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ELECTROMAGNETIC ENGINEERING EE325 INDEX Ampere's circuital law.....11 Ampere's law ................... 6 angstrom .......................... 2 Avogadro's number........... 2 B Ampere's circuital law 11 Biot-Savart law ...............11 Boltzmann's constant........ 2 capacitance ...................7, 8 between coaxial cylinders ................................ 7 between concentric spheres .................... 7 between parallel plates. 7 between two conductors 7 characteristic impedance .. 2 complex conjugate............ 1 complex notation.............. 1 conductance ..................... 8 conductivity ..................... 8 semiconductor.............. 8 conservative field law....... 6 constants .......................... 2 continuity equation........... 8 coordinate systems ..........10 coordinate transformations10 coulomb ........................... 1 Coulomb's law.................. 7 cross product...................10 curl .................................. 9 current ............................. 8 current density ................. 7 D flux density ................. 6 del ................................... 8 divergence........................ 9 dot product....................... 9 duality of J and D............. 8 E electric field................. 5 electric field..................... 5 electron mass ................... 2 electron volt ..................... 2 electrostatic force ............................ 5 potential ...................... 5 electrostatics .................... 5 elipse ............................... 8 Faraday's law ..............6, 12 flux density...................... 6 force electrostatic ................. 5 magnetic .....................11 Gauss' law........................ 6 geometry.......................... 8 grad operator.................... 8 H magnetic field intensity12 impedance short-circuit ................. 2 induced voltage due to changing magnetic field........................13 due to conductor motion13 Faraday's law ..............12 slider problem.............13 inductance.......................12 J current density.............. 7 joule ................................ 2 Laplacian ......................... 9 Lenz's law .......................12 light, speed of .................. 2 line impedance ................. 3 linkage ............................12 COULOMB [C] shunt stub ........................ 4 single-stub tuning............. 4 Smith chart ...................... 4 Smith charts..................... 4 space derivative ............... 8 sphere .............................. 8 standing wave ratio .......... 4 static magnetic field ........11 stub length ....................... 4 surface charge density ...... 6 time average power .......... 5 vector differential equation8 volume energy density...... 7 wave forward-traveling ......... 5 wave equation .................. 2 wavelength....................... 2 We potential energy......... 7 we volume energy density 7 X reactance ..................... 3 Zin line impedance ........... 3 Φ electrostatic potential ...................... 5 Γ reflection coefficient .... 2 Ψ magnetic flux .............12 λ wavelength................... 2 ρs surface charge density . 6 σ conductivity ................. 8 ∇ del............................... 8 ∇× curl ........................... 9 ∇· divergence................ 9 ∇2 Laplacian ................... 9 COMPLEX CONJUGATES A unit of electrical charge equal to one amp second, 18 the charge on 6.21×10 electrons, or one joule per volt. The complex conjugate of a number is simply that number with the sign changed on the imaginary part. This applies to both rectangular and polar notation. When conjugates are multiplied, the result is a scalar. (a + jb)(a − jb) = a 2 + b 2 COMPLEX NOTATION ( A∠B°)( A∠ − B°) = A 2 ae jb = (a∠b) where b may be in radians or degrees (if noted). Tom Penick magnetic energy ..............12 magnetic field .................11 at the center of a circular wire ........................11 central axis of a solenoid ...............................11 due to a finite straight conductor................11 due to an infinite straight conductor................11 magnetic field intensity ...12 magnetic flux ..................12 magnetic force.................11 magnetization..................13 matching transformer inline – reactive load.... 3 inline – resistive load... 3 mathematics ..................... 8 Maxwell's equations......... 6 mutual inductance ...........12 nabla operator .................. 