Motional EMF and Maxwell's Equations Motional EMF Magnetic force on charge q q q moving with velocity u u u in a magnetic field B B B : This magnetic force is equivalent to the electrical force that would be exerted on the particle by the electric field E m E_m E m given by This, in turn, induces a voltage difference between ends 1 and 2, with end 2 being at the higher potential. The induced voltage is called a motional emf. If any segment of a closed circuit with contour C C C moves with a velocity u u u across a static magnetic field B B B , then the induced motional emf is given byV < e m > e m f = ∮ < / e m > C ( u × B ) ⋅ d l V<em>{emf} = \oint</em>C (u \times B) \cdot dl V < e m > e m f = ∮ < / e m > C ( u × B ) ⋅ d l Only those segments of the circuit that cross magnetic field lines contribute to V e m f V_{emf} V e m f . Example 6-3: Sliding Bar The length of the loop is related to u u u by x 0 = u t x_0 = ut x 0 = u t . Note that B B B increases with x x x Example 6-5: Moving Rod Next to a Wire The wire carries a current I = 10 A I = 10 A I = 10 A . A 30-cm-long metal rod moves with a constant velocity u = 25 m / s u = 25 m/s u = 25 m / s . Find V 12 V_{12} V 12 . B = μ 0 I 2 π r z ^ B = \frac{\mu_0 I}{2 \pi r} \hat{z} B = 2 π r μ 0 I z ^ V < e m > 12 = ∫ < / e m > 10 c m 40 c m ( u × B ) ⋅ d l = ∫ < e m > 10 c m 40 c m ( 25 x ^ × μ < / e m > 0 I 2 π r z ^ ) ⋅ x ^ d r V<em>{12} = \int</em>{10 cm}^{40 cm} (u \times B) \cdot dl = \int<em>{10 cm}^{40 cm} (25 \hat{x} \times \frac{\mu</em>0 I}{2 \pi r} \hat{z}) \cdot \hat{x} dr V < e m > 12 = ∫ < / e m > 10 c m 40 c m ( u × B ) ⋅ d l = ∫ < e m > 10 c m 40 c m ( 25 x ^ × 2 π r μ < / e m > 0 I z ^ ) ⋅ x ^ d r V < e m > 12 = ∫ < / e m > 10 c m 40 c m ( 25 μ < e m > 0 I 2 π r ) d r = 25 μ < / e m > 0 I 2 π ∫ 0.1 0.4 1 r d r V<em>{12} = \int</em>{10 cm}^{40 cm} (25 \frac{\mu<em>0 I}{2 \pi r}) dr = \frac{25 \mu</em>0 I}{2 \pi} \int_{0.1}^{0.4} \frac{1}{r} dr V < e m > 12 = ∫ < / e m > 10 c m 40 c m ( 25 2 π r μ < e m > 0 I ) d r = 2 π 25 μ < / e m > 0 I ∫ 0.1 0.4 r 1 d r V 12 = 25 × 4 π × 10 − 7 × 10 2 π ln ( 0.4 0.1 ) = 5 × 4 π × 10 − 7 × 10 × l n ( 4 ) = 13.9 μ V V_{12} = \frac{25 \times 4 \pi \times 10^{-7} \times 10}{2 \pi} \ln(\frac{0.4}{0.1}) = 5 \times 4 \pi \times 10^{-7} \times 10 \times ln(4) = 13.9 \mu V V 12 = 2 π 25 × 4 π × 1 0 − 7 × 10 ln ( 0.1 0.4 ) = 5 × 4 π × 1 0 − 7 × 10 × l n ( 4 ) = 13.9 μ V EM Motor/Generator Reciprocity Motor: Electrical to mechanical energy conversion Generator: Mechanical to electrical energy conversion EM Generator EMF As