§3. Electromagnetic Waves §3.4. EM fields (waves) in conductors The behaviour of EM waves in a conductor is quite different from that in a source-free medium. The conduction current in a conductor is the cause of the difference. We shall analyze the source terms in the Maxwell’s equations to simplify Maxwell’s equations in a conductor. From this set of equations, we can derive a diffusion equation and investigate the skin effects. §3.4.1 Skin Effects in Conductors A. Maxwell’s Equations in a Conductor Complete Maxwell’s equations: ρ − → ∇· E = ² − → ∂B − → ∇× E = − ∂t − → ∇· B = 0 − → ∂ E − → ∇× B = µ ~j + ² ∂t Fact 1: Conducting current dominates over the displacement current In a conductor, the electric field is the driving source for the conduction current. The collision is the source of impedance. The conduction current is governed by the Ohm’s law: − → − → j f = σE where σ (S/m) is the conductivity. The AC conductivity differs from the DC conductivity. Let ν be the collision frequency of electrons (current carrier in conductors) with ions and ω the frequency of the EM waves in the conductor. The equation of motion for electrons is: m → d− v − → → = −e E − mν − v dt → → Assume − v =− v 0 e−iωt and use ∂/∂t → −iω, we obtain − → → → −iωm− v = −e E − mν − v → Phys 463, E & M III, C. Xiao − → v = −e − → E m(ν − iω) 1 / note11 − → → Recall the current density is expressed by j = −en− v (n is the electron number density in the conductor), ne2 − → − → jf= E m(ν − iω) which gives the AC conductivity in conductor: σ(ω) = 1 ne2 ν − iω m In practical situations, ω ¿ ν ∼ 1014 (1/sec) (infrared range). So the DC conductivity ne2 mν σ= can be used. Let’s now compare the magnitude of conduction current with that of the displacement current. − → − → Assume E = E 0 e−iωt . Then ¯ → ¯¯ ¯− ¯ j f¯ σE σ ¯ − ¯= = ¯ ∂→ ¯ ²ωE ²ω ¯² E ¯ ∂t In copper, σ = 6 × 107 (S/m). The condition for jf ' ² ω= − → ∂E , ∂t or σ ²ω ' 1 leads to σ 6 × 107 = ∼ 7 × 1019 (rad/sec) ² 8.85 × 10−12 At frequencies ω < 1012 (rad/sec) (communication wave frequency), σ À 1 or ²ω ¯− ¯ ¯→ ¯ ¯ j f¯ À Ampere’s law in a conductor: ¯ − ¯ ¯ →¯ ¯ ∂E ¯ ¯² ¯ ¯ ¯ ¯ ∂t ¯ − → − → − → ∇× B = µ j f = µσ E Fact 2: No significant charge accumulation Because of the good conductivity, no significant charge accumulation in a conductor is expected (ρ ' 0). Phys 463, E & M III, C. Xiao 2 / note11 From the charge conservation and Gauss’s law ρ − → ∇· E = ² ∂ρf − → ∇· j f = − ∂t we obtain ∂ρf σ − → = −σ∇· E = − ρf ∂t ε So σ ρf = ρf (0)e− ε t The free charge ρf (0) dissipates in a characteristic time τ = σε , similar to the static case in which the charge will flow out to the edge of the conductor. If the transient phase is excluded, ρf = 0 can be assumed in a conductor. For simplicity, we shall consider “good” conductor case in which the displacement current can be ignored. Maxwell’s equations in a conductor: − → ∇· E − → ∇× E − → ∇· B − → ∇× B = 0 − → ∂B = − ∂t = 0 − → = µσ E It can be shown that the EM waves in conductor are also TEM (Transverse EM ) waves B. Diffusion Equation As we did before for waves in source-free media, let’s apply curl operator to the 2nd Maxwell’s equation: − → ³ ´ ∂B ∂ ∂ ³ − − → − → →´ ∇× ∇× E = −∇× = − (∇× B ) = − µσ E ∂t ∂t ∂t LHS of the equation So ³ ³ − − →´ →´ − → − → ∇× ∇× E = ∇ ∇· E − ∇2 E = −∇2 E − → ∂E ∇ E = µσ Diffussion equation ∂t Similarly, the magnetic field also satisfies the same diffusion equation: − → ∂B → 2− ∇ B = µσ Diffussion equation ∂t → 2− Phys 463, E & M III, C. Xiao 3 / note11 C. Skin Depth Suppose we have a plane wave. It comes from the −z direction and reaches a large − → conductor surface at z = 0. Outside of a conductor: E = E0 e−iωt~ex at z = 0. Assume the wave inside the conductor has the form − → − → E = E 0 ei(kz−ωt) where k is an unknown constant. Recall ∂ → −iω ∂t ∇ → ik, for the waves of the