8 permeability..................... 2 permittivity ...................... 2 phase constant.................. 2 Planck's constant .............. 2 Poisson's equation ............ 6 potential energy................ 7 power with phasor notation..... 5 reactance.......................... 3 reflection coefficient......... 2 resistance ......................... 8 Rydberg constant.............. 2 self-inductance ................12 series stub........................ 4 [email protected] Other properties of conjugates: ( ABC + DE + F )* = ( A * B * C * + D * E * + F *) (e − jB )* = e + jB www.teicontrols.com/notes 10/22/2000 Page 1 of 13 TRANSMISSION LINES SHORT-CIRCUIT IMPEDANCE [Ω] Γ L REFLECTION COEFFICIENT [V/V] Z sc = jZ 0 tan(β l ) The reflection coefficient is a value from –1 to +1 which, when multiplied by the wave voltage, determines the amount of voltage reflected at one end of the transmission line. ΓL = ρe jψ = where: Z 0 is the characteristic impedance β = ω LC = ZL − Z0 1 + ΓL and Z L = Z 0 Z L + Z0 1 − ΓL l is the length of the line [m] where: Z L is the load impedance CONSTANTS ΓL is the load reflection coefficient ρ is the reflection coefficient magnitude ψ is the reflection coefficient phase Z0 = L is the characteristic impedance C THE COMPLEX WAVE EQUATION The complex wave equation is applicable when the excitation is sinusoidal and the circuit is under steady state conditions. d 2V ( z ) = −β 2V ( z ) dz2 2π is the phase constant λ where β = ω LC = The complex wave equation above is a second-order ordinary differential equation commonly found in the analysis of physical systems. The general solution is: + V ( z) = V e − jβ z − jβ z − +V e 2π is the phase constant λ + jβz + jβ z where e and e represent wave propagation in the +z and –z directions respectively. The same equation applies to current: I ( z ) = I + e − jβz + I − e + jβz Avogadro’s number [molecules/mole] N A = 6.02 × 10 23 Boltzmann’s constant k = 1.38 × 10 −23 J/K = 8.62 × 10 −5 eV/K Elementary charge q = 1.60 × 10 −19 C Electron mass m0 = 9.11 × 10 −31 kg Permittivity of free space ε 0 = 8.85 × 10 −12 F/m Permeability constant µ 0 = 4π × 10 −7 H/m Planck’s constant h = 6.63 × 10 −34 J-s Rydberg constant = 4.14 × 10 −15 cV-s R = 109,678 cm-1 kT @ room temperature kT = 0.0259 eV Speed of light c = 2.998 × 10 8 m/s 1 Å (angstrom) 10-8 cm = 10-10 m 1 µm (micron) 10-4 cm 1 nm = 10Å = 10-7 cm 1 eV = 1.6 × 10-19 J 1 V = 1 J/C 1 N/C = 1 V/m 1 J = 1 N· m = 1 C· V and I ( z) = + V e − jβz + V − e + jβz Z0 λ WAVELENGTH [m] where Z 0 = L / C is the characteristic impedance of the line. These equations represent the voltage and current phasors. Tom Penick [email protected] λ= vp f vp = velocity of propagation (2.998×108 m/s for a line in air) f = frequency [Hz] www.teicontrols.com/notes 10/22/2000 Page 2 of 13 ¼ -WAVELENGTH INLINE MATCHING TRANSFORMER – resistive load X REACTANCE [Ω] For use with a purely resistive load that does not match the line impedance. The load is matched to the line by inserting a ¼-wavelength segment having a characteristic impedance ZQ. −j XC = ωC λ /4 Z0 X L = jω L ZQ RL Z0 = characteristic impedance of the transmission line [Ω] λ = wavelength [meters] RL = resistance of the load [Ω] ZQ = characteristic impedance of the ¼-wave matching segment [Ω] Z Q = Z 0 RL ¼ -WAVELENGTH INLINE MATCHING TRANSFORMER – reactive load For use with a reactive load. The load is matched to the line by inserting a ¼-wavelength segment having a characteristic impedance ZQ at a distance l from the load. l is the length of transmission line required to produce the first voltage maximum—closest to the load. If the load is inductive, the first voltage maximum will be closer than the first voltage minimum, i.e. within ½ wavelength. λ /4 Z0 XC = reactance [Ω] XL = reactance [Ω] j = −1 ω = frequency [radians] C = capacitance [F] L = inductance [H] Z in = Z 0 Z L + jZ 0 tan β l Z 0 + jZ L tan β l l = distance from load [m] j = −1 β = phase constant Z0 = characteristic impedance [Ω] ZL = load impedance [Ω] The line impedance of a ¼-wavelength line is the inverse of the load impedance. Impedance is a real value when its magnitude is maximum or minimum. Z max = Z 0 S = Z 0 Z min = l ZQ Zin Z0 Zin LINE IMPEDANCE [Ω] 1+ ρ 1− ρ Z0 1− ρ = Z0 S 1+ ρ Z0 = characteristic impedance [Ω] S = standing wave ratio ρ = magnitude of the reflection coefficient ZL First find the reflection coefficient in order to determine the value of ψ. Then find the length l of the line that will convert