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Electromagnetic Waves

5.1 The Wave Equation

In free space (ρ=0\rho = 0, J=0\mathbf{J} = \mathbf{0}), take the curl of Faraday’s law:

×(×E)=t(×B)=μ0ε02Et2\nabla \times (\nabla \times \mathbf{E}) = -\frac{\partial}{\partial t}(\nabla \times \mathbf{B}) = -\mu_0 \varepsilon_0 \frac{\partial^2 \mathbf{E}}{\partial t^2}

Using the identity ×(×E)=(E)2E\nabla \times (\nabla \times \mathbf{E}) = \nabla(\nabla \cdot \mathbf{E}) - \nabla^2 \mathbf{E} And E=0\nabla \cdot \mathbf{E} = 0:

2E=μ0ε02Et2\nabla^2 \mathbf{E} = \mu_0 \varepsilon_0 \frac{\partial^2 \mathbf{E}}{\partial t^2}

Similarly: 2B=μ0ε02Bt2\nabla^2 \mathbf{B} = \mu_0 \varepsilon_0 \frac{\partial^2 \mathbf{B}}{\partial t^2}.

These are wave equations with wave speed c=1/μ0ε03×108c = 1/\sqrt{\mu_0 \varepsilon_0} \approx 3 \times 10^8 m/s.

5.2 Properties of EM Waves

Theorem 5.1. Electromagnetic waves in free space are:

  1. Transverse: E\mathbf{E} and B\mathbf{B} are perpendicular to the direction of propagation.
  2. Mutually perpendicular: EB\mathbf{E} \perp \mathbf{B}.
  3. In phase: E=cBE = cB at every point.
  4. Linearly polarised (; other polarisations are superpositions).

Energy. The energy density of an EM wave is u=12(ε0E2+B2/μ0)u = \frac{1}{2}(\varepsilon_0 E^2 + B^2/\mu_0).

The Poynting vector S=1μ0E×B\mathbf{S} = \frac{1}{\mu_0}\mathbf{E} \times \mathbf{B} represents the energy Flux (power per unit area).

5.3 Worked Example

Problem. Show that E=E0cos(kzωt)x^\mathbf{E} = E_0 \cos(kz - \omega t)\,\hat{\mathbf{x}} satisfies the wave Equation and find the associated B\mathbf{B} field.

Solution. 2E=2Exz2x^=k2E0cos(kzωt)x^\nabla^2 \mathbf{E} = \frac{\partial^2 E_x}{\partial z^2}\hat{\mathbf{x}} = -k^2 E_0 \cos(kz - \omega t)\,\hat{\mathbf{x}}.

2Et2=ω2E0cos(kzωt)x^\frac{\partial^2 \mathbf{E}}{\partial t^2} = -\omega^2 E_0 \cos(kz - \omega t)\,\hat{\mathbf{x}}.

The wave equation requires k2=μ0ε0ω2k^2 = \mu_0 \varepsilon_0 \omega^2I.e., ω/k=c\omega/k = c.

From Faraday’s law: ×E=Bt\nabla \times \mathbf{E} = -\frac{\partial \mathbf{B}}{\partial t}.

(×E)y=Exz=kE0sin(kzωt)(\nabla \times \mathbf{E})_y = -\frac{\partial E_x}{\partial z} = k E_0 \sin(kz - \omega t)

Byt=kE0sin(kzωt)    By=kωE0cos(kzωt)=E0ccos(kzωt)\frac{\partial B_y}{\partial t} = -k E_0 \sin(kz - \omega t) \implies B_y = \frac{k}{\omega} E_0 \cos(kz - \omega t) = \frac{E_0}{c}\cos(kz - \omega t)

So B=E0ccos(kzωt)y^\mathbf{B} = \frac{E_0}{c}\cos(kz - \omega t)\,\hat{\mathbf{y}}. \blacksquare

5.4 Poynting’s Theorem and Energy Conservation

Poynting’s theorem is the statement of energy conservation for electromagnetic fields.

