Lecture 23 Date:

Similar documents
EELE 3332 Electromagnetic II Chapter 10

Electromagnetic Waves

Electrical Boundary Conditions. Electric Field Boundary Conditions: Magnetic Field Boundary Conditions: K=J s

1. Basic introduction to electromagnetic field. wave properties and particulate properties.

ELECTROMAGNETIC WAVES AND PHOTONS

Lecture 3 Basic radiometric quantities.

Lecture 15 - Current. A Puzzle... Advanced Section: Image Charge for Spheres. Image Charge for a Grounded Spherical Shell

EP225 Note No. 5 Mechanical Waves

Math 273 Solutions to Review Problems for Exam 1

FUNDAMENTALS OF POWER SYSTEMS

No-load And Blocked Rotor Test On An Induction Machine

Basic parts of an AC motor : rotor, stator, The stator and the rotor are electrical

Pulsed Magnet Crimping

Tuning of High-Power Antenna Resonances by Appropriately Reactive Sources

Department of Mechanical Engineering Massachusetts Institute of Technology Modeling, Dynamics and Control III Spring 2002

Effects of vector attenuation on AVO of offshore reflections

c = ω k = 1 v = ω k = 1 ²µ

Streaming Calculations using the Point-Kernel Code RANKERN

Electrodynamics Part 1 12 Lectures

Section Induction motor drives

Assessment Schedule 2017 Scholarship Physics (93103)

Liquid cooling

Question 1 Equivalent Circuits

MULTI-LAYERED LOSSY FINITE LENGTH DIELECTRIC CYLINDIRICAL MODEL OF MAN AT OBLIQUE INCIDENCE

FI 3221 ELECTROMAGNETIC INTERACTIONS IN MATTER

Mechanics. Free rotational oscillations. LD Physics Leaflets P Measuring with a hand-held stop-clock. Oscillations Torsion pendulum

LECTURE 22. Collective effects in multi-particle beams: Parasitic Losses. Longitudinal impedances in accelerators (continued)

Plane Waves Part II. 1. For an electromagnetic wave incident from one medium to a second medium, total reflection takes place when

Lecture 10 Filtering: Applied Concepts

Lecture 7 Grain boundary grooving

0 of the same magnitude. If we don t use an OA and ignore any damping, the CTF is

Conduction Heat transfer: Unsteady state

Chapter 1 Basic Description of Laser Diode Dynamics by Spatially Averaged Rate Equations: Conditions of Validity

Basics of a Quartz Crystal Microbalance

Finite Element Analysis of a Fiber Bragg Grating Accelerometer for Performance Optimization

PHYS 110B - HW #2 Spring 2004, Solutions by David Pace Any referenced equations are from Griffiths Problem statements are paraphrased

PHYS 110B - HW #6 Spring 2004, Solutions by David Pace Any referenced equations are from Griffiths Problem statements are paraphrased

A) At each point along the pipe, the volume of fluid passing by is given by dv dt = Av, thus, the two velocities are: v n. + ρgy 1

The Electric Potential Energy

Online supplementary information

ELECTROMAGNETIC FIELD IN THE PRESENCE OF A THREE-LAYERED SPHERICAL REGION

MODERN CONTROL SYSTEMS

Determination of the local contrast of interference fringe patterns using continuous wavelet transform

Design By Emulation (Indirect Method)

Cake ltration analysis the eect of the relationship between the pore liquid pressure and the cake compressive stress

APPLICATION OF THE SINGLE IMPACT MICROINDENTATION FOR NON- DESTRUCTIVE TESTING OF THE FRACTURE TOUGHNESS OF NONMETALLIC AND POLYMERIC MATERIALS

On the Isentropic Forchheimer s Sound Waves Propagation in a Cylindrical Tube Filled with a Porous Media

Supplementary Figures

Tarzan s Dilemma for Elliptic and Cycloidal Motion

ECE 320 Energy Conversion and Power Electronics Dr. Tim Hogan. Chapter 1: Introduction and Three Phase Power

11.2 Stability. A gain element is an active device. One potential problem with every active circuit is its stability

SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuits II. Solutions to Assignment 3 February 2005.

Bernoulli s equation may be developed as a special form of the momentum or energy equation.

Emittance limitations due to collective effects for the TOTEM beams

Uniform Plane Waves Page 1. Uniform Plane Waves. 1 The Helmholtz Wave Equation

Exam 1 Solutions. +4q +2q. +2q +2q

High-field behavior: the law of approach to saturation (Is there an equation for the magnetization at high fields?)