the load to a pure resistance, i.e. produces the first voltage maximum. Find this resistance (Zin) using the line impedance formula. Then determine the impedance ZQ of the ¼-wavelength segment that will match the load to the line. ΓL is the load reflection coefficient ZL − Z0 ψ = phase of the reflection jψ ΓL = ρe = coefficient [radians] ZL + Z0 ρ = magnitude of the i.e. ΓL = ρ∠ψ (radians) reflection coefficient [Ω] Z0 = characteristic ψ ψλ impedance [Ω] l= = 2β 4π Z + jZ 0 tan βl Z in = Z 0 L Z 0 + jZ L tan βl Z Q = Z 0 Z in β = 2π / λ λ = vp/f wavelength [m] Zin = impedance (resistive) of the load combined with the l segment [Ω] ZQ = line impedance of the ¼-wave matching segment [Ω] Tom Penick [email protected] www.teicontrols.com/notes 10/22/2000 Page 3 of 13 SMITH CHARTS FINDING A STUB LENGTH 2. 0 0 . 1 .05 .0 6 Admittance (short) Y= ∞ .04 .03 .22 .02 .23 5 2 0 . 1 1 . 0 .49 0 . 2 6 .2 7 5. 0 .46 45 .29 .324 λ .28 .47 .48 . 5 . 0 .01 .24 Admittance (open) Y =0 . .34 .35 0 . 1 2 .33 .36 .37 .38 .39 .4 .41 .42 4 0. 5 1 .4 .3 .4 3 SINGLE-STUB TUNING .18 5.0 Shorted stub of length .324 λ matches an admittance of 1-j.5 The basic idea is to connect a line stub in parallel (shunt) or series a distance d from the load so that the imaginary part of the load impedance will be canceled. .17 .3 Z = normalized impedance [Ω] .07 .074 λ .13 .14 .15 .16 .21 reflection coefficient β = phase constant Γ = reflection coefficient .08 .09 2.0 e j 2βz = 1∠2β z Z( z ) − 1 Γ( z ) = Z( z ) + 1 Z Γ −1 Z= L ZL = L Z0 ΓL + 1 Towar d g ener ato r .11 .12 .1 .2 z = distance from load [m] j = −1 ρ = magnitude of the j .5 9 .1 Γ( z ) = ΓL e j 2 βz Open stub of length .074 λ matches an admittance of 1-j.5 5 0. Anchor a compass at the center of the chart and draw an arc through the normalized load impedance point. Points along this arc represent the normalized impedance at various points along the transmission line. Clockwise movement along the arc represents movement from the load toward the source with one full revolution representing 1/2 wavelength as marked on the outer circle. The two points where the arc intersects the horizontal axis are the voltage maxima (right) and the voltage minima (left). Points opposite the impedance (180° around the arc) are admittance. The reason admittance is useful is because admittances in parallel are simply added. 2 Draw a straight line from the center of the chart through the normalized load impedance point to the edge of the chart. Example: Find the lengths of open and shorted shunt stubs to match an admittance of 1-j0.5. The admittance of an open shunt (zero length) is Y=0; this point is located at the left end of the Smith Chart x-axis. We proceed clockwise around the Smith chart, i.e. away from the end of the stub, to the +j0.5 arc (the value needed to match –j0.5). The difference in the starting point and the end point on the wavelength scale is the length of the stub in wavelengths. The length of a shorted-type stub is found in the same manner but with the starting point at Y=∞ ∞. .3 First normalize the load impedance by dividing by the characteristic impedance, and find this point on the chart. An inductive load will be located on the top half of the chart, a capacitive load on the bottom half. 5 In this example, all values were in units of admittance. If we were interested in finding a stub length for a series stub problem, the units would be in impedance. The problem would be worked in exactly the same way. Of course in impedance, an open shunt (zero length) would have the value Z=∞ ∞ , representing a point at the right end of the x-axis. Shunt-stub: Select d so that the admittance Y looking toward the load from a distance d is of the form Y0 + jB. Then the stub susceptance is chosen as –jB, resulting in a matched condition. Series-stub: Select d so that the admittance Z looking toward the load from a distance d is of the form Z0 + jX. Then the stub susceptance is chosen as -jX, resulting in a matched condition. d Y0 Open or short Y0 YL SWR STANDING WAVE RATIO [V/V] Y0 SWR = l V V max min = I I max min = 1+ ρ 1− ρ d Z0 Z0 ZL Z0 l Open or short Tom Penick [email protected] www.teicontrols.com/notes 10/22/2000 Page 4 of 13 E ELECTRIC FIELD P(z) TIME-AVERAGE POWER ON A LOSSLESS TRANSMISSION LINE [W] Equal to the power delivered to the load. The power delivered to the load is maximized under matched conditions, i.e. ρ = 0, otherwise part of the power is reflected back to the source. To calculate power, it may be simpler to find the input impedance