the loop rotates with an angular velocity ω \omega ω about its own axis, segment 1–2 moves with velocity u u u . Segment 3-4 moves with velocity − u -u − u . Displacement Current This term is conduction current I C I_C I C . This term must represent a current. Application of Stokes’s theorem gives: Define Displacement Current The displacement current does not involve real charges; it is an equivalent current that depends on the rate of change of the electric field. Capacitor Circuit Given: Wires are perfect conductors and capacitor insulator material is perfect dielectric. For Surface S1: I < e m > 1 = I < / e m > 1 c + I 1 d I<em>1 = I</em>{1c} + I_{1d} I < e m > 1 = I < / e m > 1 c + I 1 d . (D = 0 D = 0 D = 0 in perfect conductor) Capacitor Circuit For Surface S2: I < e m > 2 = I < / e m > 2 c + I 2 d I<em>2 = I</em>{2c} + I_{2d} I < e m > 2 = I < / e m > 2 c + I 2 d I 2 c = 0 I_{2c} = 0 I 2 c = 0 (perfect dielectric)Conclusion: I < e m > 1 = I < / e m > 2 I<em>1 = I</em>2 I < e m > 1 = I < / e m > 2 Example 6-7: Displacement Current Density Given: Conductivity " s i g m a = 2 × 10 7 S / m "sigma = 2 \times 10^7 S/m " s i g ma = 2 × 1 0 7 S / m and relative permittivity ϵ r = 1 \epsilon_r = 1 ϵ r = 1 . Conduction current: I c = 2 sin ( ω t ) ( m A ) I_c = 2 \sin(\omega t) (mA) I c = 2 sin ( ω t ) ( m A ) , where ω = 10 9 r a d / s \omega = 10^9 rad/s ω = 1 0 9 r a d / s . Find the displacement current. Solution I c = J A = σ E A I_c = JA = \sigma EA I c = J A = σ E A , where A is the cross-section of the wire.
E = I c σ A = 2 × 10 − 3 sin ( ω t ) 2 × 10 7 A = 10 − 10 sin ( ω t ) A ( V / m ) E = \frac{I_c}{\sigma A} = \frac{2 \times 10^{-3} \sin(\omega t)}{2 \times 10^7 A} = \frac{10^{-10} \sin(\omega t)}{A} (V/m) E = σ A I c = 2 × 1 0 7 A 2 × 1 0 − 3 s i n ( ω t ) = A 1 0 − 10 s i n ( ω t ) ( V / m ) .
D = ϵ E D = \epsilon E D = ϵ E , so I d = ∂ D ∂ t A = ϵ A ∂ E ∂ t I_d = \frac{\partial D}{\partial t} A = \epsilon A \frac{\partial E}{\partial t} I d = ∂ t ∂ D A = ϵ A ∂ t ∂ E .
I d = ϵ A ∂ ∂ t ( 10 − 10 A sin ( ω t ) ) = ϵ ω × 10 − 10 cos ( ω t ) = 8.85 × 10 − 12 × 10 9 × 10 − 10 cos ( ω t ) = 0.885 × 10 − 12 cos ( ω t ) ( A ) I_d = \epsilon A \frac{\partial}{\partial t} (\frac{10^{-10}}{A} \sin(\omega t)) = \epsilon \omega \times 10^{-10} \cos(\omega t) = 8.85 \times 10^{-12} \times 10^9 \times 10^{-10} \cos(\omega t) = 0.885 \times 10^{-12} \cos(\omega t) (A) I d = ϵ A ∂ t ∂ ( A 1 0 − 10 sin ( ω t )) = ϵ ω × 1 0 − 10 cos ( ω t ) = 8.85 × 1 0 − 12 × 1 0 9 × 1 0 − 10 cos ( ω t ) = 0.885 × 1 0 − 12 cos ( ω t ) ( A ) .