Clustering Methods without Given Number of Clusters

General review: - a) Dot Product

III.9. THE HYSTERESIS CYCLE OF FERROELECTRIC SUBSTANCES

An Analytical Solution of the Radiative Transfer Equation for Inhomogeneous Finite Medium with Fresnel Boundary Conditions

Time-harmonic form Phasor form. =0 (1.11d)

Module 1: Learning objectives

USPAS Course on Recirculated and Energy Recovered Linear Accelerators

GNSS Solutions: What is the carrier phase measurement? How is it generated in GNSS receivers? Simply put, the carrier phase

Social Studies 201 Notes for March 18, 2005

Design spacecraft external surfaces to ensure 95 percent probability of no mission-critical failures from particle impact.

A Single Particle Thermal Model for Lithium Ion Batteries

Chapter 7: 17, 20, 24, 25, 32, 35, 37, 40, 47, 66 and 79.

ELECTROMAGNETIC FIELD IN THE AIR GENERATED BY A HORIZONTAL ELECTRIC DIPOLE LOCATED IN THE SPHERICAL ELECTRICALLY EARTH COATED WITH A DIELECTRIC LAYER

region 0 μ 0, ε 0 d/2 μ 1, ε 1 region 1 d/2 region 2 μ 2, ε 2

Plane Waves GATE Problems (Part I)

An Inequality for Nonnegative Matrices and the Inverse Eigenvalue Problem

Annex-A: RTTOV9 Cloud validation

MAE 101A. Homework 3 Solutions 2/5/2018

Wake Field. Impedances: gz j

Physics 2212 G Quiz #2 Solutions Spring 2018

How a charge conserving alternative to Maxwell s displacement current entails a Darwin-like approximation to the solutions of Maxwell s equations

Physics 741 Graduate Quantum Mechanics 1 Solutions to Final Exam, Fall 2014

Physics 111. Exam #3. March 4, 2011

The Influence of Landau Damping on Multi Bunch Instabilities

Source slideplayer.com/fundamentals of Analytical Chemistry, F.J. Holler, S.R.Crouch. Chapter 6: Random Errors in Chemical Analysis

Lecture 2 Review of Maxwell s Equations, EM Energy and Power

4-4 E-field Calculations using Coulomb s Law

NCAAPMT Calculus Challenge Challenge #3 Due: October 26, 2011

Uniform Plane Waves. Ranga Rodrigo. University of Moratuwa. November 7, 2008

Introduction to Laplace Transform Techniques in Circuit Analysis

SOLUTIONS

15 Problem 1. 3 a Draw the equivalent circuit diagram of the synchronous machine. 2 b What is the expected synchronous speed of the machine?

A Compensated Acoustic Actuator for Systems with Strong Dynamic Pressure Coupling

EELE 3332 Electromagnetic II Chapter 11. Transmission Lines. Islamic University of Gaza Electrical Engineering Department Dr.

Social Studies 201 Notes for November 14, 2003

Blackbody radiation. Main radiation laws. Sun as an energy source. Solar spectrum and solar constant.

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get

Convex Hulls of Curves Sam Burton

Isentropic Sound Waves Propagation in a Tube Filled with a Porous Media

Control Systems Analysis and Design by the Root-Locus Method

Lecture 2 Phys 798S Spring 2016 Steven Anlage. The heart and soul of superconductivity is the Meissner Effect. This feature uniquely distinguishes

Single-scattering solutions to radiative transfer in infinite turbid media

THE EXPERIMENTAL PERFORMANCE OF A NONLINEAR DYNAMIC VIBRATION ABSORBER

Transcription:

Lecture 3 Date: 4.4.16 Plane Wave in Free Space and Good Conductor Power and Poynting Vector

Wave Propagation in Loy Dielectric Wave propagating in z-direction and having only x-component i given by: E ( z) E e E e x z ( j ) z Where: 1 1 1 1 Inerting the time factor yield: j t ( ) ˆ z j t z ˆ x x x E( z, t) Re E ( z) e a Re E e e a The olution for magnetic field i: z j( t z) H ( z, t) ReH ˆ e e a y Where: H E η i a complex quantity known a the intrinic impedance of the medium. j e j j / 1 1/4 tan θ η 45

Wave Propagation in Loy Dielectric (contd.) In term of β, the wave velocity u and wavelength λ are: u Furthermore, the ratio of the magnitude of conduction current denity J c to that of the diplacement current denity J d i: J c E J d j E tan tanθ i known a the lo tangent and θ i the lo angle of the medium. A medium i good (lole or perfect) dielectric if tanθ i very mall (σ ωε) or a good conductor if tanθ i large (σ ωε)

Plane Wave in Lole Dielectric In a lole dielectric, σ ωε. In uch a cenario: σ, ε = ε ε r, μ = μ μ r. Therefore: u 1 Thu E and H are in time phae with each other.