and use P = I2R or P = IV. V+ = the voltage of the 2 P( z ) = V + (1 − ρ ) 2 2Z 0 1 P( z ) = Re{V ( z ) 2 [ I ( z) ]*} forward-traveling wave [V] Z0 = characteristic impedance [Ω] ρ = magnitude of the reflection coefficient Re = "the real part" POWER USING PHASOR NOTATION [W] 1 S = VI * 2 S = power [W] V = volts [V] I* = complex conjugate of current [A] V+ FORWARD-TRAVELING WAVE V+ = Z inV0 (Z in + Z S )e jβl 1 + ΓL e − j 2βl ( coefficient ELECTROSTATICS F ELECTROSTATIC FORCE F12 = (r − r ) 1 Q1Q2 2 1 3 4πε 0 r2 − r1 1 = 9 × 10 9 4πε 0 F12 = the force exerted by charge Q1 on Q2. [N] r1 = vector from the origin to Q1 r2 = vector from the origin to Q2. When finding the force on one charge due to multiple charges, the result can be found by summing the effects of each charge separately or by converting the multiple charges to a single equivalent charge and solving as a 2-charge problem. Tom Penick 1 n r − rk′ Qk ∑ 4πε0 k =1 r − rk′ 3 dE = 1 ˆ ρl (r ′) R dl ′ 4πε0 r − r′ 2 E= 1 ˆ ρl (r ′) dl ′ R 2 ∫ 4πε0 r − r′ Electric field from a potential: E = −∇Φ refer to the NABLA notes on page 8. *NOTE: The l symbols could be replaced by a symbol for area or volume. See Working With … on page 9. ) β = phase constant l = length of the line [m] ΓL = load reflection V+ = the voltage of the forwardtraveling wave [V] V0 = source voltage [V] Zin = input impedance [Ω] ZS = source impedance [Ω] Ep = [email protected] Ep = electric field at point p due to a charge Q or charge density ρ [V/m] dE = an increment of electric field [V/m] Q = electric charge [C] ε0 = permittivity of free space 8.85 × 10-12 F/m ρl = charge density; charge per unit length* [C/m] dl' = a small segment of line l* R̂ = unit vector pointing from r' to r , i.e. in the direction of r - r'. r' = vector location of the source charge in relation to the origin r = vector location of the point at which the value of Ep is observed ∇ = Del, Grad, or Nabla operator Φ ELECTROSTATIC POTENTIAL [V] 1 n Qk ∑ 4πε0 k =1 r − rk′ 1 ρl dl ′ dΦ = 4πε0 r − r′ Φ= Φ= 1 4πε0 ρl ∫ r − r′ dl ′ Potential due to an electric field: b Φ ab = − ∫ E·d l a To evaluate voltage at all points. Φ (r ) = − ∫ E·d l r ∞ *NOTE: The l symbols could be replaced by a symbol for area or volume. See Working With … on page 9. Φ = the potential [V] dΦ = an increment of potential [V] Φ ab = the potential difference between points a and b [V] E = electric field dl' = a small segment of line l* dl = the differential vector displacement along the path from a to b ε0 = permittivity of free space 8.85 × 10-12 F/m Q = electric charge [C] ρl = charge density along a line* [C/m] rk' = vector location of source charge Qk r' = vector location of the source charge in relation to the origin r = vector location of electrostatic potential Φ in relation to the origin www.teicontrols.com/notes 10/22/2000 Page 5 of 13 MAXWELL'S EQUATIONS GAUSS'S LAW Maxwell's equations govern the principles of guiding and propagation of electromagnetic energy and provide the foundations of all electromagnetic phenomena and their applications. ∇× E = - ∂B ∂t ∫ ε E·ds = Q Faraday's Law S Gauss' Law ∇× H = J + ∂D ∂t Ampere's Law* ∇ ⋅B = 0 no name law, where: E = electric field [V/m] B = magnetic field [T] t = time [s] D = electric flux density [C/m2] ρ = volume charge density [C/m3] H = magnetic field intensity [A/m] J = current density [A/m2] S enc V ε0 = permittivity of free space 8.85 × 10 F/m E = electric field [V/m] D = electric flux density vector [C/m2] ds = a small increment of surface S ρ = volume charge density [C/m3] dv = a small increment of volume V Qenc = total electric charge enclosed by the Gaussian surface [S] ∇·D = ρ div (ε 0 ·E ) = ρ or GAUSS'S LAW – an example problem Find the intensity of the electric field at distance r from a straight conductor having a voltage V. Consider a cylindrical surface of length l and radius r enclosing a portion of the conductor. The electric field passes through the curved surface of the cylinder but not the ends. Gauss's law says that the electric flux passing through this curved surface is equal to the charge enclosed. POISSON'S EQUATION ρ ∇2Φ = − ε0 2π ∫ ε0E·ds = ε0 ∫ Er lr dφ = Qenc = ρl l = ClVl 0 S ρ s SURFACE CHARGE DENSITY [C/m ] 2 ˆE E n = n· ∫ D·ds = ∫ ρ dv = Q The differential version of Gauss's law is: *Maxwell added the ∂ D term to Ampere's Law. ∂t ε0 = permittivity of free space 8.85 × 1012 enc 0 -12 ∇ ⋅D = ρ ρ s = ε 0 En The net flux passing through a surface enclosing a charge is equal to the charge. Careful, what this first