Electromagnetism Concepts and Principles The Quantities SourcesCharge: Q Q Q (C) Line charge density: ρ l \rho_l ρ l (C/m) Surface charge density: ρ s \rho_s ρ s (C/m²) Volume charge density: ρ v \rho_v ρ v (C/m³) CurrentI : Current (A) J : Conduction current density (A/m²) I = d Q d t I = \frac{dQ}{dt} I = d t d Q Fields ElectricE E E : Electric field strength (V/m)D D D : Electric flux density (C/m²) MagneticH H H : Magnetic field strength (A/m)B B B : Magnetic flux density (Wb/m²) Material Properties ϵ \epsilon ϵ : Permittivity of a material (F/m)μ \mu μ : Permeability of a material (H/m)σ \sigma σ : Conductivity of a material (S/m)D = ϵ E D = \epsilon E D = ϵ E B = μ H B = \mu H B = μ H Electromagnetism History ~1820 – 1831 – 1835Ampere quantified the relationship between magnetic field and current. Faraday discovered that changing magnetic flux induces EMF (electromotive force). Gauss showed that the source of electric fields were electric charges (no magnetic charge). Maxwell's Equations Gauss’s law: ∇ ⋅ D = ρ v \nabla \cdot D = \rho_v ∇ ⋅ D = ρ v Gauss’s law for magnetic fields: ∇ ⋅ B = 0 \nabla \cdot B = 0 ∇ ⋅ B = 0 Faraday’s law: ∇ × E = − ∂ B ∂ t \nabla \times E = -\frac{\partial B}{\partial t} ∇ × E = − ∂ t ∂ B Ampere’s law: ∇ × H = J \nabla \times H = J ∇ × H = J Maxwell's Correction to Ampere's Law Maxwell noticed that the original equations were incomplete. The divergence of Ampere’s equation leads to ∇ ⋅ ( ∇ × H ) = 0 \nabla \cdot (\nabla \times H) = 0 ∇ ⋅ ( ∇ × H ) = 0 , which implies ∇ ⋅ J = 0 \nabla \cdot J = 0 ∇ ⋅ J = 0 . This implication suggests that the source of electric current is zero, conflicting with the continuity equation: ∇ ⋅ J = − ∂ ρ v ∂ t \nabla \cdot J = -\frac{\partial \rho_v}{\partial t} ∇ ⋅ J = − ∂ t ∂ ρ v . Maxwell added a displacement current term to satisfy the continuity equation and Gauss's law: ∇ ⋅ D = ρ v \nabla \cdot D = \rho_v ∇ ⋅ D = ρ v The complete Ampere’s law is then expressed as: ∇ × H = J + ∂ D ∂ t \nabla \times H = J + \frac{\partial D}{\partial t} ∇ × H = J + ∂ t ∂ D Integral form of Maxwell's equations:Gauss's law: ∮ < e m > S D ⋅ d s = ∫ < / e m > v ρ v d v = Q \oint<em>S D \cdot ds = \int</em>v \rho_v dv = Q ∮ < e m > S D ⋅ d s = ∫ < / e m > v ρ v d v = Q Gauss's law for magnetism: ∮ S B ⋅ d s = 0 \oint_S B \cdot ds = 0 ∮ S B ⋅ d s = 0 Faraday's law: ∮ < e m > C E ⋅ d l = − d d t ∮ < / e m > S B ⋅ d s \oint<em>C E \cdot dl = -\frac{d}{dt} \oint</em>S B \cdot ds ∮ < e m > CE ⋅ d l = − d t d ∮ < / e m > SB ⋅ d s Ampere-Maxwell's law: ∮ < e m > C H ⋅ d l = ∮ < / e m > S J ⋅ d s + d d t ∮ S D ⋅ d s \oint<em>C H \cdot dl = \oint</em>S J \cdot ds + \frac{d}{dt} \oint_S D \cdot ds ∮ < e m > C H ⋅ d l = ∮ < / e m > S J ⋅ d s + d t d ∮ S D ⋅ d s Maxwell’s Equations - Static Fields Electrostatics∇ × E = 0 ⇒ ∮ C E ⋅ d l = 0 \nabla \times E = 0 \Rightarrow \oint_C E \cdot dl = 0 ∇ × E = 0 ⇒ ∮ C E ⋅ d l = 0 ∇ ⋅ D = ρ ⇒ ∮ S D ⋅ d s = Q \nabla \cdot D = \rho \Rightarrow \oint_S D \cdot ds = Q ∇ ⋅ D = ρ ⇒ ∮ S D ⋅ d s = Q Magnetostatics∇ × H = J ⇒ ∮ < e m > C H ⋅ d l = ∫ < / e m > S J ⋅ d s \nabla \times H = J \Rightarrow \oint<em>C H \cdot dl = \int</em>S J \cdot ds ∇ × H = J ⇒ ∮ < e m > C H ⋅ d l = ∫ < / e m > S J ⋅ d s ∇ ⋅ B = 0 ⇒ ∮ S B ⋅ d s = 0 \nabla \cdot B = 0 \Rightarrow \oint_S B \cdot ds = 0 ∇ ⋅ B = 0 ⇒ ∮ S B ⋅ d s = 0 Charge Distributions Volume charge density: ρ < e m > v = lim < / e m > Δ V → 0 Δ q Δ V = d q d V \rho<em>v = \lim</em>{\Delta V \to 0} \frac{\Delta q}{\Delta V} = \frac{dq}{dV} ρ < e m > v = lim < / e m > Δ V → 0 Δ V Δ q = d V d q (C/m³) Total charge in a volume: Q = ∫ < e m > V ρ < / e m > v d v Q = \int<em>V \rho</em>v dv Q = ∫ < e m > V ρ < / e m > v d v (C) Total charge on a surface: Q = ∫ < e m > S ρ < / e m > s d S Q = \int<em>S \rho</em>s dS Q = ∫ < e m > Sρ < / e m > s d S Total charge along a line: Q = ∫ < e m > l ρ < / e m > l d l Q = \int<em>l \rho</em>l dl Q = ∫ < e m > lρ < / e m > l d l Current Density Current flowing in a tube: Δ I = J ⋅ Δ s \Delta I = J \cdot \Delta s Δ I = J ⋅ Δ s Current density: J = ρ v u J = \rho_v u J = ρ v u (A/m²), where u u u is the velocity of the charge. Total current: I = ∫ S J ⋅ d s I = \int_S J \cdot ds I = ∫ S J ⋅ d s (A) Convection Current The amount of charge that crosses the tube's cross-sectional surface Δ s \Delta s Δ s in time Δ t \Delta t Δ t is Δ q = ρ < e m > v Δ V = ρ < / e m > v u Δ s ′ Δ t \Delta q = \rho<em>v \Delta V = \rho</em>v u \Delta s' \Delta t Δ q = ρ < e m > v Δ V = ρ < / e m > vu Δ s ′ Δ t For a surface with any orientation: J = ρ v u J = \rho_v u J = ρ v u (A/m²) I = ∫ S J ⋅ d s I = \int_S J \cdot ds I = ∫ S J ⋅ d s (A)Conduction Current When current is due to movement of charged particles relative to their host material, J J J is called conduction current density. Conduction current obeys Ohm's law, whereas convection current does