above type, we find from the diffusion equation − → − → (ik)2 E = −iωµσ E π k 2 = iωµσ = ωµσe 2 i → r ωµσ √ k = ±e ωµσ = ±(1 + i) 2 π i 4 Choose “+” sign to allow the electric field to damp (to “propagate”) in the +z direction. Separate the real and imaginary parts of k: k = k+ + ik− , k+ = k− = r ωµσ 2 − → − → E = E 0 e−k− z ei(k+ z−ωt) − → − → B = B 0 e−k− z ei(k+ z−ωt) (1) (2) If the “good” conductor assumption is not valid, the displacement current should be included in the 4th Maxwell’s equation. The solution for E and B are the same as above with s 1/2 r µ ¶ εµ σ 2 1+ ± 1 k± = ω 2 εω The equations (1) and (2) indicate that the amplitude of E and B fields decays to 1/e of their values at z = 0 in a distance: δ= 1 k− Phys 463, E & M III, C. Xiao 4 / note11 where δ is called skin depth For a good conductor (σ À εω): δ= s 2 (m) ωµσ Also, the wavelength is λ = 2π/k+ = 2πδ inqa good conductor. The wave decays significantly within one wavelength. Since δ ∝ 1/ωσ, deep penetration occurs for 1. Low frequency 2. poor conductor Example: skin depth at f = 60 Hz for copper. δ= s 2 = 8 × 10−3 m = 8 mm −7 7 2π × 60 × 4π × 10 × 6 × 10 Phys 463, E & M III, C. Xiao 5 / note11 There is no advantage to construct AC transmission lines using wires with a radius much larger than the skin depth because the current flows mainly in the outer part of the conductor. For a poor conductor (σ ¿ εω): 2 δ= σ s ε (m) µ independent of the frequency. Example: For sea water, µ = µ0 = 4π × 10−7 N/A2 , ε ' 70²0 = 6 × 10−10 C2 /N·m2 , and σ ' 5 (Ω·m)−1 . Sea water is a poor conductor for frequency ω σ f= À = 109 Hz 2π 2πε or λ ¿ 30 cm. The skin depth is s s 2 ε 2 70ε0 δ = = σ µ σ µ0 √ √ 2 70 2 70 = = ' 1 cm σZ 5 × 377 In the radioq frequency range (f ¿ 109 Hz) sea water is a good conductor, the skin depth δ = 2/(ωµσ) is quite short. To reach a depth δ = 10 m, for communication with submarines, ω 1 f= ' 500 Hz = 2π πµσδ 2 Phys 463, E & M III, C. Xiao 6 / note11 The wavelength in the air is about λ= c 3 × 108 = = 600 km f 500 The required λ/4 antenna would be gigantic. §3.4.2 Monochromatic plane waves in a Conductor A. Transverse waves The E and B fields in a conductor ~ t) = B ~ 0 e−k− z ei(k+ z−ωt) B(z, ~ t) = E ~ 0 e−k− z ei(k+ z−ωt) , E(z, can be rewritten as ~ t) = E ~ 0 ei(kz−ωt) , E(z, ~ t) = B ~ 0 ei(kz−ωt) B(z, They have the same functions as EM wave in vacuum, except that k is a complex number Following the same calculation for waves in vacuum, we can derive from ~ = 0, ∇·E ~ =0 ∇·B and the following results: ~k · E ~ = k~ez · E ~ =0 ~k · B ~ = k~ez · B ~ =0 ~ and B ~ are perpendicular to ~ez , the wave propagation direction. Both E Let’s assume ~ = E0 ei(kz−ωt)~ex = E0 e−k− z ei(k+ z−ωt)~ex E From ~ ~ = − ∂B ∇×E ∂t we obtain ~ = k E0 e−k− z ei(k+ z−ωt)~ey B ω |k| iφ = e E0 e−k− z ei(k+ z−ωt)~ey ω where à ! k− φ = tan , k+ √ For a good conductor φ = 450 , |k| = ωµσ −1 |k| = q 2 2 k+ + k− The B fields lags behind the electric fields Phys 463, E & M III, C. Xiao 7 / note11 §4.3.3 Reflection of EM Waves on a Conductor Surface We have seen that the EM waves do not penetrate the conductor deeply. Where do the waves go? Absorbed or reflected? Back to our example with a plane wave perpendicularly propagating to a conducting surface ~ = Hy~ey = H0 ei(z/δ−ωt) e−z/δ~ey H ~ = ~j = σEx~ex = σE0 ei(z/δ−ωt) e−z/δ~ex ∇×H ~ x = [∇ × (Hy~ey )]x = ∂Hz − ∂Hy = 1 − i Hy (∇ × H) ∂y ∂z δ | {z } =0 So 1−i Hy = σEx δ Phys 463, E & M III, C. Xiao 8 / note11 Characteristic impedance of the conductor Z = Ex 1−i 1−i = = Hy σδ σ 1−i = √ 2 r ωµ = σ s r ωµσ 2 −iωµ σ For 4mm microwave, f = 75 Ghz. If the conductor is aluminum (σAl = 2 × 107 S/m) r s ωµ 2π × 75 × 109 × 4π × 10−7 |ZAl | = = σ 2 × 107 = 0.17 Ω ¿ Zair = 377 Ω The reflectivity: Γ= ZAl − Zair −Zair ' = −1 ZAl + Zair Zair Almost complete reflection. Phys 463, E & M III, C. Xiao 9 / note11