integral really means is the surface area multiplied by the perpendicular electric field. There may not be any integration involved. F/m En = electric field normal to the surface [V/m] D FLUX DENSITY [C/m2] 2π so ε0 Er r ∫ dφ = ClV 0 and Er = ClV 2πε0 r Er = electric field at distance r from the conductor [V/m] l = length [m] r dφ φ = a small increment of the cylindrical surface S [m2] ρl = charge density per unit length [C/m] Cl = capacitance per unit length [F/m] V = voltage on the line [V] or ELECTRIC DISPLACEMENT PER UNIT AREA D ≡ rˆ Q 4πr 2 D = εE Q = electric charge [C] ε = dielectric constant ε = ε 0 ε r E = electric field [V/m] CONSERVATIVE FIELD LAW ∇×E = 0 ∫ E·dl = 0 S E = electric field [V/m] ds = a small increment of length Tom Penick [email protected] www.teicontrols.com/notes 10/22/2000 Page 6 of 13 COULOMB'S LAW ∇·D = ρ C CAPACITANCE BETWEEN TWO PARALLEL SOLID CYLINDRICAL CONDUCTORS ∫ D·ds = ∫ ρ dv S V D = electric flux density vector [C/m2] ρ = volume charge density [C/m3] ds = a small increment of surface S We POTENTIAL ENERGY [J] This also applies to a single conductor above ground, where the height above ground is d/2. C = capacitance πε [F/m] C= , where d ? a ε = permittivity of ln d / a ( The energy required to bring charge q from infinity to a distance R from charge Q. We = qΦ = We = or Qq 4πεR 1 1 ρΦ dv = ∫ D·E dv ∫ 2 V 2V Φ = the potential between q and Q [V] q,Q = electric charges [C] ε = permittivity of the material R = distance [m] ρ = volume charge density [C/m3] E = electric field [V/m] D = electric flux density vector [C/m2] ) C= the material d = separation (center-tocenter) [m] a = conductor radius [m] πε cosh −1 d 2a C CAPACITANCE BETWEEN PARALLEL PLATES C = capacitance [F] ε = permittivity of the material d = separation of the plates [m] A = area of one plate [m2] εA C= d C CAPACITANCE BETWEEN COAXIAL CYLINDERS we VOLUME ENERGY DENSITY [J/m3] for the Electrostatic Field C= 1 1 we = D·E = εE 2 2 2 Φ = the potential between q and Q [V] ε = permittivity of the material R = distance [m] E = electric field [V/m] D = electric flux density vector [C/m2] C CAPACITANCE OF CONCENTRIC SPHERES 4πεab C= b−a CAPACITANCE C CAPACITANCE [F] C= Cl = Q Φ ρl V 2πε ln ( b / a ) C = capacitance [F/m] ε = permittivity of the material b = radius of the outer cylinder [m] a = radius of the inner cylinder [m] Q = total electric charge [C] Φ = the potential between q and Q [V] Cl = capacitance per unit length [F/m] ρl = charge density per unit length [C/m] V = voltage on the line [V] C = capacitance [F/m] ε = permittivity of the material b = radius of the outer sphere [m] a = radius of the inner sphere [m] J CURRENT DENSITY The amount of current flowing perpendicularly 2 through a unit area [A/m ] σ = conductivity of the material [S/m] J = σE E = electric field [V/m] I = current [A] I = J·ds S ds = a small increment of surface S In nc = the number of conduction band semiconductor electrons material: qe = electron charge -1.602×10-19 C J = nc q e v d vd = a small increment of surface S ∫ Tom Penick [email protected] www.teicontrols.com/notes 10/22/2000 Page 7 of 13 MATHEMATICS CONTINUITY EQUATION ∇·J + ∂ρ =0 ∂t WORKING WITH LINES, SURFACES, AND VOLUMES J = current density [A/m2] J = σE ρ = volume charge density [C/m3] DUALITY RELATIONSHIP of J and D RESISTANCE, CAPACITANCE, CURRENT, CONDUCTIVITY Where current enters and leaves a conducting medium via two perfect conductors (electrodes) we have: σ σQ D·ds = ∫ S ε ε J = current density [A/m2] J = σE I = ∫ J·ds = σ ∫ E·ds = S S E = electric field [V/m] D = electric flux density vector [C/m2] D = εE As a result of this, we have the following relation, useful in finding the resistance between two conductors: R = resistance [Ω] ε C = capacitance [F] RC = ε = permittivity of the material σ σ = conductivity of the material [S/m] G CONDUCTANCE [Ω−1] G= = 1 I = R ∆Φ σ ∫ E·ds ∫ S − + R = resistance [Ω] I = current [A] ∆Φ = voltage potential [V] σ = conductivity of the material [S/m] E·dl σ SEMICONDUCTOR CONDUCTIVITY [Ω −1] σ ≈ q µe N d σ = conductivity of the material [S/m]G = conductance [Ω−1] q = electron charge -1.602×10-19 C µe = electron mobility [m2/(V-s)] Nd = concentration of donors, and thereby the electron concentration -3 in the transition region [m ] Tom Penick [email protected] ρl(r') means "the charge density along line l as a function of r'." This might be a value in C/m or it could be a function. Similarly, ρs(r') would be the charge density of a surface and ρv(r') is the charge density of a