I < e m > c I<em>c I < e m > c and I < / e m > d I</em>d I < / e m > d are in phase quadrature (90° phase shift between them).
I < e m > d I<em>d I < e m > d is about nine orders of magnitude smaller than I < / e m > c I</em>c I < / e m > c , so the displacement current usually is ignored in good conductors.
Boundary Conditions Table summarizing boundary conditions for electric and magnetic fields between different media (Dielectric, Conductor). Tangential E General Form: n ^ < e m > 2 × ( E < / e m > 1 − E 2 ) = 0 \hat{n}<em>2 \times (E</em>1 - E_2) = 0 n ^ < e m > 2 × ( E < / e m > 1 − E 2 ) = 0 Dielectric-Dielectric: E < e m > 1 t = E < / e m > 2 t E<em>{1t} = E</em>{2t} E < e m > 1 t = E < / e m > 2 t Dielectric-Conductor: E < e m > 1 t = E < / e m > 2 t = 0 E<em>{1t} = E</em>{2t} = 0 E < e m > 1 t = E < / e m > 2 t = 0 Normal D General Form: n ^ < e m > 2 ⋅ ( D < / e m > 1 − D < e m > 2 ) = ρ < / e m > s \hat{n}<em>2 \cdot (D</em>1 - D<em>2) = \rho</em>s n ^ < e m > 2 ⋅ ( D < / e m > 1 − D < e m > 2 ) = ρ < / e m > s Dielectric-Dielectric: D < e m > 1 n − D < / e m > 2 n = ρ s D<em>{1n} - D</em>{2n} = \rho_s D < e m > 1 n − D < / e m > 2 n = ρ s Dielectric-Conductor: D < e m > 1 n = ρ < / e m > s , D 2 n = 0 D<em>{1n} = \rho</em>s, D_{2n} = 0 D < e m > 1 n = ρ < / e m > s , D 2 n = 0 Tangential H General Form: n ^ < e m > 2 × ( H < / e m > 1 − H < e m > 2 ) = J < / e m > s \hat{n}<em>2 \times (H</em>1 - H<em>2) = J</em>s n ^ < e m > 2 × ( H < / e m > 1 − H < e m > 2 ) = J < / e m > s Dielectric-Dielectric: H < e m > 1 t = H < / e m > 2 t H<em>{1t} = H</em>{2t} H < e m > 1 t = H < / e m > 2 t Dielectric-Conductor: H < e m > 1 t = J < / e m > s , H 2 t = 0 H<em>{1t} = J</em>s, H_{2t} = 0 H < e m > 1 t = J < / e m > s , H 2 t = 0 Normal B Charge Current Continuity Equation Current I I I out of a volume is equal to the rate of decrease of charge Q Q Q contained in that volume: ∑ I = 0 \sum I = 0 ∑ I = 0 EM Potentials Static Condition V ( R ) = 1 4 π ϵ ∫ < e m > V ′ ρ < / e m > v ( R ′ ) R ′ d v ′ V(R) = \frac{1}{4 \pi \epsilon} \int<em>{V'} \frac{\rho</em>v(R')}{R'} dv' V ( R ) = 4 π ϵ 1 ∫ < e m > V ′ R ′ ρ < / e m > v ( R ′ ) d v ′ Dynamic Condition V ( R , t ) = 1 4 π ϵ ∫ < e m > V ′ ρ < / e m > v ( R ′ , t ) R ′ d v ′ V(R, t) = \frac{1}{4 \pi \epsilon} \int<em>{V'} \frac{\rho</em>v(R', t)}{R'} dv' V ( R , t ) = 4 π ϵ 1 ∫ < e m > V ′ R ′ ρ < / e m > v ( R ′ , t ) d v ′ Dynamic condition with propagation delay V ( R , t ) = 1 4 π ϵ ∫ < e m > V ′ ρ < / e m > v ( R < e m > i , t − R ′ / u < / e m > p ) R ′ d v ′ V(R,t) = \frac{1}{4 \pi \epsilon} \int<em>{V'} \frac{\rho</em>v(R<em>i, t - R'/u</em>p)}{R'} dv' V ( R , t ) = 4 π ϵ 1 ∫ < e m > V ′ R ′ ρ < / e m > v ( R < e m > i , t − R ′ / u < / e m > p ) d v ′ A ( R , t ) = μ 4 π ∫ < e m > V ′ J ( R < / e m > i , t − R ′ / u p ) R ′ d v ′ A(R,t) = \frac{\mu}{4 \pi} \int<em>{V'} \frac{J(R</em>i, t - R'/u_p)}{R'} dv' A ( R , t ) = 4 π μ ∫ < e m > V ′ R ′ J ( R < / e m > i , t − R ′ / u p ) d v ′ Time Harmonic Potentials If charges and currents vary sinusoidally with time: we can use phasor notation: e.g., ∂ ∂ t ⇒ j ω \frac{\partial}{\partial t} \Rightarrow j \omega ∂ t ∂ ⇒ jω Expressions for potentials become: Maxwell’s Equations Time Harmonic Time harmonic implies ∂ ∂ t ⇒ j ω \frac{\partial}{\partial t} \Rightarrow j \omega ∂ t ∂ ⇒ jω Maxwell's Equations Time Harmonic ∇ × E ~ = − j ω μ H ~ \nabla \times \tilde{E} = -j \omega \mu \tilde{H} ∇ × E ~ = − jω μ H ~ H ~ = − 1 j ω μ ∇ × E ~ \tilde{H} = -\frac{1}{j \omega \mu} \nabla \times \tilde{E} H ~ = − jω μ 1 ∇ × E ~ ∇ × H ~ = j ω ϵ E ~ \nabla \times \tilde{H} = j \omega \epsilon \tilde{E} ∇ × H ~ = jω ϵ E ~ E ~ = 1 j ω ϵ ∇ × H ~ \tilde{E} = \frac{1}{j \omega \epsilon} \nabla \times \tilde{H} E ~ = jω ϵ 1 ∇ × H ~ Example 6-8: Relating E to H Given a nonconducting medium with ϵ = 16 ϵ < e m > 0 \epsilon = 16 \epsilon<em>0 ϵ = 16 ϵ < e m > 0 and μ = μ < / e m > 0 \mu = \mu</em>0 μ = μ < / e m > 0 , the electric field intensity of an electromagnetic wave is E ( z , t ) = x ^ 10 sin ( 10 10 t − k z ) ( V / m ) E(z, t) = \hat{x} 10 \sin(10^{10} t - kz) (V/m) E ( z , t ) = x ^ 10 sin ( 1 0 10 t − k z ) ( V / m ) Determine the associated magnetic field intensity H and find the value of k. Solution: Rewrite E ( z , t ) E(z, t) E ( z , t ) as E ( z , t ) = x ^ 10 cos ( 10 10 t − k z − π / 2 ) = R e [ E ~ ( z ) e j ω t ] E(z, t) = \hat{x} 10 \cos(10^{10} t - kz - \pi/2) = Re[\tilde{E}(z) e^{j \omega t}] E ( z , t ) = x ^ 10 cos ( 1 0 10 t − k z − π /2 ) = R e [ E ~ ( z ) e jω t ] , with ω = 10 10 r a d / s \omega = 10^{10} rad/s ω = 1 0 10 r a d / s E ~ ( z ) = x ^ 10 e − j k z e − j π / 2 = − y ^ j 10 e − j k z \tilde{E}(z) = \hat{x} 10 e^{-jkz} e^{-j\pi/2} = -\hat{y} j 10 e^{-jkz} E ~ ( z ) = x ^ 10 e − jk z e − jπ /2 = − y ^ j 10 e − jk z Example 6-8: Relating E to H (Continued) To find both H ~ ( z ) \tilde{H}(z) H ~ ( z ) and k k k , use Faraday's law to find H ~ ( z ) \tilde{H}(z) H ~ ( z ) ; then Ampère's law to find E ~ ( z ) \tilde{E}(z) E ~ ( z ) , which we will then compare with the original expression for E ~ ( z ) \tilde{E}(z) E ~ ( z ) to find k k k . Applying Faraday's Law: H ~ ( z ) = 1 j ω μ ∇ × E ~ = 1 j ω μ ∣ x ^ a m p ; y ^ a m p ; z ^ ∂ ∂ x a m p ; ∂ ∂ y a m p ; ∂ ∂ z 0 a m p ; − j 10 e − j k z a m p ; 0 ∣ \tilde{H}(z) = \frac{1}{j \omega \mu} \nabla \times \tilde{E} = \frac{1}{j \omega \mu} \begin{vmatrix} \hat{x} & \hat{y} & \hat{z} \ \frac{\partial}{\partial x} & \frac{\partial}{\partial y} & \frac{\partial}{\partial z} \ 0 & -j 10 e^{-jkz} & 0 \end{vmatrix} H ~ ( z ) = jω μ 1 ∇ × E ~ = jω μ 1 x ^ am p ; y ^ am p ; z ^ ∂ x ∂ am p ; ∂ y ∂ am p ; ∂ z ∂ 0 am p ; − j 10 e − jk z am p ; 0 H ~ ( z ) = 1 j ω μ x ^ ∂ ∂ z ( − j 10 e − j k z ) = x ^ 10 k ω μ e − j k z \tilde{H}(z) = \frac{1}{j \omega \mu} \hat{x} \frac{\partial}{\partial z} (-j 10 e^{-jkz}) = \hat{x} \frac{10k}{\omega \mu} e^{-jkz} H ~ ( z ) = jω μ 1 x ^ ∂ z ∂ ( − j 10 e − jk z ) = x ^ ω μ 10 k e − jk z Example 6-8 (Continued) Use H ~ ( z ) \tilde{H}(z) H ~ ( z ) in Ampère's law to find E ~ ( z ) \tilde{E}(z) E ~ ( z ) : E ~ ( z ) = 1 j ω ϵ ∇ × H ~ = 1 j ω ϵ ∣ x ^ a m p ; y ^ a m p ; z ^ ∂ ∂ x a m p ; ∂ ∂ y a m p ; ∂ ∂ z 10 k ω μ e − j k z a m p ; 0 a m p ; 0 ∣ \tilde{E}(z) = \frac{1}{j \omega \epsilon} \nabla \times \tilde{H} = \frac{1}{j \omega \epsilon} \begin{vmatrix} \hat{x} & \hat{y} & \hat{z} \ \frac{\partial}{\partial x} & \frac{\partial}{\partial y} & \frac{\partial}{\partial z} \ \frac{10k}{\omega \mu} e^{-jkz} & 0 & 0 \end{vmatrix} E ~ ( z ) = jω ϵ 1 ∇ × H ~ = jω ϵ 1 x ^ am p ; y ^ am p ; z ^ ∂ x ∂ am p ; ∂ y ∂ am p ; ∂ z ∂ ω μ 10 k e − jk z am p ; 0 am p ; 0 E ~ ( z ) = 1 j ω ϵ ( − y ^ ) ∂ ∂ z ( 10 k ω μ e − j k z ) = 1 j ω ϵ ( − y ^ ) ( 10 k ω μ ( − j k ) e − j k z ) = − y ^ j 10 k 2 ω μ ϵ e − j k z \tilde{E}(z) = \frac{1}{j \omega \epsilon} (-\hat{y}) \frac{\partial}{\partial z} (\frac{10k}{\omega \mu} e^{-jkz}) = \frac{1}{j \omega \epsilon} (-\hat{y}) (\frac{10k}{\omega \mu} (-jk) e^{-jkz}) = -\hat{y} j \frac{10 k^2}{\omega \mu \epsilon} e^{-jkz} E ~ ( z ) = jω ϵ 1 ( − y ^ ) ∂ z ∂ ( ω μ 10 k e − jk z ) = jω ϵ 1 ( − y ^ ) ( ω μ 10 k ( − jk ) e − jk z ) = − y ^ j ω μ ϵ 10 k 2 e − jk z Equating the two expressions for E ~ ( z ) \tilde{E}(z) E ~ ( z ) leads to: k 2 = ω 2 μ ϵ k^2 = \omega^2 \mu \epsilon k 2 = ω 2 μ ϵ k = ω μ ϵ = 4 ω μ < e m > 0 ϵ < / e m > 0 = 4 ω c = 4 × 10 10 3 × 10 8 = 133 ( r a d / m ) k = \omega \sqrt{\mu \epsilon} = 4 \omega \sqrt{\mu<em>0 \epsilon</em>0} = \frac{4 \omega}{c} = \frac{4 \times 10^{10}}{3 \times 10^8} = 133 (rad/m) k = ω μ ϵ = 4 ω μ < e m > 0 ϵ < / e m > 0 = c 4 ω = 3 × 1 0 8 4 × 1 0 10 = 133 ( r a d / m ) Example 6-8 (Final) H ( z , t ) = R e [ H ~ ( z ) e j ω t ] = R e [ x ^ 10 k ω μ e − j k z e j ω t ] = x ^ 10 k ω μ cos ( ω t − k z ) H(z, t) = Re[\tilde{H}(z) e^{j \omega t}] = Re[\hat{x} \frac{10k}{\omega \mu} e^{-jkz} e^{j \omega t}] = \hat{x} \frac{10k}{\omega \mu} \cos(\omega t - kz) H ( z , t ) = R e [ H ~ ( z ) e jω t ] = R e [ x ^ ω μ 10 k e − jk z e jω t ] = x ^ ω μ 10 k cos ( ω t − k z ) H ( z , t ) = x ^ 10 × 133 10 10 × 4 π × 10 − 7 cos ( 10 10 t − 133 z ) = x ^ 0.11 cos ( 10 10 t − 133 z ) ( A / m ) H(z, t) = \hat{x} \frac{10 \times 133}{10^{10} \times 4 \pi \times 10^{-7}} \cos(10^{10} t - 133z) = \hat{x} 0.11 \cos(10^{10} t - 133z) (A/m) H ( z , t ) = x ^ 1 0 10 × 4 π × 1 0 − 7 10 × 133 cos ( 1 0 10 t − 133 z ) = x ^ 0.11 cos ( 1 0 10 t − 133 z ) ( A / m ) Ulaby 6.26 Given the electric field radiated by a short dipole antenna in spherical coordinates: E ( R , θ , t ) = θ ^ 6 × 10 8 π sin ( θ ) R cos ( 2 π × 10 8 t − 2 π R ) E(R, \theta, t) = \hat{\theta} \frac{6 \times 10^8 \pi \sin(\theta)}{R} \cos(2 \pi \times 10^8 t - 2 \pi R) E ( R , θ , t ) = θ ^ R 6 × 1 0 8 π s i n ( θ ) cos ( 2 π × 1 0 8 t − 2 π R ) Find H ( R , θ , t ) H(R, \theta, t) H ( R , θ , t ) . Ulaby 6.26 Solution Radiated electric field in phasor form: E ~ ( R , θ ) = θ ^ 6 × 10 8 π sin ( θ ) R e − j 2 π R \tilde{E}(R, \theta) = \hat{\theta} \frac{6 \times 10^8 \pi \sin(\theta)}{R} e^{-j2 \pi R} E ~ ( R , θ ) = θ ^ R 6 × 1 0 8 π s i n ( θ ) e − j 2 π R ∇ × E ~ = − j ω μ H ~ \nabla \times \tilde{E} = -j \omega \mu \tilde{H} ∇ × E ~ = − jω μ H ~ H ~ = 1 − j ω μ ∇ × E ~ \tilde{H} = \frac{1}{-j \omega \mu} \nabla \times \tilde{E} H ~ = − jω μ 1 ∇ × E ~ ∇ × E ~ = 1 R [ ∂ ∂ R ( R E θ ~ ) ] ϕ ^ \nabla \times \tilde{E} = \frac{1}{R} [\frac{\partial}{\partial R} (R \tilde{E_\theta})] \hat{\phi} ∇ × E ~ = R 1 [ ∂ R ∂ ( R E θ ~ )] ϕ ^ H ~ = ϕ ^ 1 − j ω μ 1 R ∂ ∂ R ( R E θ ~ ) \tilde{H} = \hat{\phi} \frac{1}{-j \omega \mu} \frac{1}{R} \frac{\partial}{\partial R} (R \tilde{E_\theta}) H ~ = ϕ ^ − jω μ 1 R 1 ∂ R ∂ ( R E θ ~ ) H ~ = ϕ ^ 1 − j ω μ 1 R ∂ ∂ R ( 6 × 10 8 π sin ( θ ) e − j 2 π R ) \tilde{H} = \hat{\phi} \frac{1}{-j \omega \mu} \frac{1}{R} \frac{\partial}{\partial R} (6 \times 10^8 \pi \sin(\theta) e^{-j2 \pi R}) H ~ = ϕ ^ − jω μ 1 R 1 ∂ R ∂ ( 6 × 1 0 8 π sin ( θ ) e − j 2 π R ) H ~ = ϕ ^ 6 × 10 8 π sin ( θ ) ( − j 2 π ) − j ω μ R e − j 2 π R \tilde{H} = \hat{\phi} \frac{6 \times 10^8 \pi \sin(\theta) (-j2 \pi)}{-j \omega \mu R} e^{-j2 \pi R} H ~ = ϕ ^ − jω μ R 6 × 1 0 8 π s i n ( θ ) ( − j 2 π ) e − j 2 π R H ~ = ϕ ^ 12 π 2 × 10 8 s