Wave Polarization and Electromagnetic Waves Wave Polarization Instantaneous Distribution The instantaneous distribution equations are given as:
Electric field: E ( z ) = E < e m > 0 e − j k z + E < / e m > 0 e + j k z E(z) = E<em>0 e^{-jkz} + E</em>0 e^{+jkz} E ( z ) = E < e m > 0 e − jk z + E < / e m > 0 e + jk z Magnetic field: H = E η H = \frac{E}{\eta} H = η E Wave Polarization A plane wave propagates along the +z direction. A separate definition for H is not necessary. E is linearly polarized (vertical). Describes the locus traced by the tip of the E vector. The vector is in the plane orthogonal to the direction of propagation. It is a function of time at a given point in space. Plane wave propagating along +z:E ~ ( z ) = x ^ E ~ < e m > x ( z ) + y ^ E ~ < / e m > y ( z ) \tilde{E}(z) = \hat{x}\tilde{E}<em>x(z) + \hat{y}\tilde{E}</em>y(z) E ~ ( z ) = x ^ E ~ < e m > x ( z ) + y ^ E ~ < / e m > y ( z ) E < e m > x ( z ) = E < / e m > x o e − j k z E<em>x(z) = E</em>{xo}e^{-jkz} E < e m > x ( z ) = E < / e m > x o e − jk z E < e m > y ( z ) = E < / e m > y o e − j k z E<em>y(z) = E</em>{yo}e^{-jkz} E < e m > y ( z ) = E < / e m > yo e − jk z E < e m > x o = a < / e m > x E<em>{xo} = a</em>x E < e m > x o = a < / e m > x E < e m > y o = a < / e m > y e j δ E<em>{yo} = a</em>y e^{j\delta} E < e m > yo = a < / e m > y e j δ E ~ ( z ) = ( x ^ a < e m > x + y ^ a < / e m > y e j δ ) e − j k z \tilde{E}(z) = (\hat{x}a<em>x + \hat{y}a</em>y e^{j\delta})e^{-jkz} E ~ ( z ) = ( x ^ a < e m > x + y ^ a < / e m > y e j δ ) e − jk z E ( z , t ) = R e [ E ~ ( z ) e j ω t ] E(z, t) = Re[\tilde{E}(z)e^{j\omega t}] E ( z , t ) = R e [ E ~ ( z ) e jω t ] = x ^ a < e m > x cos ( ω t − k z ) + y ^ a < / e m > y cos ( ω t − k z + δ ) = \hat{x}a<em>x \cos(\omega t - kz) + \hat{y}a</em>y \cos(\omega t - kz + \delta) = x ^ a < e m > x cos ( ω t − k z ) + y ^ a < / e m > y cos ( ω t − k z + δ ) Polarization State Describes the trace of E as a function of time at a fixed z. Includes magnitude of E and inclination angle. Linear Polarization δ = 0 \delta = 0 δ = 0 or δ = π \delta = \pi δ = π A wave is linearly polarized if, for a fixed z, the tip of E ( z , t ) E(z, t) E ( z , t ) traces a straight line segment as a function of time. This happens when E < e m > x ( z , t ) E<em>x(z, t) E < e m > x ( z , t ) and E < / e m > y ( z , t ) E</em>y(z, t) E < / e m > y ( z , t ) are in-phase (δ = 0 \delta = 0 δ = 0 ) or out-of-phase (δ = π \delta = \pi δ = π ). Under these conditions, the equation simplifies to:E ( z , t ) = R e [ E ~ ( z ) e j ω t ] = x ^ a < e m > x cos ( ω t − k z ) + y ^ a < / e m > y cos ( ω t − k z + δ ) E(z, t) = Re[\tilde{E}(z)e^{j\omega t}] = \hat{x}a<em>x \cos(\omega t - kz) + \hat{y}a</em>y \cos(\omega t - kz + \delta) E ( z , t ) = R e [ E ~ ( z ) e jω t ] = x ^ a < e m > x cos ( ω t − k z ) + y ^ a < / e m > y cos ( ω t − k z + δ ) In-phase:δ = 0 \delta = 0 δ = 0 E ( 0 , t ) = ( x ^ a < e m > x + y ^ a < / e m > y ) cos ( ω t − k z ) E(0, t) = (\hat{x}a<em>x + \hat{y}a</em>y)\cos(\omega t - kz) E ( 0 , t ) = ( x ^ a < e m > x + y ^ a < / e m > y ) cos ( ω t − k z ) Out-of-phase:δ = π \delta = \pi δ = π E ( 0 , t ) = ( x ^ a < e m > x − y ^ a < / e m > y ) cos ( ω t − k z ) E(0, t) = (\hat{x}a<em>x - \hat{y}a</em>y)\cos(\omega t - kz) E ( 0 , t ) = ( x ^ a < e m > x − y ^ a < / e m > y ) cos ( ω t − k z ) The field's magnitude is:∣ E ( z , t ) ∣ = [ a < e m > x 2 + a < / e m > y 2 ] 1 / 2 ∣ cos ( ω t − k z ) ∣ |E(z, t)| = [a<em>x^2 + a</em>y^2]^{1/2} |\cos(\omega t - kz)| ∣ E ( z , t ) ∣ = [ a < e m > x 2 + a < / e m > y 2 ] 1/2 ∣ cos ( ω t − k z ) ∣ The inclination angle is:ψ = tan − 1 ( E < e m > y E < / e m > x ) = tan − 1 ( ∓ a < e m > y a < / e m > x ) \psi = \tan^{-1}(\frac{E<em>y}{E</em>x}) = \tan^{-1}(\mp \frac{a<em>y}{a</em>x}) ψ = tan − 1 ( E < / e m > x E < e m > y ) = tan − 1 ( ∓ a < / e m > x a < e m > y ) (out-of-phase). If a y = 0 a_y = 0 a y = 0 , then ψ = 0 \psi = 0 ψ = 0 ° or 180°, and the wave is x-polarized. Conversely, if a x = 0 a_x = 0 a x = 0 , then ψ = 90 \psi = 90 ψ = 90 ° or -90°, and the wave is y-polarized. Linear Polarization cases a < e m > x = a < / e m > y a<em>x = a</em>y a < e m > x = a < / e m > y ψ = − 45 \psi = -45 ψ = − 45 °Circular Polarization a < e m > x = a < / e m > y = a a<em>x = a</em>y = a a < e m > x = a < / e m > y = a and δ = π / 2 \delta = \pi/2 δ = π /2 a < e m > x = a < / e m > y = a a<em>x = a</em>y = a a < e m > x = a < / e m > y = a and δ = − π / 2 \delta = -\pi/2 δ = − π /2 For a < e m > x = a < / e m > y = a a<em>x = a</em>y = a a < e m > x = a < / e m > y = a and δ = π / 2 \delta = \pi/2 δ = π /2 , the equations become:E ~ ( z ) = ( x ^ a + y ^ a e j π / 2 ) e − j k z = a ( x ^ + j y ^ ) e − j k z \tilde{E}(z) = (\hat{x}a + \hat{y}ae^{j\pi/2})e^{-jkz} = a(\hat{x} + j\hat{y})e^{-jkz} E ~ ( z ) = ( x ^ a + y ^ a e jπ /2 ) e − jk z = a ( x ^ + j y ^ ) e − jk z E ( z , t ) = R e [ E ~ ( z ) e j ω t ] = x ^ a cos ( ω t − k z ) + y ^ a cos ( ω t − k z + π / 2 ) = x ^ a cos ( ω t − k z ) − y ^ a sin ( ω t − k z ) E(z, t) = Re[\tilde{E}(z)e^{j\omega t}] = \hat{x}a\cos(\omega t - kz) + \hat{y}a\cos(\omega t - kz + \pi/2) = \hat{x}a\cos(\omega t - kz) - \hat{y}a\sin(\omega t - kz) E ( z , t ) = R e [ E ~ ( z ) e jω t ] = x ^ a cos ( ω t − k z ) + y ^ a cos ( ω t − k z + π /2 ) = x ^ a cos ( ω t − k z ) − y ^ a sin ( ω t − k z ) Circular Polarization cont. a < e m > x = a < / e m > y = a a<em>x = a</em>y = a a < e m > x = a < / e m > y = a and δ = π / 2 \delta = \pi/2 δ = π /2 The corresponding field magnitude and inclination angle are:∣ E ( z , t ) ∣ = [ E < e m > x 2 ( z , t ) + E < / e m > y 2 ( z , t ) ] 1 / 2 = [ a 2 cos 2 ( ω t − k z ) + a 2 sin 2 ( ω t − k z ) ] 1 / 2 = a |E(z, t)| = [E<em>x^2(z, t) + E</em>y^2(z, t)]^{1/2} = [a^2 \cos^2(\omega t - kz) + a^2 \sin^2(\omega t - kz)]^{1/2} = a ∣ E ( z , t ) ∣ = [ E < e m > x 2 ( z , t ) + E < / e m > y 2 ( z , t ) ] 1/2 = [ a 2 cos 2 ( ω t − k z ) + a 2 sin 2 ( ω t − k z ) ] 1/2 = a ψ ( z , t ) = tan − 1 ( E < e m > y ( z , t ) E < / e m > x ( z , t ) ) = tan − 1 ( − a sin ( ω t − k z ) a cos ( ω t − k z ) ) = − ( ω t − k z ) \psi(z, t) = \tan^{-1}(\frac{E<em>y(z, t)}{E</em>x(z, t)}) = \tan^{-1}(\frac{-a\sin(\omega t - kz)}{a\cos(\omega t - kz)}) = -(\omega t - kz) ψ ( z , t ) = tan − 1 ( E < / e m > x ( z , t ) E < e m > y ( z , t ) ) = tan − 1 ( a c o s ( ω t − k z ) − a s i n ( ω t − k z ) ) = − ( ω t − k z ) a < e m > x = a < / e m > y = a a<em>x = a</em>y = a a < e m > x = a < / e m > y = a and δ = − π / 2 \delta = -\pi/2 δ = − π /2 ∣ E ( z , t ) ∣ = a , ψ = ( ω t − k z ) |E(z, t)| = a, \quad \psi = (\omega t - kz) ∣ E ( z , t ) ∣ = a , ψ = ( ω t − k z ) Circular Polarization Visuals For a Left Hand Circular Polarized (LHCP) wave:E ( z , t ) = x ^ E < e m > o cos ( ω t − k z ) − y ^ E < / e m > o sin ( ω t − k z ) E(z,t) = \hat{x}E<em>o \cos(\omega t - kz) - \hat{y}E</em>o \sin(\omega t - kz) E ( z , t ) = x ^ E < e m > o cos ( ω t − k z ) − y ^ E < / e m > o sin ( ω t − k z ) For a Right Hand Circular Polarized (RHCP) wave:E ( z , t ) = x ^ E < e m > o cos ( ω t − k z ) + y ^ E < / e m > o sin ( ω t − k z ) E(z,t) = \hat{x}E<em>o \cos(\omega t - kz) + \hat{y}E</em>o \sin(\omega t - kz) E ( z , t ) = x ^ E < e m > o cos ( ω t − k z ) + y ^ E < / e m > o sin ( ω t − k z ) LHCP and RHCP Illustrations of LHCP and RHCP waves at different times. Elliptical Polarization: General Case When a < e m > x ≠ a < / e m > y a<em>x \neq a</em>y a < e m > x = a < / e m > y , or the phase shift is not exactly π / 2 \pi/2 π /2 tan 2 ψ = ( tan 2 α 0 ) cos δ \tan 2\psi = (\tan 2\alpha_0) \cos \delta tan 2 ψ = ( tan 2 α 0 ) cos δ sin 2 χ = ( sin 2 α 0 ) sin δ \sin 2\chi = (\sin 2\alpha_0) \sin \delta sin 2 χ = ( sin 2 α 0 ) sin δ ( − π / 2 ≤ ψ ≤ π / 2 ) (-\pi/2 \le \psi \le \pi/2) ( − π /2 ≤ ψ ≤ π /2 ) ( − π / 4 ≤ χ ≤ π / 4 ) (-\pi/4 \le \chi \le \pi/4) ( − π /4 ≤ χ ≤ π /4 ) where α < e m > 0 \alpha<em>0 α < e m > 0 is an auxiliary angle defined by tan α < / e m > 0 = a < e m > y a < / e m > x ( 0 ≤ α 0 ≤ π 2 ) \tan \alpha</em>0 = \frac{a<em>y}{a</em>x} \quad (0 \le \alpha_0 \le \frac{\pi}{2}) tan α < / e m > 0 = a < / e m > x a < e m > y ( 0 ≤ α 0 ≤ 2 π ) \psi > 0 if \cos \delta > 0 \psi < 0 if \cos \delta < 0 The polarization ellipse may be tilted. Linear and Circular Polarization as Special Cases of Elliptical Polarization Axial Ratio (AR): AR = major axis minor axis \text{AR} = \frac{\text{major axis}}{\text{minor axis}} AR = minor