volume. For example, a disk of radius a having a uniform charge density of ρ C/m2, would have a total charge of ρπa2, but to find its influence on points along the central axis we might consider incremental rings of the charged surface as ρs(r') dr'= ρs2πr' dr'. If dl' refers to an incremental distance along a circular contour C, the expression is r'dφ φ, where r' is the radius and dφ φ is the incremental angle. GEOMETRY SPHERE Area A = 4πr Volume V = ELLIPSE Area A = πAB Circumference 2 4 3 πr 3 L ≈ 2π a2 + b2 2 ∇ NABLA, DEL OR GRAD OPERATOR [+ m-1] Compare the ∇ operation to taking the time derivative. Where ∂/∂t means to take the derivative with respect to time and introduces a s-1 component to the units of the result, the ∇ operation means to take the derivative with respect to distance (in 3 dimensions) and introduces a m-1 component to the units of the result. ∇ terms may be called space derivatives and an equation which contains the ∇ operator may be called a vector differential equation. In other words ∇A is how fast A changes as you move through space. ∂A ∂A ∂A in rectangular ∇A = xˆ + yˆ + zˆ coordinates: ∂x ∂y ∂z in cylindrical ∂A ˆ 1 ∂A ∂A ∇A = rˆ +φ + zˆ coordinates: in spherical coordinates: ∂r r ∂φ ∂z ∂A ˆ 1 ∂A ˆ 1 ∂A ∇A = rˆ +θ +φ ∂r r ∂θ r sin θ ∂φ www.teicontrols.com/notes 10/22/2000 Page 8 of 13 ∇ 2 THE LAPLACIAN [+ m-2] ∇ 2 A = xˆ ∇ 2 Ax + yˆ ∇ 2 Ay + zˆ ∇ 2 Az = 0 in rectangular coordinates: ∂2 ∂2 ∂2 + + =0 ∂x 2 ∂y 2 ∂z 2 ∇ 2 A ≡ ∇ (∇·A ) − ∇ × ∇ × A = grad (div A ) − curl(curl A ) ∇2 ≡ in spherical and cylindrical coordinates: for example, the Laplacian of electrostatic potential: ∇· ∇ 2Φ = ∂ 2Φ ∂ 2Φ ∂ 2Φ + + 2 =0 ∂x 2 ∂y 2 ∂z -1 DIVERGENCE [+ m ] The del operator followed by the dot product operator is read as "the divergence of" and is an operation performed on a vector. In rectangular coordinates, ∇⋅ means the sum of the partial derivatives of the magnitudes in the x, y, and z directions with respect to the x, y, and z variables. The result is a scalar, and a factor of m-1 is contributed to the units of the result. For example, in this form of Gauss' law, where D is a density per unit area, ∇⋅D becomes a density per unit volume. div D = ∇ ⋅ D = ∂ Dx ∂ Dy ∂ Dz + + =ρ ∂x ∂y ∂z in cylindrical coordinates: div D = ∂z ∂D 1 ∂ (rDr ) + 1 φ + ∂Dz r ∂r r ∂φ ∂z in spherical coordinates: 1 ∂ (r Dr ) 1 ∂(sin θDθ ) 1 ∂Dφ div D = 2 + + r ∂r r sin θ ∂θ r sin θ ∂φ 2 Tom Penick curl B = ∇ × B = ∂B ∂B ∂B ∂B ∂B ∂B xˆ z − y + yˆ x − z + zˆ y − x ∂z ∂x ∂x ∂y ∂z ∂y in cylindrical coordinates: curl B = ∇ × B = 1 ∂Bz ∂Bφ ˆ ∂Br ∂Bz 1 ∂ ( rBφ ) ∂Br rˆ − +φ − + zˆ − ∂r r ∂r ∂φ ∂z r ∂φ ∂z in spherical coordinates: curl B = ∇ × B = rˆ 1 ∂ ( Bφ sin θ ) ∂Bθ − + r sin θ ∂θ ∂φ 1 1 ∂Br ∂ ( rBφ ) ˆ 1 ∂ ( rBθ ) ∂Br θˆ − − +φ r sin θ ∂φ ∂r r ∂r ∂θ The divergence of a curl is always zero: ∇·(∇ × H ) = 0 The dot product is a scalar value. In the electrostatic context, the divergence of D is the total outward flux per unit volume due to a source charge. The divergence of vector D is: in rectangular ∂Dx ∂Dy ∂Dz div D = + + coordinates: ∂y The circulation around an enclosed area. The curl of vector B is in rectangular coordinates: DOT PRODUCT [= units2] D = electric flux density vector D = εE [C/m2] ρ = source charge density [C/m3] ∂x ∇ × CURL [+ m-1] [email protected] A • B = (xˆ Ax + yˆ Ay + zˆ Az ) • (xˆ B x + yˆ B y + zˆ B z ) = Ax Bx + Ay B y + Az B z A • B = A B cos ψ AB B ψ xˆ • yˆ = 0 , xˆ • xˆ = 1 B • yˆ = (xˆ Bx + yˆ By + zˆ Bz ) • yˆ = By Projection of B along â: A•B B (B • aˆ )aˆ ψ A B â ψ â The dot product of 90° vectors is zero. The dot product is commutative and distributive: A •B = B• A A • (B + C) = A • B + A • C www.teicontrols.com/notes 10/22/2000 Page 9 of 13 CROSS PRODUCT COORDINATE TRANSFORMATIONS A × B = (xˆ Ax + yˆ Ay + zˆ Az ) × (xˆ B x + yˆ B y + zˆ B z ) = xˆ ( Ay B z − Az B y ) + yˆ ( Az B x − Ax B z ) + zˆ ( Ax B y − Ay B x ) A × B = nˆ A B sin ψ AB A×B where n̂ is the unit vector normal to both A and B (thumb of right-hand rule). B × A = −A × B x×y = z y × x = −z φ× z = r φ× r = − z n A x× x = 0 ψ B The cross product is distributive: A × (B × C) = ( A ⋅ C) B − ( A ⋅ B) C Cartesian or Rectangular Coordinates: x̂ is a unit vector r = x2 + y2 + z 2 φˆ = − xˆ sin φ + yˆ cos φ zˆ = zˆ Cylindrical to Rectangular: To obtain: r ( x, y, z) = xxˆ + yyˆ + zzˆ xˆ = rˆ cos φ − φˆ cos φ φˆ = rˆ sin φ + yˆ cos φ zˆ = zˆ ˆ r + θˆ Aθ + φˆ Aφ To obtain: A ( r , θ, φ) = rA Ar = x 2 + y 2 + z 2 rˆ = xˆ sin θ cos φ + yˆ sin θ sin φ + zˆ cos θ θ= Spherical Coordinates: r is distance from center θ is angle from vertical φ is the CCW angle from the x-axis r̂ , θ̂ , and φ̂ are unit vectores and are functions of position—their orientation depends on where they are located. Cylindrical Coordinates: r is distance from the vertical (z) axis φ is the CCW angle from the x-axis z is the vertical distance from origin z cos −1 x2 + y2 + z2 θˆ = xˆ cos θ cos φ + yˆ cos θ sin φ − zˆ sin θ y φ = tan −1 φˆ = − xˆ sin φ + yˆ cos φ x Spherical to Rectangular: To obtain: r ( x, y, z) = xxˆ + yyˆ + zzˆ x = r sin θ cos φ xˆ = rˆ sin θ cos φ − θˆ cos θ cos φ − φˆ sin φ y = r sin θ sin φ yˆ = rˆ sin θ sin φ + θˆ cos θ sin φ + φˆ cos φ z = r cos θ Tom Penick rˆ = xˆ cos φ + yˆ sin φ Rectangular to Spherical: COORDINATE SYSTEMS C(r , φ, z ) Ar = x 2 + y 2 y φ = tan −1 x z=z y = r sin φ z=z Also, we have: P(r , θ, φ) ˆ r + φˆ Aφ + zA ˆ z To obtain: A ( r , φ, z) = rA x = r cos φ A × (B + C ) = A × B + A × C r ( x, y, z) = xxˆ + yyˆ + zzˆ Rectangular to Cylindrical: [email protected] www.teicontrols.com/notes zˆ = rˆ cos θ − θˆ sin θ 10/22/2000 Page 10 of 13 THE STATIC MAGNETIC FIELD F F12 MAGNETIC FORCE [N/m] due to a conductor If the current in the two wires travels in opposite directions, the force will be attractive. F12 = the force exerted by conductor 1 carrying current I on conductor 2. xˆ µ 0 I1 I 2 [N/m] F12 = -7 µ 0 = permeability constant 4π×10 2πd [H/m] I = current [A] d = distance between conductors [m] BP BIOT-SAVART LAW Determines the B field vector at any point P identified by the position vector r, due to a differential current element I dl' located at vector r'. BP = magnetic field vector ˆ [T] µ 0 I dl '×R dB P = µ = permeability constant 0 4πR 2 4π×10-7 [H/m] µ I dl'×(r − r ') I dl' = current element [A] BP = 0 3 R̂ = unit vector pointing 4π C ∫ r − r' ˆ = r − r' R r − r' from the current element to point P R = distance between the current element and point P [m] B MAGNETIC FIELD [T or A/m] due to an infinite straight conductor May also be applied to the magnetic field close to a conductor of finite length. BP = magnetic field vector [T] µ0 = permeability constant 4π×10-7 [H/m] µ0 I ˆ I = current [A] BP = φ 2πr r = perpendicular distance from the conductor [m] B MAGNETIC FIELD [T] due to a finite straight conductor at a point perpendicular to the midpoint BP = magnetic field vector [T] µ0 Ia B P = φˆ µ0 = permeability constant 2πr r 2 + a 2 4π×10-7 [H/m] I = current [A] a a = half the length of the r conductor [m] r = perpendicular distance I from the conductor [m] B MAGNETIC FIELD [T] Bctr at the center of a circular wire of N turns B = magnetic field [T] -7 µ 0 NI µ0 = permeability const. 4π×10 [H/m] N = number of turns of the coil = zˆ 2a I = current [A] a = radius [m] B AMPERE'S CIRCUITAL LAW Ampere's law is a consequence of the Biot-Savart law and serves the same purpose as Gauss's law. Ampere's law states that the line integral of B around any closed contour is equal to µ0 times the total net current I passing through the surface S enclosed by the contour C. This law is useful in solving magnetostatic problems having some degree of symmetry. B = magnetic field vector, equal to B times the appropriate unit vector [T] µ0 = permeability constant 4π×10-7 B·dl = µ 0 J·ds [H/m] C S dl = an increment of the line which = µ0 I is the perimeter of contour C [ m] J = current density [A/m2] J = σE ds = an increment of surface [m2] ∫ ∫ Tom Penick [email protected] B MAGNETIC FIELD [T] along the central axis of a solenoid µ 0 NI (z + l / 2) − (z − l / 2) 2 2l a 2 + (z + l / 2 )2 a 2 + (z − l / 2 ) µ NI and at the center of the coil: Bctr ≈ zˆ 0 l B(z ) = zˆ B = magnetic field [T] µ0 = permeability constant 4π×10-7 [H/m] N = number of turns I = current [A] www.teicontrols.com/notes l = length of the solenoid [m] z = distance from center of the coil [m] a = coil radius [m] 10/22/2000 Page 11 of 13 H MAGNETIC FIELD INTENSITY [A/m] L11 SELF-INDUCTANCE [H] The magnetic field intensity vector is directly analogous to the electric flux density vector D in electrostatics in that both D and H are mediumindependent and are directly related to their sources. H = magnetic field [A/m] B B = magnetic field vector [T] H≡ −M µ0 µ0 = permeability const. 