mathbf{r}'

Where p\mathbf{p} is the electric dipole moment.

Quadrupole term (n=2n = 2): Depends on the quadrupole moment tensor:

Qij=(3rirjr2δij)ρ(r)d3rQ_{ij} = \int (3r_i' r_j' - r'^2 \delta_{ij})\,\rho(\mathbf{r}')\,d^3\mathbf{r}'

V2=14πε012r3i,jQijr^ir^jV_2 = \frac{1}{4\pi\varepsilon_0}\frac{1}{2r^3}\sum_{i,j} Q_{ij}\,\hat{r}_i\,\hat{r}_j

For a neutral charge distribution (Q=0Q = 0), the dipole term dominates. If additionally p=0\mathbf{p} = \mathbf{0}The quadrupole term dominates.

Example: Dipole potential of two charges

A charge +q+q at z=+d/2z = +d/2 and q-q at z=d/2z = -d/2.

The dipole moment: p=q(d/2)z^+(q)(d/2)z^=qdz^\mathbf{p} = q(d/2)\,\hat{\mathbf{z}} + (-q)(-d/2)\,\hat{\mathbf{z}} = qd\,\hat{\mathbf{z}}.

On the zz-axis (θ=0\theta = 0): V1=qd4πε0r2V_1 = \frac{qd}{4\pi\varepsilon_0 r^2}.

In the equatorial plane (θ=π/2\theta = \pi/2): V1=0V_1 = 0.

The exact potential on the zz-axis is:

V=q4πε0(1rd/21r+d/2)=q4πε0dr2d2/4V = \frac{q}{4\pi\varepsilon_0}\left(\frac{1}{r-d/2} - \frac{1}{r+d/2}\right) = \frac{q}{4\pi\varepsilon_0}\frac{d}{r^2 - d^2/4}

For rdr \gg d: this reduces to V1=qd4πε0r2V_1 = \frac{qd}{4\pi\varepsilon_0 r^2}Confirming the Dipole approximation. \blacksquare

2.10 Dielectrics

Polarization. When an external field E\mathbf{E} is applied to a dielectric, the material Develops a polarization P\mathbf{P}The dipole moment per unit volume. This produces bound charges:

ρb=P,σb=Pn^\rho_b = -\nabla \cdot \mathbf{P}, \quad \sigma_b = \mathbf{P} \cdot \hat{\mathbf{n}}

The displacement field D\mathbf{D} is defined as:

D=ε0E+P\mathbf{D} = \varepsilon_0 \mathbf{E} + \mathbf{P}

Gauss’s law in terms of D\mathbf{D}:

D=ρf\nabla \cdot \mathbf{D} = \rho_f

Where ρf\rho_f is the free charge density. This form is useful because D\mathbf{D} depends Only on free charges, not bound charges.

Linear dielectrics. For an isotropic linear dielectric:

P=ε0χeE,D=εE\mathbf{P} = \varepsilon_0 \chi_e \mathbf{E}, \quad \mathbf{D} = \varepsilon \mathbf{E}

Where χe\chi_e is the electric susceptibility and ε=ε0(1+χe)\varepsilon = \varepsilon_0(1 + \chi_e) is the Permittivity. The relative permittivity (dielectric constant) is εr=ε/ε0=1+χe\varepsilon_r = \varepsilon/\varepsilon_0 = 1 + \chi_e.

Boundary conditions at dielectric interfaces (no free charges):

D1n=D2n    ε1E1n=ε2E2nD_{1n} = D_{2n} \implies \varepsilon_1 E_{1n} = \varepsilon_2 E_{2n}

E1t=E2tE_{1t} = E_{2t}

The tangential component of E\mathbf{E} is continuous, but the normal component changes. The angles of the field with respect to the normal satisfy ε1tanθ2=ε2tanθ1\varepsilon_1 \tan\theta_2 = \varepsilon_2 \tan\theta_1.

Example: Dielectric slab in a uniform field

A dielectric slab of permittivity ε\varepsilon and thickness dd is placed in a uniform External field E0\mathbf{E}_0 perpendicular to its faces.