axis major axis 1 ≤ AR ≤ ∞ 1 \le \text{AR} \le \infty 1 ≤ AR ≤ ∞ Example 7-2: RHC Polarized Wave An RHC polarized plane wave with an electric field magnitude of 3 (mV/m) is traveling in the +y-direction in a dielectric medium with ε = 4 ε < e m > 0 \varepsilon = 4\varepsilon<em>0 ε = 4 ε < e m > 0 , μ = μ < / e m > 0 \mu = \mu</em>0 μ = μ < / e m > 0 , and σ = 0 \sigma = 0 σ = 0 . If the frequency is 100 MHz, obtain expressions for E ( y , t ) E(y, t) E ( y , t ) and H ( y , t ) H(y, t) H ( y , t ) . Since the wave is traveling in the +y-direction, its field must have components along the x- and z-directions. By comparison with the RHC polarized wave, we assign the z-component of E ~ ( y ) \tilde{E}(y) E ~ ( y ) a phase angle of zero and the x-component a phase shift of δ = − π / 2 \delta = -\pi/2 δ = − π /2 . E ~ ( y ) = x ^ E ~ < e m > x + z ^ E ~ < / e m > z \tilde{E}(y) = \hat{x}\tilde{E}<em>x + \hat{z}\tilde{E}</em>z E ~ ( y ) = x ^ E ~ < e m > x + z ^ E ~ < / e m > z Example 7-2 cont. ω = 2 π f = 2 π × 10 8 (rad/s) \omega = 2\pi f = 2\pi \times 10^8 \text{ (rad/s)} ω = 2 π f = 2 π × 1 0 8 (rad/s) k = ω c ε r = 2 π × 10 8 4 3 × 10 8 = 4 π 3 (rad/m) k = \frac{\omega}{c} \sqrt{\varepsilon_r} = \frac{2\pi \times 10^8 \sqrt{4}}{3 \times 10^8} = \frac{4\pi}{3} \text{ (rad/m)} k = c ω ε r = 3 × 1 0 8 2 π × 1 0 8 4 = 3 4 π (rad/m) E ~ ( y ) = x ^ a e − j π / 2 e − j k y + z ^ a e − j k y = ( − x ^ j + z ^ ) 3 e − j k y (mV/m) \tilde{E}(y) = \hat{x}ae^{-j\pi/2}e^{-jky} + \hat{z}ae^{-jky} = (-\hat{x}j + \hat{z})3e^{-jky} \text{ (mV/m)} E ~ ( y ) = x ^ a e − jπ /2 e − jk y + z ^ a e − jk y = ( − x ^ j + z ^ ) 3 e − jk y (mV/m) H ~ ( y ) = 1 η y ^ × E ~ ( y ) = 1 η y ^ × ( − x ^ j + z ^ ) 3 e − j k y = 3 η ( − z ^ j − x ^ ) e − j k y (mA/m) \tilde{H}(y) = \frac{1}{\eta} \hat{y} \times \tilde{E}(y) = \frac{1}{\eta} \hat{y} \times (-\hat{x}j + \hat{z})3e^{-jky} = \frac{3}{\eta} (-\hat{z}j - \hat{x})e^{-jky} \text{ (mA/m)} H ~ ( y ) = η 1 y ^ × E ~ ( y ) = η 1 y ^ × ( − x ^ j + z ^ ) 3 e − jk y = η 3 ( − z ^ j − x ^ ) e − jk y (mA/m) Example 7-2 cont.. \eta = \frac{\eta0}{\sqrt{\varepsilon r}} = \frac{120\pi}{\sqrt{4}} = 60\pi \text{ (\Omega)} The instantaneous fields E ( y , t ) E(y, t) E ( y , t ) and H ( y , t ) H(y, t) H ( y , t ) are:E ( y , t ) = R e [ E ~ ( y ) e j ω t ] = R e [ ( − x ^ j + z ^ ) 3 e − j k y e j ω t ] = 3 [ x ^ sin ( ω t − k y ) + z ^ cos ( ω t − k y ) ] (mV/m) E(y, t) = Re[\tilde{E}(y)e^{j\omega t}] = Re[(-\hat{x}j + \hat{z})3e^{-jky}e^{j\omega t}] = 3[\hat{x}\sin(\omega t - ky) + \hat{z}\cos(\omega t - ky)] \text{ (mV/m)} E ( y , t ) = R e [ E ~ ( y ) e jω t ] = R e [( − x ^ j + z ^ ) 3 e − jk y e jω t ] = 3 [ x ^ sin ( ω t − k y ) + z ^ cos ( ω t − k y )] (mV/m) H ( y , t ) = R e [ H ~ ( y ) e j ω t ] = R e [ 3 η ( − z ^ j − x ^ ) e − j k y e j ω t ] = 1 20 