Derivation. Start with the two Maxwell equations containing time derivatives:

×E=Bt,×B=μ0J+μ0ε0Et\nabla \times \mathbf{E} = -\frac{\partial \mathbf{B}}{\partial t}, \quad \nabla \times \mathbf{B} = \mu_0 \mathbf{J} + \mu_0 \varepsilon_0 \frac{\partial \mathbf{E}}{\partial t}

Compute B(×E)E(×B)\mathbf{B} \cdot (\nabla \times \mathbf{E}) - \mathbf{E} \cdot (\nabla \times \mathbf{B}):

B(×E)=BBt=t(B22)\mathbf{B} \cdot (\nabla \times \mathbf{E}) = -\mathbf{B} \cdot \frac{\partial \mathbf{B}}{\partial t} = -\frac{\partial}{\partial t}\left(\frac{B^2}{2}\right)

E(×B)=μ0EJμ0ε0EEt=μ0EJt(ε0E22)-\mathbf{E} \cdot (\nabla \times \mathbf{B}) = -\mu_0 \mathbf{E} \cdot \mathbf{J} - \mu_0 \varepsilon_0 \mathbf{E} \cdot \frac{\partial \mathbf{E}}{\partial t} = -\mu_0 \mathbf{E} \cdot \mathbf{J} - \frac{\partial}{\partial t}\left(\frac{\varepsilon_0 E^2}{2}\right)

Using the vector identity (E×B)=B(×E)E(×B)\nabla \cdot (\mathbf{E} \times \mathbf{B}) = \mathbf{B} \cdot (\nabla \times \mathbf{E}) - \mathbf{E} \cdot (\nabla \times \mathbf{B}):

(E×B)=μ0JEμ0ε0t(E22)t(B22)\nabla \cdot (\mathbf{E} \times \mathbf{B}) = -\mu_0 \mathbf{J} \cdot \mathbf{E} - \mu_0 \varepsilon_0 \frac{\partial}{\partial t}\left(\frac{E^2}{2}\right) - \frac{\partial}{\partial t}\left(\frac{B^2}{2}\right)

Dividing by μ0\mu_0 and rearranging:

S=JE+ut\boxed{-\nabla \cdot \mathbf{S} = \mathbf{J} \cdot \mathbf{E} + \frac{\partial u}{\partial t}}

Where S=1μ0E×B\mathbf{S} = \frac{1}{\mu_0}\mathbf{E} \times \mathbf{B} is the Poynting vector and u=12(ε0E2+B2μ0)u = \frac{1}{2}\left(\varepsilon_0 E^2 + \frac{B^2}{\mu_0}\right) is the energy density.

Interpretation: The rate of energy leaving a volume equals the work done on charges plus The rate of increase of field energy. In integral form:

SSdA=ddtVudV+VJEdV-\oint_S \mathbf{S} \cdot d\mathbf{A} = \frac{d}{dt}\int_V u\,dV + \int_V \mathbf{J} \cdot \mathbf{E}\,dV

5.5 EM Wave Propagation: Worked Examples

Intensity. For a plane wave, the time-averaged Poynting vector is:

S=E022μ0ck^=12ε0cE02k^\langle\mathbf{S}\rangle = \frac{E_0^2}{2\mu_0 c}\,\hat{\mathbf{k}} = \frac{1}{2}\varepsilon_0 c E_0^2\,\hat{\mathbf{k}}

Example: Radiation pressure

A plane wave normally incident on a perfectly absorbing surface exerts a radiation pressure. The momentum flux of the wave is S/c\langle S \rangle/c per unit area, so:

Pabs=Sc=ε0E022P_{\mathrm{abs} = \frac{\langle S \rangle}{c} = \frac{\varepsilon_0 E_0^2}{2}}

For a perfectly reflecting surface, the momentum transfer is doubled:

Pref=2Sc=ε0E02P_{\mathrm{ref} = \frac{2\langle S \rangle}{c} = \varepsilon_0 E_0^2}

A 1 kW/m2^2 beam (like sunlight near Earth) exerts a pressure of about 3.3 μ3.3\ \muPa on a Perfect absorber. \blacksquare

Example: Polarization of EM waves

Linear polarization. E=E0cos(kzωt)x^\mathbf{E} = E_0\cos(kz - \omega t)\,\hat{\mathbf{x}}. The field Oscillates in a fixed direction.