Outside the slab: E=E0\mathbf{E} = \mathbf{E}_0.

Inside the slab: by continuity of DnD_n:

Din=Dout=ε0E0D_{\mathrm{in} = D_{\mathrm{out} = \varepsilon_0 E_0}}

E_{\mathrm{in} = \frac{D_{\mathrm{in}}{\varepsilon} = \frac{\varepsilon_0}{\varepsilon} E_0 = \frac{E_0}{\varepsilon_r}}}

The polarization: P=ε0χeEin=ε0(εr1)E0εrP = \varepsilon_0 \chi_e E_{\mathrm{in} = \varepsilon_0 (\varepsilon_r - 1) \frac{E_0}{\varepsilon_r}}.

The bound surface charge density on each face:

σb=±P=±ε0(11εr)E0\sigma_b = \pm P = \pm \varepsilon_0 \left(1 - \frac{1}{\varepsilon_r}\right) E_0

The bound charges produce a field opposing E0\mathbf{E}_0Reducing the net field inside the Dielectric. \blacksquare

flowchart TD
    A[2_Electrostaticsx] --> B[Key Concepts]
    A --> C[Core Principles]
    A --> D[Practical Applications]
    B --> E[Fundamental definitions]
    C --> F[Design patterns]
    D --> G[Real-world usage]

Intuition

Electrostatics studies how stationary charges create electric fields and potentials. Gauss’s law is a bookkeeping tool: the total flux through any closed surface equals the enclosed charge divided by the permittivity, regardless of surface shape. This makes symmetric problems trivial to solve. The potential is like a topographic map of electrical height, where charges sit on hills. The uniqueness theorem guarantees that any solution satisfying the boundary conditions is the only solution, so clever guesses like the method of images are valid. Dielectrics respond to external fields by polarising, creating bound charges that partially cancel the applied field.

Common Mistakes

Mistake 1: Using Gauss’s law when the symmetry is insufficient Gauss’s law is always true, but it is only useful for computing E\mathbf{E} when the charge distribution has sufficient symmetry (spherical, cylindrical, or planar) to pull EE out of the integral. Applying it to asymmetric distributions without the symmetry argument gives an integral equation that cannot be solved analytically.

Mistake 2: Confusing the potential of a point charge with the potential energy The electric potential V=q/(4πε0r)V = q/(4\pi\varepsilon_0 r) is the potential energy per unit charge, not the total energy. To find the energy of a system of charges, you must compute U=12iqiViU = \frac{1}{2}\sum_i q_i V_i or equivalently U=12ρVd3rU = \frac{1}{2}\int \rho V\, d^3\mathbf{r}. The factor of 12\frac{1}{2} avoids double-counting.

Mistake 3: Assuming the electric field is continuous across a charged surface The normal component of E\mathbf{E} is discontinuous across a surface charge density σ\sigma: E2nE1n=σ/ε0E_{2n} - E_{1n} = \sigma/\varepsilon_0. Only the tangential component EtE_t is continuous. Students who assume full continuity obtain incorrect boundary conditions for dielectric interfaces.

Cross-References

  • Maxwell’s Equations: Electrostatics provides the static electric field solutions that form two of Maxwell’s four equations.
  • Potentials and Gauge Transformations: The electric potential introduced here is the scalar potential used in the general gauge theory framework.
  • Electrodynamics: Electrostatics is the zero-velocity limit of the full electrodynamics theory developed in the next chapter.

References

  1. Griffiths, D. J. (2017). Introduction to Electrodynamics (4th ed.). Cambridge University Press.
  2. Purcell, E. M. & Morin, D. J. (2013). Electricity and Magnetism (3rd ed.). Cambridge University Press.
  3. Jackson, J. D. (1998). Classical Electrodynamics (3rd ed.). John Wiley & Sons.
  4. Zangwill, A. I. (2013). Modern Electrodynamics. Cambridge University Press.
  5. Feynman, R. P., Leighton, R. B. & Sands, M. (2011). The Feynman Lectures on Physics, Vol. II: The New Millennium Edition — Mainly Electromagnetism and Matter. Basic Books.