π [ x ^ cos ( ω t − k y ) − z ^ sin ( ω t − k y ) ] (mA/m) H(y, t) = Re[\tilde{H}(y)e^{j\omega t}] = Re[\frac{3}{\eta} (-\hat{z}j - \hat{x})e^{-jky}e^{j\omega t}] = \frac{1}{20\pi} [\hat{x}\cos(\omega t - ky) - \hat{z}\sin(\omega t - ky)] \text{ (mA/m)} H ( y , t ) = R e [ H ~ ( y ) e jω t ] = R e [ η 3 ( − z ^ j − x ^ ) e − jk y e jω t ] = 20 π 1 [ x ^ cos ( ω t − k y ) − z ^ sin ( ω t − k y )] (mA/m) 2017 Exam Q5 Given values:f = 10 8 Hz f = 10^8 \text{ Hz} f = 1 0 8 Hz ϵ r = 2.25 \epsilon_r = 2.25 ϵ r = 2.25 μ r = 1 \mu_r = 1 μ r = 1 E o = 0.1 E_o = 0.1 E o = 0.1 Calculations:ω = 2 π f = 2 π × 10 8 \omega = 2\pi f = 2\pi \times 10^8 ω = 2 π f = 2 π × 1 0 8 k = ω μ ϵ = 2 π × 10 8 μ < e m > o ϵ < / e m > o ϵ r = 2 π × 10 8 c 2.25 = 2 π × 10 8 3 × 10 8 1.5 = π k = \omega \sqrt{\mu \epsilon} = 2\pi \times 10^8 \sqrt{\mu<em>o \epsilon</em>o \epsilon_r} = \frac{2\pi \times 10^8}{c} \sqrt{2.25} = \frac{2\pi \times 10^8}{3 \times 10^8} 1.5 = \pi k = ω μ ϵ = 2 π × 1 0 8 μ < e m > oϵ < / e m > o ϵ r = c 2 π × 1 0 8 2.25 = 3 × 1 0 8 2 π × 1 0 8 1.5 = π η = μ ϵ = μ < e m > o ϵ < / e m > o ϵ r = 120 π 2.25 = 120 π 1.5 = 80 π \eta = \sqrt{\frac{\mu}{\epsilon}} = \sqrt{\frac{\mu<em>o}{\epsilon</em>o \epsilon_r}} = \frac{120\pi}{\sqrt{2.25}} = \frac{120\pi}{1.5} = 80\pi η = ϵ μ = ϵ < / e m > o ϵ r μ < e m > o = 2.25 120 π = 1.5 120 π = 80 π E ~ ( z , t ) = x ^ E o e − j k z = x ^ 0.1 e − j π z \tilde{E}(z, t) = \hat{x} E_o e^{-jkz} = \hat{x} 0.1 e^{-j\pi z} E ~ ( z , t ) = x ^ E o e − jk z = x ^ 0.1 e − jπ z E ( t , z ) = x ^ cos ( 2 × 10 8 t − π z ) E(t, z) = \hat{x} \cos(2 \times 10^8 t - \pi z) E ( t , z ) = x ^ cos ( 2 × 1 0 8 t − π z ) Linear polarization - Horizontal 2017 Exam Q5 - Linear Polarization Linear polarization condition: a y = 0 a_y = 0 a y = 0 Given: a < e m > x = a ; a < / e m > y = 0 a<em>x = a; a</em>y = 0 a < e m > x = a ; a < / e m > y = 0 δ = 0 \delta = 0 δ = 0 ψ = tan − 1 ( E < e m > y E < / e m > x ) = 0 \psi = \tan^{-1}(\frac{E<em>y}{E</em>x}) = 0 ψ = tan − 1 ( E < / e m > x E < e m > y ) = 0 2013 Tut 1 Q2 Given:a x = 30 a_x = 30 a x = 30 a y = 30 a_y = 30 a y = 30 δ = − π 6 = − 30 \delta = -\frac{\pi}{6} = -30 δ = − 6 π = − 30 ° Calculations:ψ = tan − 1 ( E < e m > y E < / e m > x ) = tan − 1 ( a < e m > y a < / e m > x ) = tan − 1 ( − 30 30 ) = − π 6 \psi = \tan^{-1}(\frac{E<em>y}{E</em>x}) = \tan^{-1}(\frac{a<em>y}{a</em>x}) = \tan^{-1}(-\frac{30}{30}) = -\frac{\pi}{6} ψ = tan − 1 ( E < / e m > x E < e m > y ) = tan − 1 ( a < / e m > x a < e m > y ) = tan − 1 ( − 30 30 ) = − 6 π E ( z , t ) = x ^ 30 cos ( ω t ) + y ^ 30 sin ( ω t − π 6 ) E(z, t) = \hat{x}30\cos(\omega t) + \hat{y}30\sin(\omega t - \frac{\pi}{6}) E ( z , t ) = x ^ 30 cos ( ω t ) + y ^ 30 sin ( ω t − 6 π ) E ~ = x ^ 30 − j y ^ 6 \tilde{E} = \hat{x}30 - j\hat{y}6 E ~ = x ^ 30 − j y ^ 6 2013 Tut 