Circular polarization. Two orthogonal linear polarizations with a phase difference of π/2\pi/2:

E=E0cos(kzωt)x^±E0sin(kzωt)y^\mathbf{E} = E_0\cos(kz - \omega t)\,\hat{\mathbf{x}} \pm E_0\sin(kz - \omega t)\,\hat{\mathbf{y}}

The tip of E\mathbf{E} traces a circle. The ++ sign gives left-circular polarization (LCP) and the - sign gives right-circular polarization (RCP).

Elliptical polarization. The general case with arbitrary amplitudes and phase:

E=E0xcos(kzωt)x^+E0ycos(kzωt+δ)y^\mathbf{E} = E_{0x}\cos(kz - \omega t)\,\hat{\mathbf{x}} + E_{0y}\cos(kz - \omega t + \delta)\,\hat{\mathbf{y}}

\blacksquare

5.6 EM Waves in Conductors

In a conductor with conductivity σ\sigmaOhm’s law gives J=σE\mathbf{J} = \sigma\mathbf{E}. Substituting into the Ampere-Maxwell law:

×B=μ0σE+μ0ε0Et\nabla \times \mathbf{B} = \mu_0\sigma\mathbf{E} + \mu_0\varepsilon_0\frac{\partial \mathbf{E}}{\partial t}

For a monochromatic wave E=E0eiωt\mathbf{E} = \mathbf{E}_0\,e^{-i\omega t}This leads to a complex Wave number:

k~2=μ0ε0ω2+iμ0σω\tilde{k}^2 = \mu_0\varepsilon_0\omega^2 + i\mu_0\sigma\omega

Writing k~=k+iκ\tilde{k} = k + i\kappa where kk is the real part (wave number) and κ\kappa is the Imaginary part (attenuation constant):

E(z,t)=E0eκzcos(kzωt)\mathbf{E}(z,t) = \mathbf{E}_0\,e^{-\kappa z}\cos(kz - \omega t)

The field decays exponentially. The skin depth is the distance over which the amplitude Falls by a factor of 1/e1/e:

δ=1κ\delta = \frac{1}{\kappa}

For a good conductor (σε0ω\sigma \gg \varepsilon_0\omega):

δ=2μ0σω\delta = \sqrt{\frac{2}{\mu_0\sigma\omega}}

Example: Skin depth in copper at 60 Hz and 1 MHz

Copper: σ=5.96×107\sigma = 5.96 \times 10^7 S/m, μr1\mu_r \approx 1.

At f=60f = 60 Hz (ω=2π×60\omega = 2\pi \times 60 rad/s):

δ=24π×107×5.96×107×2π×608.5 mm\delta = \sqrt{\frac{2}{4\pi \times 10^{-7} \times 5.96 \times 10^7 \times 2\pi \times 60}} \approx 8.5\ \mathrm{mm}

At f=1f = 1 MHz (ω=2π×106\omega = 2\pi \times 10^6 rad/s):

δ=24π×107×5.96×107×2π×10665 μm\delta = \sqrt{\frac{2}{4\pi \times 10^{-7} \times 5.96 \times 10^7 \times 2\pi \times 10^6}} \approx 65\ \mu\mathrm{m}

The skin depth decreases as 1/f1/\sqrt{f}So higher-frequency signals are confined to thinner Surface layers. \blacksquare

5.7 Waveguides

Electromagnetic waves can be guided by hollow conducting pipes (waveguides). Consider a Rectangular waveguide with dimensions aa (width) and bb (height).

TE modes (transverse electric, Ez=0E_z = 0, Bz0B_z \neq 0). The lowest-order mode is \mathrm{TE_}{10}With fields:

Ey=E0sin ⁣(πxa)cos(kgzωt)E_y = E_0 \sin\!\left(\frac{\pi x}{a}\right)\cos(k_g z - \omega t)

Bx=kgωE0sin ⁣(πxa)cos(kgzωt)B_x = -\frac{k_g}{\omega}E_0 \sin\!\left(\frac{\pi x}{a}\right)\cos(k_g z - \omega t)

Bz=πωaE0cos ⁣(πxa)sin(kgzωt)B_z = \frac{\pi}{\omega a}E_0 \cos\!\left(\frac{\pi x}{a}\right)\sin(k_g z - \omega t)

Where the guide wave number is kg=(ω/c)2(π/a)2k_g = \sqrt{(\omega/c)^2 - (\pi/a)^2}.