4π×10-7 [H/m] ∂D M = magnetization [A/m2] ∇×H = J + J = current density [A/m ] J = σE ∂ t D = electric flux density vector [C/m2] When a current in coil 1 induces a current in coil 2, the induced current in coil 2 induces a current back in coil 1. This is self-inductance. N = number of turns of the coil NΛ L11 = 1 11 Λ11 = the total flux linked by a single I1 turn of coil 1 [Wb] 2 I1 = current in coil 1 [A] N Ψ = 1 11 Ψ11 = the magnetic flux produced by I1 a single turn of coil 1 and linked by a single turn of coil 1 [Wb] Ψ, Λ (,lambda) MAGNETIC FLUX, LINKAGE Flux linkage Λ is the ability of a closed circuit to store magnetic energy. It depends, in part, on the physical layout of the conductors. It is the total magnetic field due to circuit #1 passing through the area enclosed by the conductors of circuit #2. The text seemed to describe Ψ as the flux due to one turn and Λ as the flux due to all of the turns of the coil, but was not consistent so be careful. Ψ12 = the magnetic flux passing Ψ12 = ∫ B1 ·ds 2 S2 Λ 12 = N 1 Ψ12 Λ = N ∫ B·ds S through coil 2 that is produced by a current in coil 1 [Wb] Λ = total flux linkage [Wb] B = magnetic field vector [T] N = number of turns of the coil ds = an increment of surface [m2] LENZ'S LAW Induced voltage causes current to flow in the direction that produces a magnetic flux which opposes the flux that induced the voltage in the first place. This law is useful in checking or determining the sign or polarity of a result. L INDUCTANCE [H] Inductance is the ability of a conductor configuration to "link magnetic flux", i.e. store magnetic energy. Two methods of calculating inductance are given below. Λ I 2W L = 2m I L= Λ = flux linkage [Wb] I = current [A] Wm = energy stored in a magnetic field [J] Tom Penick [email protected] L12 MUTUAL INDUCTANCE [H] The mutual inductance between two coils. N = number of turns of N Λ N NΨ L12 = 2 12 I1 = 2 1 12 the coil I1 Neumann formula: L12 = µ 0 N1 N 2 4π ∫ ∫ C1 C2 dl 1 ·dl 2 r − r' Λ = flux linkage [Wb] I = current [A] Ψ = magnetic flux [Wb] r = vector to the point of observation r' = vector to source Wm MAGNETIC ENERGY [J] Energy stored in a magnetic field [Joules]. Wm = energy stored in a magnetic field [J] 1 2 µ = permeability constant 0 Wm = B dv ' 4π×10-7 [H/m] 2µ 0 V B = magnetic field [T] ∫ FARADAY'S LAW When the magnetic flux enclosed by a loop of wire changes with time, a current is produced in the loop. The variation of the magnetic flux can result from a time-varying magnetic field, a coil in motion, or both. ∂B ∇×E = the curl of the electric field ∇×E = − B = magnetic field vector [T] ∂t Another way of expressing Faraday's law is that a changing magnetic field induces an electric field. where S is the surface d Vind = E·dl = − B·ds enclosed by contour C dt S C. Ñ∫ ∫ (see also Induced Voltage below) www.teicontrols.com/notes 10/22/2000 Page 12 of 13 Vind INDUCED VOLTAGE M MAGNETIZATION [A/m] The voltage induced in a coil due to a changing magnetic field is equal to the number of turns in the coil times the rate at which the magnetic field is changing (could be a change in field strength or coil area normal to the field). dΨ N = number of turns of the coil Vind = − N Ψ = the magnetic flux produced by dt a single turn of the coil [Wb] The induced magnetic dipole moment per unit volume. N = number of turns of the coil Nq 2 a 2 B M=− e qe = electron charge 4me 1.602×10-19 C a = orbit radius of an electron [m] χ B or M = m B = magnetic field vector [T] µ0 µ0 = permeability constant 4π×10-7 where [H/m] me = who knows? Nq e2 a 2 µ 0 χm = − χm = magnetic susceptibility Vind = ∫ E·dl C Vind INDUCED VOLTAGE DUE TO 4me MOTION When conductors move in the presence of magnetic fields, an induced voltage is produced even if the magnetic fields do not vary in time. For the voltage produced due to both a changing magnetic field and a conductor in motion: ∂B ·ds + Ñ∫ ( v × B )·dl S ∂t C Vind = − ∫ B = magnetic field vector [T] v = velocity vector of the conductor [m/s] ds = increment of the surface normal to the magnetic field vector [m2] dl = incremental length of conductor [m] INDUCED VOLTAGE – SLIDER PROBLEM A frictionless conducting bar moves to the right at velocity v produces a current I. d I R B0 v h An expanding magnetic field area having a static magnetic field directed into the page produces a CCW current. Vind = induced voltage [V] B0 = static magnetic field [T] h = distance between the conductor rails [T] v = velocity of the conductor [m/s] Vind = B0 hv Fmag = magnetic force opposing slider [N] Fmag = xˆ B0 Ih x̂ = unit vector in the direction against conductor movement [m/s] d E = I 2R I = current [A] v E = energy produced [J or W/s] R = circuit resistance [Ω] d = distance the conductor moves [m] Tom Penick [email protected] www.teicontrols.com/notes 10/22/2000 Page 13 of 13