1 Q2 - RHCP Given: a < e m > x = 30 ; a < / e m > y = 30 a<em>x = 30; a</em>y = 30 a < e m > x = 30 ; a < / e m > y = 30 E ( 0 , t ) = x ^ 30 cos ( ω t ) + y ^ 30 sin ( ω t ) E(0,t) = \hat{x}30\cos(\omega t) + \hat{y}30\sin(\omega t) E ( 0 , t ) = x ^ 30 cos ( ω t ) + y ^ 30 sin ( ω t ) E ~ = x ^ 30 − j y ^ 6 \tilde{E} = \hat{x}30 - j\hat{y}6 E ~ = x ^ 30 − j y ^ 6 2013 Test 1 Q2 - Linear Polarization Linear polarization at 45° Given: a < e m > θ = a < / e m > ϕ = E o 2 a<em>{\theta} = a</em>{\phi} = \frac{E_o}{\sqrt{2}} a < e m > θ = a < / e m > ϕ = 2 E o δ = 0 \delta = 0 δ = 0 E ( R , t ) = θ ^ E < e m > θ cos ( ω t − k R + ϕ < / e m > θ ) + ϕ ^ E < e m > ϕ cos ( ω t − k R + ϕ < / e m > ϕ ) E(R, t) = \hat{\theta}E<em>{\theta} \cos(\omega t - kR + \phi</em>{\theta}) + \hat{\phi}E<em>{\phi} \cos(\omega t - kR + \phi</em>{\phi}) E ( R , t ) = θ ^ E < e m > θ cos ( ω t − k R + ϕ < / e m > θ ) + ϕ ^ E < e m > ϕ cos ( ω t − k R + ϕ < / e m > ϕ ) ψ = tan − 1 ( E < e m > ϕ E < / e m > θ ) \psi = \tan^{-1}(\frac{E<em>{\phi}}{E</em>{\theta}}) ψ = tan − 1 ( E < / e m > θ E < e m > ϕ ) E ~ ( z ) = θ ^ + ϕ ^ \tilde{E}(z) = \hat{\theta} + \hat{\phi} E ~ ( z ) = θ ^ + ϕ ^ 2016 Exam Q5 Given:a x = 10 a_x = 10 a x = 10 a y = 10 a_y = 10 a y = 10 δ = π 2 \delta = \frac{\pi}{2} δ = 2 π Calculations:ψ = tan − 1 ( E < e m > y E < / e m > x ) \psi = \tan^{-1}(\frac{E<em>y}{E</em>x}) ψ = tan − 1 ( E < / e m > x E < e m > y ) E ( z , t ) = − x ^ 10 cos ( ω t + k z ) − y ^ 10 sin ( ω t + k z ) E(z,t) = -\hat{x}10\cos(\omega t + kz) - \hat{y}10\sin(\omega t + kz) E ( z , t ) = − x ^ 10 cos ( ω t + k z ) − y ^ 10 sin ( ω t + k z ) 2016 Exam Q5 - Left Hand Circular E ( z , t ) = − x ^ 10 cos ( ω t + k z ) − y ^ 10 sin ( ω t + k z ) E(z,t) = -\hat{x}10\cos(\omega t + kz) - \hat{y}10\sin(\omega t + kz) E ( z , t ) = − x ^ 10 cos ( ω t + k z ) − y ^ 10 sin ( ω t + k z ) k ^ = − z ^ \hat{k} = -\hat{z} k ^ = − z ^ For a uniform plane wave with electric field E ~ = x ^ E x ( z ) \tilde{E} = \hat{x}E_x(z) E ~ = x ^ E x ( z ) traveling along the z-direction, the wave equation reduces to:d 2 E < e m > x ( z ) d z 2 − γ 2 E < / e m > x ( z ) = 0 \frac{d^2 E<em>x(z)}{dz^2} - \gamma^2 E</em>x(z) = 0 d z 2 d 2 E < e m > x ( z ) − γ 2 E < / e m > x ( z ) = 0 where γ 2 = − ω 2 μ ϵ c = − ω 2 μ ( ϵ ′ − j ϵ ′ ′ ) \gamma^2 = -\omega^2 \mu \epsilon_c = -\omega^2 \mu (\epsilon' - j\epsilon'') γ 2 = − ω 2 μ ϵ c = − ω 2 μ ( ϵ ′ − j ϵ ′′ ) ϵ ′ ′ = σ ω \epsilon'' = \frac{\sigma}{\omega} ϵ ′′ = ω σ Since γ \gamma γ is complex, we express it as γ = α + j β \gamma = \alpha + j\beta γ = α + j β , where α \alpha α is the attenuation constant and β \beta β is the phase constant. Replacing γ \gamma γ with ( α + j β ) (\alpha + j\beta) ( α + j β ) , we obtain α 2 − β 2 + j 2 α β = − ω 2 μ ϵ ′ + j ω 2 μ ϵ ′ ′ \alpha^2 - \beta^2 + j2\alpha\beta = -\omega^2 \mu \epsilon' + j\omega^2 \mu \epsilon'' α 2 − β 2 + j 2 α β = − ω 2 μ ϵ ′ + j ω 2 μ ϵ ′′ Complex algebra requires the real and imaginary parts on one side of an equation to equal the real and imaginary parts on the other side. Hence:α 2 − β 2 = − ω 2 μ ϵ ′ \alpha^2 - \beta^2 = -\omega^2 \mu \epsilon' α 2 − β 2 = − ω 2 μ ϵ ′ 2 α β = ω 2 μ ϵ ′ ′ 2\alpha\beta = \omega^2 \mu \epsilon'' 2 α β = ω 2 μ ϵ ′′ Solving these two equations for α \alpha α and β \beta β gives:α = ω μ ϵ ′ 2 [ 1 + ( ϵ ′ ′ ϵ ′ ) 2 − 1 ] 1 / 2 (Np/m) \alpha = \omega \sqrt{\frac{\mu \epsilon'}{2}} \left[ \sqrt{1 + (\frac{\epsilon''}{\epsilon'})^2} - 1 \right]^{1/2} \text{ (Np/m)} α = ω 2 μ ϵ ′ [ 1 + ( ϵ ′ ϵ ′′ ) 2 − 1 ] 1/2 (Np/m) β = ω μ ϵ ′ 2 [ 1 + ( ϵ ′ ′ ϵ ′ ) 2 + 1 ] 1 / 2 (rad/m) \beta = \omega \sqrt{\frac{\mu \epsilon'}{2}} \left[ \sqrt{1 + (\frac{\epsilon''}{\epsilon'})^2} + 1 \right]^{1/2} \text{ (rad/m)} β = ω 2 μ ϵ ′ [ 1 + ( ϵ ′ ϵ ′′ ) 2 + 1 ] 1/2 (rad/m) Attenuation of E and H Fields E ~ ( z ) = x ^ E ~ < e m > x ( z ) = x ^ E < / e m > x 0 e − γ z = x ^ E x 0 e − α z e − j β z \tilde{E}(z) = \hat{x} \tilde{E}<em>x(z) = \hat{x} E</em>{x0} e^{-\gamma z} = \hat{x} E_{x0} e^{-\alpha z} e^{-j\beta z} E ~ ( z ) = x ^ E ~ < e m > x ( z ) = x ^ E < / e m > x 0 e − γ z = x ^ E x 0 e − α z e − j β z The associated magnetic field H ~ \tilde{H} H ~ can be determined by:∇ × E ~ = − j ω μ H ~ \nabla \times \tilde{E} = -j\omega \mu \tilde{H} ∇ × E ~ = − jω μ H ~ , or using H ~ = ( k ^ × E ~ ) / η c \tilde{H} = (\hat{k} \times \tilde{E})/\eta_c H ~ = ( k ^ × E ~ ) / η c H ~ ( z ) = y ^ H ~ < e m > y ( z ) = y ^ E ~ < / e m > x ( z ) η < e m > c = y ^ E < / e m > x 0 η c e − α z e − j β z \tilde{H}(z) = \hat{y} \tilde{H}<em>y(z) = \hat{y} \frac{\tilde{E}</em>x(z)}{\eta<em>c} = \hat{y} \frac{E</em>{x0}}{\eta_c} e^{-\alpha z} e^{-j\beta z} H ~ ( z ) = y ^ H ~ < e m > y ( z ) = y ^ η < e m > c E ~ < / e m > x ( z ) = y ^ η c E < / e m > x 0 e − α z e − j β z where \etac = \sqrt{\frac{\mu}{\epsilon c}} = \sqrt{\frac{\mu}{\epsilon'}} \left[ 1 - j\frac{\epsilon''}{\epsilon'} \right]^{-1/2} \text{ (\Omega)} Attenuation and Skin Depth Magnitude of E field: ∣ E ~ < e m > x ( z ) ∣ = ∣ E < / e m > x 0 e − α z e − j β z ∣ = ∣ E x 0 ∣ e − α z |\tilde{E}<em>x(z)| = |E</em>{x0} e^{-\alpha z} e^{-j\beta z}| = |E_{x0}| e^{-\alpha z} ∣ E ~ < e m > x ( z ) ∣ = ∣ E < / e m > x 0 e − α z e − j β z ∣ = ∣ E x 0 ∣ e − α z Skin depth: δ s = 1 α (m) \delta_s = \frac{1}{\alpha} \text{ (m)} δ s = α 1 (m) The skin depth δ < e m > s \delta<em>s δ < e m > s is the value of z at which ∣ E ~ < / e m > x ( z ) ∣ / ∣ E x 0 ∣ = e − 1 ≈ 0.37 |\tilde{E}</em>x(z)|/|E_{x0}| = e^{-1} \approx 0.37 ∣ E ~ < / e m > x ( z ) ∣/∣ E x 0 ∣ = e − 1 ≈ 0.37 . At depth z = 3 δ < e m > s z = 3\delta<em>s z = 3 δ < e m > s , the field magnitude is