Cutoff frequency. Waves propagate only when ω>ωc\omega \gt \omega_c where:

ωc,mn=cπ(ma)2+(nb)2\omega_{c,mn} = c\pi\sqrt{\left(\frac{m}{a}\right)^2 + \left(\frac{n}{b}\right)^2}

For the \mathrm{TE_}{10} mode: fc=c2af_c = \frac{c}{2a}.

Phase and group velocities. In a waveguide, the phase velocity exceeds cc:

vp=ωkg=c1(ωc/ω)2>cv_p = \frac{\omega}{k_g} = \frac{c}{\sqrt{1 - (\omega_c/\omega)^2}} \gt c

The group velocity (signal velocity) is less than cc:

vg=dωdkg=c1(ωc/ω)2<cv_g = \frac{d\omega}{dk_g} = c\sqrt{1 - (\omega_c/\omega)^2} \lt c

They satisfy vpvg=c2v_p\,v_g = c^2.

:::caution Common Pitfall The phase velocity in a waveguide exceeds ccBut this does not violate special relativity. No information or energy travels faster than cc; the signal velocity is the group velocity vg<cv_g \lt c. The phase velocity is the speed of the wave crests, which is a purely Kinematic quantity.

5.8 Electric Dipole Radiation

An oscillating electric dipole is the simplest source of electromagnetic radiation.

Consider a dipole p(t)=p0cos(ωt)z^\mathbf{p}(t) = p_0\cos(\omega t)\,\hat{\mathbf{z}}. In the radiation zone (rλr \gg \lambda), the fields are:

E=μ0p0ω24πsinθrcos[ω(tr/c)]θ^\mathbf{E} = -\frac{\mu_0 p_0 \omega^2}{4\pi}\frac{\sin\theta}{r}\cos[\omega(t - r/c)]\,\hat{\boldsymbol{\theta}}

B=μ0p0ω24πcsinθrcos[ω(tr/c)]ϕ^\mathbf{B} = -\frac{\mu_0 p_0 \omega^2}{4\pi c}\frac{\sin\theta}{r}\cos[\omega(t - r/c)]\,\hat{\boldsymbol{\phi}}

The fields fall off as 1/r1/r (not 1/r21/r^2 as for static fields), which is characteristic of Radiation.

Radiation pattern. The intensity varies as sin2θ\sin^2\thetaWith maximum radiation in the Equatorial plane (θ=π/2\theta = \pi/2) and zero along the dipole axis (θ=0,π\theta = 0, \pi).

Total radiated power. Integrating the Poynting vector over a sphere:

P=μ0p02ω412πcP = \frac{\mu_0 p_0^2 \omega^4}{12\pi c}

Larmor formula. For a point charge qq undergoing acceleration aa:

P=q2a26πε0c3P = \frac{q^2 a^2}{6\pi\varepsilon_0 c^3}

This is the non-relativistic limit and is valid whenever vcv \ll c.

Derivation: Power radiated by an oscillating dipole

The time-averaged Poynting vector magnitude in the radiation zone:

S=12μ0EθBϕ=μ0p02ω432π2csin2θr2\langle S \rangle = \frac{1}{2\mu_0}\lvert E_\theta\rvert\,\lvert B_\phi\rvert = \frac{\mu_0 p_0^2\omega^4}{32\pi^2 c}\frac{\sin^2\theta}{r^2}

The total power through a sphere of radius rr:

P=02π ⁣ ⁣0πSr2sinθdθdϕ=μ0p02ω432π2c2π0πsin3θdθP = \int_0^{2\pi}\!\!\int_0^\pi \langle S \rangle\, r^2\sin\theta\,d\theta\,d\phi = \frac{\mu_0 p_0^2\omega^4}{32\pi^2 c} \cdot 2\pi \int_0^\pi \sin^3\theta\,d\theta

Using 0πsin3θdθ=4/3\int_0^\pi \sin^3\theta\,d\theta = 4/3:

P=μ0p02ω432π2c2π43=μ0p02ω412πcP = \frac{\mu_0 p_0^2\omega^4}{32\pi^2 c} \cdot 2\pi \cdot \frac{4}{3} = \frac{\mu_0 p_0^2\omega^4}{12\pi c}

\blacksquare

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