not. Coulomb's Law Electric field at point P due to single charge. Electric force on a test charge placed at P. Electric Flux Density D = ϵ E D = \epsilon E D = ϵ E ϵ = ϵ < e m > r ϵ < / e m > 0 \epsilon = \epsilon<em>r \epsilon</em>0 ϵ = ϵ < e m > rϵ < / e m > 0 ϵ 0 = 8.85 × 10 − 12 ≈ ( 1 / 36 π ) × 10 − 9 \epsilon_0 = 8.85 \times 10^{-12} \approx (1/36\pi) \times 10^{-9} ϵ 0 = 8.85 × 1 0 − 12 ≈ ( 1/36 π ) × 1 0 − 9 (F/m)If ϵ \epsilon ϵ is independent of the magnitude of E E E , the material is linear. If ϵ \epsilon ϵ is independent of the direction of E E E , the material is isotropic. Electric Field Due to Multiple Charges Electric field due to charge 1: E < e m > 1 = q < / e m > 1 ( R − R < e m > 1 ) 4 π ϵ ∣ R − R < / e m > 1 ∣ 3 E<em>1 = \frac{q</em>1 (R - R<em>1)}{4\pi\epsilon |R - R</em>1|^3} E < e m > 1 = 4 π ϵ ∣ R − R < / e m > 1 ∣ 3 q < / e m > 1 ( R − R < e m > 1 ) Electric field due to charge 2: E < e m > 2 = q < / e m > 2 ( R − R < e m > 2 ) 4 π ϵ ∣ R − R < / e m > 2 ∣ 3 E<em>2 = \frac{q</em>2 (R - R<em>2)}{4\pi\epsilon |R - R</em>2|^3} E < e m > 2 = 4 π ϵ ∣ R − R < / e m > 2 ∣ 3 q < / e m > 2 ( R − R < e m > 2 ) The electric field obeys the principle of linear superposition: E = E < e m > 1 + E < / e m > 2 E = E<em>1 + E</em>2 E = E < e m > 1 + E < / e m > 2 E = 1 4 π ϵ ∑ < e m > i = 1 N q < / e m > i ( R − R < e m > i ) ∣ R − R < / e m > i ∣ 3 E = \frac{1}{4\pi\epsilon} \sum<em>{i=1}^N \frac{q</em>i (R - R<em>i)}{|R - R</em>i|^3} E = 4 π ϵ 1 ∑ < e m > i = 1 N ∣ R − R < / e m > i ∣ 3 q < / e m > i ( R − R < e m > i ) Electric Field Due to Charge Distributions Field due to a line charge: d E = ρ l d l ′ R ^ 4 π ϵ R 2 dE = \frac{\rho_l dl' \hat{R}}{4\pi\epsilon R^2} d E = 4 π ϵ R 2 ρ l d l ′ R ^ Field due to a surface charge: d E = ρ s d S ′ R ^ 4 π ϵ R 2 dE = \frac{\rho_s dS' \hat{R}}{4\pi\epsilon R^2} d E = 4 π ϵ R 2 ρ s d S ′ R ^ Field due to a volume charge: d E = ρ v d V ′ R ^ 4 π ϵ R 2 dE = \frac{\rho_v dV' \hat{R}}{4\pi\epsilon R^2} d E = 4 π ϵ R 2 ρ v d V ′ R ^ Where: R ^ = R − R ′ ∣ R − R ′ ∣ \hat{R} = \frac{R - R'}{|R - R'|} R ^ = ∣ R − R ′ ∣ R − R ′ Example: Electric Field Due to a Finite Line Charge Problem: Find the electric field, E ( P ) E(P) E ( P ) , due to a constant line charge ρ l \rho_l ρ l between z = a z = a z = a and z = b z = b z = b . Geometry: The problem is independent of ϕ \phi ϕ , so use cylindrical coordinates. R ^ = R − R ′ ∣ R − R ′ ∣ \hat{R} = \frac{R - R'}{|R - R'|} R ^ = ∣ R − R ′ ∣ R − R ′ d E ( R ) = ρ l d z ′ R ^ 4 π ϵ R 2 dE(R) = \frac{\rho_l dz' \hat{R}}{4 \pi \epsilon R^2} d E ( R ) = 4 π ϵ R 2 ρ l d z ′ R ^ R ′ ⃗ = z ′ z ^ \vec{R'} = z' \hat{z} R ′ = z ′ z ^ R ⃗ = r r ^ + z z ^ \vec{R} = r \hat{r} + z \hat{z} R = r r ^ + z z ^ R ⃗ = R ⃗ − R ′ ⃗ = r r ^ + ( z − z ′ ) z ^ \vec{R} = \vec{R} - \vec{R'} = r \hat{r} + (z - z') \hat{z} R = R − R ′ = r r ^ + ( z − z ′ ) z ^ ∣ R ∣ = r 2 + ( z − z ′ ) 2 |R| = \sqrt{r^2 + (z - z')^2} ∣ R ∣ = r 2 + ( z − z ′ ) 2 E ( R ) = ∫ < e m > a b d E = ∫ < / e m > a b ρ l ( r r ^ + ( z − z ′ ) z ^ ) d z ′ 4 π ϵ ( r 2 + ( z − z ′ ) 2 ) 3 / 2 E(R) = \int<em>a^b dE = \int</em>a^b \frac{\rho_l (r \hat{r} + (z - z') \hat{z}) dz'}{4 \pi \epsilon (r^2 + (z - z')^2)^{3/2}} E ( R ) = ∫ < e m > a b d E = ∫ < / e m > a b 4 π ϵ ( r 2 + ( z − z ′ ) 2 ) 3/2 ρ l ( r r ^ + ( z − z ′ ) z ^ ) d z ′ Using the substitution u = z ′ − z u = z' - z u = z ′ − z :E ( R ) = ρ < e m > l 4 π ϵ [ r ^ ∫ < / e m > u ( a ) u ( b ) r d u ( r 2 + u 2 ) 3 / 2 + z ^ ∫ u ( a ) u ( b ) − u d u ( r 2 + u 2 ) 3 / 2 ] E(R) = \frac{\rho<em>l}{4 \pi \epsilon} \left[ \hat{r} \int</em>{u(a)}^{u(b)} \frac{r du}{(r^2 + u^2)^{3/2}} + \hat{z} \int_{u(a)}^{u(b)} \frac{-u du}{(r^2 + u^2)^{3/2}} \right] E ( R ) = 4 π ϵ ρ < e m > l [ r ^ ∫ < / e m > u ( a ) u ( b ) ( r 2 + u 2 ) 3/2 r d u + z ^ ∫ u ( a ) u ( b ) ( r 2 + u 2 ) 3/2 − u d u ] E ( R ) = ρ < e m > l 4 π ϵ [ r ^ u r r 2 + u 2 ∣ < / e m > z − b z − a + z ^ 1 r 2 + u 2 ∣ z − b z − a ] E(R) = \frac{\rho<em>l}{4 \pi \epsilon} \left[ \hat{r} \frac{u}{r \sqrt{r^2 + u^2}} \Big|</em>{z-b}^{z-a} + \hat{z} \frac{1}{\sqrt{r^2 + u^2}} \Big|_{z-b}^{z-a} \right] E ( R ) = 4 π ϵ ρ < e m > l [ r ^ r r 2 + u 2 u < / e m > z − b z − a + z ^ r 2 + u 2 1 z − b z − a ] E ( R ) = ρ < e m > l 4 π ϵ [ 1 r r 2 + ( z ′ − z ) 2 ∣ < / e m > a b r ^ + 1 r 2 + ( z ′ − z ) 2 ∣ a b z ^ ] E(R) = \frac{\rho<em>l}{4 \pi \epsilon} \left[ \frac{1}{r \sqrt{r^2 + (z'-z)^2}} \Big|</em>{a}^{b} \hat{r} + \frac{1}{\sqrt{r^2 + (z'-z)^2}} \Big|_{a}^{b}\hat{z} \right] E ( R ) = 4 π ϵ ρ < e m > l [ r r 2 + ( z ′ − z ) 2 1 < / e m > a b r ^ + r 2 + ( z ′ − z ) 2 1 a b z ^ ] E ( R ) = ρ < e m > l 4 π ϵ [ ( z − z ′ r 2 + ( z − z ′ ) 2 ) < / e m > z = a z = b z ^ + ( r r 2 + ( z − z ′ ) 2 ) z = a z = b r ^ ] E(R) = \frac{\rho<em>l}{4 \pi \epsilon} \left[ \left(\frac{z-z'}{\sqrt{r^2 + (z - z')^2}}\right)</em>{z=a}^{z=b}\hat{z} + \left(\frac{r}{\sqrt{r^2 + (z-z')^2}}\right)_{z=a}^{z=b}\hat{r} \right] E ( R ) = 4 π ϵ ρ < e m > l [ ( r 2 + ( z − z ′ ) 2 z − z ′ ) < / e m > z = a z = b z ^ + ( r 2 + ( z − z ′ ) 2 r ) z = a z = b r ^ ] Example 4-4: Electric Field of a Ring of Charge Problem: Determine the electric field intensity E E E at a point P = ( 0 , 0 , h ) P = (0, 0, h) P = ( 0 , 0 , h ) along the axis of a ring of charge with radius b b b and uniform line charge density ρ l \rho_l ρ l . Solution: Consider a differential ring segment with cylindrical coordinates ( b , ϕ , 0 ) (b, \phi, 0) ( b , ϕ , 0 ) . The segment has length d l = b d ϕ dl = b d\phi d l = b d ϕ and charge d q = ρ < e m > l d l = ρ < / e m > l b d ϕ dq = \rho<em>l dl = \rho</em>l b d\phi d q = ρ < e m > l d l = ρ < / e m > l b d ϕ . The distance vector from segment 1 to point P = ( 0 , 0 , h ) P = (0, 0, h) P = ( 0 , 0 , h ) is R 1 ⃗ = − b r ^ + h z ^ \vec{R_1} = -b \hat{r} + h \hat{z} R 1 = − b r ^ + h z ^ . ∣ R 1 ∣ = b 2 + h 2 |R_1| = \sqrt{b^2 + h^2} ∣ R 1 ∣ = b 2 + h 2 R 1 ^ = − b r ^ + h z ^ b 2 + h 2 \hat{R_1} = \frac{-b \hat{r} + h \hat{z}}{\sqrt{b^2 + h^2}} R 1 ^ = b 2 + h 2 − b r ^ + h z ^ The electric field at P = ( 0 , 0 , h ) P = (0, 0, h) P = ( 0 , 0 , h ) due to the charge in segment 1 is:d E < e m > 1 = ρ < / e m > l d l R < e m > 1 ^ 4 π ϵ < / e m > 0 R < e m > 1 2 = ρ < / e m > l b ( − b r ^ + h z ^ ) d ϕ 4 π ϵ 0 ( b 2 + h 2 ) 3 / 2 dE<em>1 = \frac{\rho</em>l dl \hat{R<em>1}}{4 \pi \epsilon</em>0 R<em>1^2} = \frac{\rho</em>l b (-b \hat{r} + h \hat{z}) d\phi}{4 \pi \epsilon_0 (b^2 + h^2)^{3/2}} d E < e m > 1 = 4 π ϵ < / e m > 0 R < e m > 1 2 ρ < / e m > l d l R < e m > 1 ^ = 4 π ϵ 0 ( b 2 + h 2 ) 3/2 ρ < / e m > l b ( − b r ^ + h z ^ ) d ϕ Symmetry considerations: For every ring segment, there is a diametrically opposite segment. The r ^ \hat{r} r ^ -components cancel, and the z ^ \hat{z} z ^ -components add. d E = d E < e m > 1 + d E < / e m > 2 = z ^ ρ < e m > l b h d ϕ 2 π ϵ < / e m > 0 ( b 2 + h 2 ) 3 / 2 dE = dE<em>1 + dE</em>2 = \hat{z} \frac{\rho<em>l b h d\phi}{2 \pi \epsilon</em>0 (b^2 + h^2)^{3/2}} d E = d E < e m > 1 + d E < / e m > 2 = z ^ 2 π ϵ < / e m > 0 ( b 2 + h 2 ) 3/2 ρ < e m > l bh d ϕ Integrating over a semicircle (0 ≤ ϕ ≤ π 0 \leq \phi \leq \pi 0 ≤ ϕ ≤ π ) to account for the symmetry:E = 2 ∫ < e m > 0 π ρ < / e m > l b h 4 π ϵ 0 ( b 2 + h 2 ) 3 / 2 d ϕ E = 2 \int<em>0^{\pi} \frac{\rho</em>l b h}{4 \pi \epsilon_0 (b^2 + h^2)^{3/2}} d\phi E = 2 ∫ < e m > 0 π 4 π ϵ 0 ( b 2 + h 2 ) 3/2 ρ < / e m > l bh d ϕ E = 2 ρ < e m > l b h 4 ϵ < / e m > 0 ( b 2 + h 2 ) 3 / 2 = z ^ Q 4 π ϵ < e m > 0 ( b 2 + h 2 ) 3 / 2 E = 2 \frac{\rho<em>l b h}{4 \epsilon</em>0 (b^2 + h^2)^{3/2}} = \hat{z} \frac{Q}{4 \pi \epsilon<em>0 (b^2 + h^2)^{3/2}} E = 2 4 ϵ < / e m > 0 ( b 2 + h 2 ) 3/2 ρ < e m > l bh = z ^ 4 π ϵ < e m > 0 ( b 2 + h 2 ) 3/2 Q , where Q = 2 π b ρ < / e m > l Q = 2 \pi b \rho</em>l Q = 2 πb ρ < / e m > l is the total charge on the ring.Example 4-5: Electric Field of a Circular Disk of Charge Problem: Find the electric field at point P = ( 0 , 0 , h ) P = (0, 0, h) P = ( 0 , 0 , h ) due to a circular disk of radius a a a and uniform charge density ρ s \rho_s ρ s . Treating the disk as a set of concentric rings, a ring of radius r r r and width d r dr d r has area d s = 2 π r d r ds = 2 \pi r dr d s = 2 π r d r and charge d q = ρ < e m > s d s = 2 π ρ < / e m > s r d r dq = \rho<em>s ds = 2 \pi \rho</em>s r dr d q = ρ < e m > s d s = 2 π ρ < / e m > sr d r . Using the result from Example 4-4 for the on-axis electric field due to a ring:d E = z ^ h ( 2 π ρ < e m > s r d r ) 4 π ϵ < / e m > 0 ( r 2 + h 2 ) 3 / 2 dE = \hat{z} \frac{h (2 \pi \rho<em>s r dr)}{4 \pi \epsilon</em>0 (r^2 + h^2)^{3/2}} d E = z ^ 4 π ϵ < / e m > 0 ( r 2 + h 2 ) 3/2 h ( 2 π ρ < e m > sr d r ) Integrating over the limits r = 0 r = 0 r = 0 to r = a r = a r = a :E = ∫ < e m > 0 a ρ < / e m > s h r d r 2 ϵ 0 ( r 2 + h 2 ) 3 / 2 z ^ E = \int<em>0^a \frac{\rho</em>s h r dr}{2 \epsilon_0 (r^2 + h^2)^{3/2}} \hat{z} E = ∫ < e m > 0 a 2 ϵ 0 ( r 2 + h 2 ) 3/2 ρ < / e m > s h r d r z ^
Solved: E = ρ < e m > s 2 ϵ < / e m > 0 ( ∣ h ∣ a 2 + h 2 ) − 1 ) = ± ρ < e m > s 2 ϵ < / e m > 0 ( 1 − ∣ h ∣ a 2 + h 2 ) ) E = \frac{\rho<em>s}{2 \epsilon</em>0} \left( \frac{|h|}{\sqrt{a^2 + h^2})} - 1\right) = \pm \frac{\rho<em>s}{2 \epsilon</em>0} \left(1 - \frac{|h|}{\sqrt{a^2 + h^2})} \right) E = 2 ϵ < / e m > 0 ρ < e m > s ( a 2 + h 2 ) ∣ h ∣ − 1 ) = ± 2 ϵ < / e m > 0 ρ < e m > s ( 1 − a 2 + h 2 ) ∣ h ∣ ) The plus sign for h > 0 (P above the disk) and the minus sign when h < 0 (P below the disk). For an infinite sheet of charge with a = ∞ a = \infty a = ∞ :E = ± ρ < e m > s 2 ϵ < / e m > 0 E = \pm \frac{\rho<em>s}{2 \epsilon</em>0} E = ± 2 ϵ < / e m > 0 ρ < e m > s E E E is the same at all points above the x-y plane and at all points below the x-y plane.