Plane Wave in Free Space In thi cae: σ =, ε = ε, μ = μ. Therefore: c u 1 c c The fact that EM wave travel in free pace with the peed of light i ignificant. It provide evidence that light i the manifetation of an EM wave. We have: The plot of E and H are hown below. 1 377 Furthermore: E E t z a ˆ co( ) x E = E + co( βz) a x E H co( t z) aˆ y H = H + co( βz) a y

Plane Wave in Free Space (contd.) In general, if a E, a H and a k are unit vector along E, H and the direction of propagation, then: aˆ aˆ aˆ aˆ aˆ aˆ aˆ aˆ aˆ k E H k H E E H k Both E and H field are everywhere normal to the direction of wave propagation. It mean that the field lie in a plane that i tranvere or orthogonal to the direction of propagation. They form an EM wave that ha no electric or magnetic field component along the direction of propagation uch a wave i called tranvere electromagnetic (TEM) wave. A combination of E and H i called a uniform plane wave becaue field have ame magnitude throughout any tranvere plane. The direction in which the electric field point i the polarization of a TEM wave Eentially, polarization of a uniform plane wave decribe the locu traced by the tip of the E vector (in the plane orthogonal to the direction of propagation) at a given point in pace a a function of time.

Plane Wave in Free Space (contd.) E( z, t) E e co( t z) a x It i polarized in x-direction z ˆ E = E + co(ωt) a x It illutrate a uniform plane wave H = H + co(ωt) a y In practice, a uniform plane wave can t exit becaue it tretche to infinity and would repreent an infinite energy however thee wave are characteritically imple and fundamentally important. Thee erve a approximation for practical wave uch a thoe from radio antenna at ditance ufficiently far from radiating ource. The on-going dicuion are applicable for any other iotropic medium.

Plane Wave in Good Conductor In a good conductor, diplacement current i negligible in comparion to conduction current (J conduction J diplacement ) Becaue, for a perfect or good conductor, σ ωε. Although thi inequality i frequency dependent, mot good conductor (uch a copper and aluminum) have conductivitie on the order of 1 7 mho/m and negligible polarization uch that we never encounter the frequencie at which the diplacement current become comparable to the conduction current. For a good conductor: σ =, ε = ε, μ = μ μ r. Therefore: f u

Plane Wave in Good Conductor (contd.) j Furthermore: 45 If: E E e t z a x Thu E lead H by 45 z ˆ co( ) Then: E H e t z a z co( 45 ) ˆ y The amplitude of E or H i attenuated by the factor e αz a it travel along the medium. The rate of attenuation in a good conductor i characterized by ditance called kin depth δ a ditance over which plane wave i attenuated by a factor e 1 (about 37% of the original value) in a good conductor. E(x) E +

Plane Wave in Good Conductor (contd.) kin depth i a meaure of the depth to which an EM wave can penetrate the medium. E e E e 1 1 Valid for any material medium 1 1 f For a partially conducting medium, the kin depth can be coniderably large. 1 1 j j /4 For a good conductor: e For good conductor, α = β = 1, therefore: z/ δ z E E e t a ˆ co( ) x

Plane Wave in Good Conductor (contd.) z E E e t a z/ ˆ co( ) x It how that kin depth (δ) i the meaure of exponential damping the wave experience a it travel through the conductor. E + 66.1/ f (mm) For Copper!.368E + It demontrate that the field dampen and will hardly propagate through good conductor

Example 1 Uniform plane wave (f = 1MHz) at an air/copper interface. Determine α 1, α, β 1, β, u 1, u, λ 1, and λ. α 1 =, β 1 = ω c α = β = 1 δ

Example 1 (contd.) In the air, c 8 31 / m 6 1 1.9 rad / 8 c 31 m 8 c 31 1 3m 6 f 1 In the copper, 1 1.66 f f f 4 1 7 5.81 7 at 1 MHZ:.66mm 1 3 15.1 Np / m.415mm u f 415 m /

Example A plane wave E = E co(ωt βz) a x i incident on a good conductor at z. Find the current denity in the conductor. Since, J = σe, the wave equation change to: J J Furthermore, the incident E ha only an x-component that varie with z. Therefore, J = J x z, t a x and: d J x J x dz The olution i: z z J x Ae Be