less than 5% of its initial value, and at z = 5 δ < / e m > s z = 5\delta</em>s z = 5 δ < / e m > s , it is less than 1%. The skin depth characterizes how deep an electromagnetic wave can penetrate into a conducting medium. Conductors and Dielectrics Materials behave as dielectric or conductor. Conduction current density vs. Displacement current density. \sigma >> \omega \epsilon: displacement current >> conduction current ⟹ \implies ⟹ dielectric σ ≈ ω ϵ \sigma \approx \omega \epsilon σ ≈ ω ϵ : displacement current ≈ \approx ≈ conduction current ⟹ \implies ⟹ quasi conductor\sigma << \omega \epsilon: displacement current << conduction current ⟹ \implies ⟹ conductor ∇ × E ~ = σ + j ω ϵ \nabla \times \tilde{E} = \sigma + j\omega \epsilon ∇ × E ~ = σ + jω ϵ Approximations for Good Conductors and Dielectrics Applying binomial expansion: Good dielectric: \sigma << \omega \epsilon \implies \frac{\epsilon''}{\epsilon'} << 1 Good conductor: \sigma >> \omega \epsilon \implies \frac{\epsilon''}{\epsilon'} >> 100α ≈ ω μ σ / 2 \alpha \approx \sqrt{\omega \mu \sigma / 2} α ≈ ω μ σ /2 β ≈ ω μ σ / 2 \beta \approx \sqrt{\omega \mu \sigma / 2} β ≈ ω μ σ /2 η c ≈ ( 1 + j ) ω μ σ \eta_c \approx (1 + j) \sqrt{\frac{\omega \mu}{\sigma}} η c ≈ ( 1 + j ) σ ω μ Low and High Frequency Approximations Table summarizing expressions for α , β , η < e m > c , v < / e m > p \alpha, \beta, \eta<em>c, v</em>p α , β , η < e m > c , v < / e m > p , and λ \lambda λ for various types of media. Any Medium:α = ω μ ϵ ′ 2 [ 1 + ( ϵ ′ ′ ϵ ′ ) 2 − 1 ] 1 / 2 \alpha = \omega \sqrt{\frac{\mu \epsilon'}{2}} \left[ \sqrt{1 + (\frac{\epsilon''}{\epsilon'})^2} - 1 \right]^{1/2} α = ω 2 μ ϵ ′ [ 1 + ( ϵ ′ ϵ ′′ ) 2 − 1 ] 1/2 β = ω μ ϵ ′ 2 [ 1 + ( ϵ ′ ′ ϵ ′ ) 2 + 1 ] 1 / 2 \beta = \omega \sqrt{\frac{\mu \epsilon'}{2}} \left[ \sqrt{1 + (\frac{\epsilon''}{\epsilon'})^2} + 1 \right]^{1/2} β = ω 2 μ ϵ ′ [ 1 + ( ϵ ′ ϵ ′′ ) 2 + 1 ] 1/2 η c = μ ϵ ′ [ 1 − j ϵ ′ ′ ϵ ′ ] − 1 / 2 \eta_c = \sqrt{\frac{\mu}{\epsilon'}} \left[ 1 - j\frac{\epsilon''}{\epsilon'} \right]^{-1/2} η c = ϵ ′ μ [ 1 − j ϵ ′ ϵ ′′ ] − 1/2 Lossless Medium (σ = 0 \sigma = 0 σ = 0 ):α = 0 \alpha = 0 α = 0 β = ω μ ϵ \beta = \omega \sqrt{\mu \epsilon} β = ω μ ϵ η c = μ ϵ \eta_c = \sqrt{\frac{\mu}{\epsilon}} η c = ϵ μ Low-loss Medium (\frac{\epsilon''}{\epsilon'} << 1):η c = μ ϵ ( 1 + j ϵ ′ ′ 2 ϵ ′ ) \eta_c = \sqrt{\frac{\mu}{\epsilon}} \left( 1 + j \frac{\epsilon''}{2\epsilon'} \right) η c = ϵ μ ( 1 + j 2 ϵ ′ ϵ ′′ ) Good Conductor (\frac{\epsilon''}{\epsilon'} > 1):α = π f μ σ \alpha = \sqrt{\pi f \mu \sigma} α = π f μ σ β = π f μ σ \beta = \sqrt{\pi f \mu \sigma} β = π f μ σ η c = ( 1 + j ) π f μ σ \eta_c = (1 + j) \sqrt{\frac{\pi f \mu}{\sigma}} η c = ( 1 + j ) σ π f μ Notes: ϵ ′ = ϵ ; ϵ ′ ′ = σ ω \epsilon' = \epsilon; \epsilon'' = \frac{\sigma}{\omega} ϵ ′ = ϵ ; ϵ ′′ = ω σ