i n ( θ ) ω μ R e − j 2 π R \tilde{H} = \hat{\phi} \frac{12 \pi^2 \times 10^8 sin(\theta)}{\omega \mu R} e^{-j2 \pi R} H ~ = ϕ ^ ω μ R 12 π 2 × 1 0 8 s in ( θ ) e − j 2 π R H ~ = ϕ ^ 12 π 2 × 10 8 sin ( θ ) 2 π × 10 8 × 4 π × 10 − 7 R e − j 2 π R = 1.53 sin ( θ ) R e − j 2 π R \tilde{H} = \hat{\phi} \frac{12 \pi^2 \times 10^8 \sin(\theta)}{2 \pi \times 10^8 \times 4 \pi \times 10^{-7} R} e^{-j2\pi R} =\frac{1.53 \sin(\theta)}{R} e^{- j2 \pi R} H ~ = ϕ ^ 2 π × 1 0 8 × 4 π × 1 0 − 7 R 12 π 2 × 1 0 8 s i n ( θ ) e − j 2 π R = R 1.53 s i n ( θ ) e − j 2 π R Ulaby 6.26 Solution(continued) H ( R , θ , t ) = R e [ H ~ ( R , θ ) e j ω t ] H(R,\theta,t) = Re[ \tilde{H}(R,\theta)e^{j \omega t}] H ( R , θ , t ) = R e [ H ~ ( R , θ ) e jω t ] H ( R , θ , t ) = ϕ ^ 1.53 sin ( θ ) R R e [ e − j 2 π R e j 2 π × 10 8 t ] H(R,\theta,t) = \hat{\phi} \frac{1.53 \sin(\theta)}{R} Re[ e^{- j2\pi R} e^{j 2\pi \times 10^8 t} ] H ( R , θ , t ) = ϕ ^ R 1.53 s i n ( θ ) R e [ e − j 2 π R e j 2 π × 1 0 8 t ] H ( R , θ , t ) = ϕ ^ 1.53 sin ( θ ) R c o s ( 2 π × 10 8 t − 2 π R ) H(R,\theta,t) = \hat{\phi} \frac{1.53 \sin(\theta)}{R} cos( 2\pi \times 10^8 t - 2\pi R ) H ( R , θ , t ) = ϕ ^ R 1.53 s i n ( θ ) cos ( 2 π × 1 0 8 t − 2 π R ) 2015 Test 2 Question 3 ∇ × E ~ = − j ω μ H ~ \nabla \times \tilde{E} = - j \omega \mu \tilde{H} ∇ × E ~ = − jω μ H ~ ∇ × H ~ = J ~ + j ω D ~ \nabla \times \tilde{H} = \tilde{J} + j \omega \tilde{D} ∇ × H ~ = J ~ + jω D ~ 2015 Test 2 Question 3(Continued) E ~ ( z ) = [ 40 x ^ − j 40 y ^ ] e − j 10 π z \tilde{E}(z) = [40 \hat{x} - j 40 \hat{y}] e^{-j10 \pi z} E ~ ( z ) = [ 40 x ^ − j 40 y ^ ] e − j 10 π z H ~ = 1 − j ω μ ∇ × E ~ \tilde{H} = \frac{1}{- j \omega \mu } \nabla \times \tilde{E} H ~ = − jω μ 1 ∇ × E ~ ∇ × E ~ = [ x ^ a m p ; y ^ a m p ; z ^ ∂ ∂ x a m p ; ∂ ∂ y a m p ; ∂ ∂ z 40 e − j 10 π z a m p ; − j 40 e − j 10 π z a m p ; 0 ] \nabla \times \tilde{E} = \begin{bmatrix} \hat{x} & \hat{y} & \hat{z} \ \frac{\partial}{\partial x} & \frac{\partial}{\partial y} & \frac{\partial}{\partial z} \ 40 e^{-j10 \pi z} & -j40 e^{-j10 \pi z} & 0 \end{bmatrix} ∇ × E ~ = [ x ^ am p ; y ^ am p ; z ^ ∂ x ∂ am p ; ∂ y ∂ am p ; ∂ z ∂ 40 e − j 10 π z am p ; − j 40 e − j 10 π z am p ; 0 ] ∇ × E ~ = x ^ [ ∂ ∂ z ( − j 40 e − j 10 π z ) ] − y ^ [ ∂ ∂ z ( 40 e − j 10 π z ) ] \nabla \times \tilde{E} = \hat{x} [ \frac{\partial}{\partial z} ( - j 40 e^{- j10 \pi z}) ] - \hat{y} [ \frac{\partial}{\partial z} ( 40 e^{- j10 \pi z}) ] ∇ × E ~ = x ^ [ ∂ z ∂ ( − j 40 e − j 10 π z )] − y ^ [ ∂ z ∂ ( 40 e − j 10 π z )] ∇ × E ~ = 400 π e − j 10 π z x ^ + j 400 π e − j 10 π z y ^ \nabla \times \tilde{E} = 400 \pi e^{- j10 \pi z} \hat{x} + j 400 \pi e^{-j10 \pi z} \hat{y} ∇ × E ~ = 400 π e − j 10 π z x ^ + j 400 π e − j 10 π z y ^ 2015 Test 2 Question 3(Continued) H ~ = 1 − j ω μ ∇ × E ~ = 1 − j ω μ [ 400 π e − j 10 π z x ^ + j 400 π e − j 10 π z y ^ ] \tilde{H} = \frac{1}{- j \omega \mu} \nabla \times \tilde{E} = \frac{1}{- j \omega \mu } [ 400 \pi e^{- j10 \pi z} \hat{x} + j 400 \pi e^{- j10 \pi z} \hat{y}] H ~ = − jω μ 1 ∇ × E ~ = − jω μ 1 [ 400 π e − j 10 π z x ^ + j 400 π e − j 10 π z y ^ ] H ~ = 400 π ω μ [ j e − j 10 π z x ^ + e − j 10 π z y ^ ] \tilde{H} = \frac{400 \pi }{ \omega \mu } [ j e^{- j10 \pi z} \hat{x} + e^{- j10 \pi z} \hat{y} ] H ~ = ω μ 400 π [ j e − j 10 π z x ^ + e − j 10 π z y ^ ] H ~ = x ^ 400 π 8 π × 10 7 j e − j 10 π z + y ^ 400 π 8 π × 10 7 e − j 10 π z = x ^ R e [ 5 × 10 − 6 j e − j 10 π z + j ω t ] + y ^ R e [ 5 × 10 − 6 e − j 10 π z + j ω t ] \tilde{H} = \hat{x} \frac{400 \pi }{ 8 \pi \times 10^7 } j e^{- j10 \pi z} + \hat{y} \frac{400 \pi }{ 8 \pi \times 10^7 } e^{- j10 \pi z} = \hat{x} Re[ 5 \times 10^{-6} j e^{-j10 \pi z + j \omega t} ] + \hat{y}Re[ 5 \times 10^{-6} e^{-j10 \pi z + j \omega t} ] H ~ = x ^ 8 π × 1 0 7 400 π j e − j 10 π z + y ^ 8 π × 1 0 7 400 π e − j 10 π z = x ^ R e [ 5 × 1 0 − 6 j e − j 10 π z + jω t ] + y ^ R e [ 5 × 1 0 − 6 e − j 10 π z + jω t ] H = x ^ 5 × 10 − 6 s i n ( ω t − 10 π z ) + y ^ 5 × 10 − 6 c o s ( ω t − 10 π z ) H = \hat{x} 5 \times 10^{-6} sin( \omega t -10 \pi z) + \hat{y} 5 \times 10^{-6}cos( \omega t - 10 \pi z) H = x ^ 5 × 1 0 − 6 s in ( ω t − 10 π z ) + y ^ 5 × 1 0 − 6 cos ( ω t − 10 π z ) Given μ = 4 π × 10 − 7 \mu = 4 \pi \times 10^{-7} μ = 4 π × 1 0 − 7 therefore ω μ = 8 π × 10 7 \omega \mu = 8 \pi \times 10^7 ω μ = 8 π × 1 0 7 2015 Test 2 Question 3(Continued) E ~ ( z ) = 40 x ^ e − j 10 π z \tilde{E}(z) = 40 \hat{x} e^{-j10 \pi z} E ~ ( z ) = 40 x ^ e − j 10 π z Assuming displacement current J ~ = j ω ϵ E ~ = j 8 π × 10 7 ( 10 − 10 / ( 36 π ) ) ( 40 e − j 10 π z x ^ ) \tilde{J} = j \omega \epsilon \tilde{E} = j 8 \pi \times 10^7 ( 10^{-10} / (36 \pi)) (40 e^{-j10 \pi z} \hat{x} ) J ~ = jω ϵ E ~ = j 8 π × 1 0 7 ( 1 0 − 10 / ( 36 π )) ( 40 e − j 10 π z x ^ ) J ~ = j 0.089 x ^ e − j 10 π z \tilde{J} = j 0.089 \hat{x} e^{-j10 \pi z} J ~ = j 0.089 x ^ e − j 10 π z ω ϵ = 8 π × 10 7 ( 10 − 9 / 36 π ) = j 0.698 \omega \epsilon = 8 \pi \times 10^7 ( 10^{-9} / 36 \pi ) = j 0.698 ω ϵ = 8 π × 1 0 7 ( 1 0 − 9 /36 π ) = j 0.698 u p = ω k = 1 u_p = {\omega \over k } = 1 u p = k ω = 1