Example (contd.) B i zero conidering that wave i propagating in +z direction. Furthermore, in a good conductor σ ωε o that α = β = 1. Therefore, δ z(1 j)/ Therefore: J Ae x j 1 j z(1 j)/ J x J x e 1 j J x () Where, J x () i the current denity on the conductor urface. J x Thi depict the cenario

Example 3 Indrapratha Intitute of Given the current denity of previou problem J x = J x ()e z(1+j)/δ, find the magnitude of total current through a trip of the conductor of infinite depth along z direction and width w along y direction. I w J dydz x w () z(1 j)/ I J x dye dz J x () δ I Jx() w 1 j I J x () w It actually reemble a uniform current denity J x () flowing through a thin urface width w and depth δ. A J x decay exponentially with depth z, a conductor of finite thickne d can be conidered electrically equivalent to one of infinite depth a long a d exceed a few kin depth (δ).

Example 4 In the previou example, what i the voltage acro a length l at the urface. What i the impedance of the conductor in conideration? J x () δ J () x V El l Z V J x() 1 j l I J () w x Z V 1 j l l Z Z I w w Z i urface impedance and the real part of thi i called ac reitance.

Plane Wave in Good Conductor (contd.) Electromagnetic Shielding The previou example how that we may encloe a volume with a thin layer of good conductor to act a an electromagnetic hield. Depending on the application, the electromagnetic hield may be neceary to prevent wave radiating out of the hielded volume or to prevent wave from penetrating into the hielded volume.

Plane Wave in Good Conductor (contd.) Given a plane wave incident on a highly-conducting urface, the electric field (and thu the current denity) i found to be concentrated at the urface of the conductor. The ame phenomenon occur for a current carrying conductor uch a a wire. The effect i frequency dependent, jut a it i in the incident plane wave example. Thi phenomenon i known a the kin effect. Therefore, one can ay, The proce whereby the field intenity in a conductor rapidly decreae i called kin effect. kin effect i the tendency of the charge to migrate from the bulk of the conducting material to the urface, reulting in higher reitance (for ac!) The field and aociated current are confined to a very thin layer (the kin) of the conductor urface.

Plane Wave in Good Conductor (contd.) For a wire of radiu a, it i a good approximation at high frequencie to aume that all of the current flow in the circular ring of thickne δ. kin effect i ued to advantage in many application. For example, becaue the kin depth in ilver i very mall, the difference in performance between a pure ilver and ilver-plated bra component i negligible, o ilver plating i often ued to reduce the material cot of waveguide component. Furthermore, hollow tubular conductor are ued intead of olid conductor in outdoor televiion antenna.

Plane Wave in Good Conductor (contd.) The kin depth i ueful in calculating the ac reitance. The reitance R = l σs The kin reitance R i the real part of η. i called the dc reitance R dc. R 1 f Reitance of a unit width and unit length of the conductor having croectional area 1 δ. Therefore, for a given width w and length l, the ac reitance i: For a conductor wire of radiu a: R R ac dc l l w a a l l S a R ac l Rl w w Since, δ a at high frequencie, R ac i far greater than R dc. In general, the ratio of the ac and dc reitance tart at 1. for dc and very low frequencie and increae a the frequency increae.

Power and Poynting Vector For any wave with an electric field E and magnetic field H, the direction of wave propagation i alo the direction of power per unit area (or power denity) carried by the wave. It i repreented by Poynting Vector S. S E H W/m Intantaneou Poynting Vector direction and denity of power flow at a point S a n The total power flowing through thi aperture i: a k P = A S. a n da = SAcoθ

Power and Poynting Vector (contd.) Except for the fact that unit of S are per unit area, the Poynting Vector i the vector analogue of the calar expreion for the intantaneou power P(z, t) flowing through a tranmiion line: P( z, t) v( z, t) i( z, t) 1 * Pav( z) Re V ( z) I ( z) From LC we can recall In a imilar manner, power denity (W/m ) aociated with a time-harmonic EM field in term of E and H phaor i: 1 P Re E H * ave

Example 5 Determine the expreion for the time-average power denity for an EM plane wave in term of electric field only and magnetic field only; given (a) a loy medium, (b) a lole medium. (a) 1 P Re E H * ave P 1 ReE H aˆ * ave k P aˆ Re E H k * ave E H j e H * E E e * * * j P ave * aˆ k E Re E j e P ave * k EE E Re co j e aˆ aˆ k

Example 5 (contd.) aˆ P Re H e H k j * ave P ave * k EE H Re co j e aˆ aˆ k (b) Lole Medium η real, θ η = P ave E aˆ k P ave H aˆ k