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Current Electricity

1. Electric Fields

1.1 Coulomb's Law

The electrostatic force between two point charges is governed by Coulomb's inverse-square law. The magnitude of the force is directly proportional to the product of the charge magnitudes and inversely proportional to the square of the separation distance:

F=kq1q2r2F = k\frac{|q_1||q_2|}{r^2}

where kk is Coulomb's constant, defined as:

k=14πε0=8.99×109Nm2C2k = \frac{1}{4\pi\varepsilon_0} = 8.99 \times 10^9 \mathrm{ N m}^2 \mathrm{ C}^{-2}

The permittivity of free space is ε0=8.85×1012C2N1m2\varepsilon_0 = 8.85 \times 10^{-12} \mathrm{ C}^2 \mathrm{ N}^{-1} \mathrm{ m}^{-2}.

In vector form, the force exerted on q2q_2 by q1q_1 is:

F12=kq1q2r2r^12\vec{F}_{12} = k\frac{q_1 q_2}{r^2}\hat{r}_{12}

where r^12\hat{r}_{12} is the unit vector pointing from q1q_1 to q2q_2. Like charges produce a repulsive force (positive FF along r^12\hat{r}_{12}), and unlike charges produce an attractive force (negative FF, i.e. anti-parallel to r^12\hat{r}_{12}).

:::info[Data Booklet Reference] Both forms appear in the IB data booklet:

F=q1q24πε0r2F = \frac{q_1 q_2}{4\pi\varepsilon_0 r^2} E=q4πε0r2E = \frac{q}{4\pi\varepsilon_0 r^2}

:::

1.2 Electric Field Strength

The electric field E\vec{E} at a point in space is defined as the electrostatic force per unit positive test charge placed at that point:

E=Fq\vec{E} = \frac{\vec{F}}{q}

The SI unit is Vm1\mathrm{V m}^{-1} (equivalent to NC1\mathrm{N C}^{-1}). For a point charge QQ, the field at distance rr is:

E=Q4πε0r2E = \frac{Q}{4\pi\varepsilon_0 r^2}

This is an inverse-square radial field. Field lines point radially outward for positive source charges and radially inward for negative source charges.

1.3 Uniform Field Between Parallel Plates

When two parallel conducting plates are separated by a distance dd and maintained at a potential difference VV, the electric field between them is uniform:

E=VdE = \frac{V}{d}

This is exact for infinite plates and an excellent approximation when the plate separation is much smaller than the plate dimensions. Field lines are parallel and equally spaced between the plates; they fringe at the edges.

The direction of the field is from the positive plate to the negative plate. A positive test charge placed in this field experiences a force F=qEF = qE directed from positive to negative plate.

Worked Example: Electric Field Between Parallel Plates

Two parallel plates are separated by d=3.0cmd = 3.0\,\mathrm{cm} with a potential difference of 600V600\,\mathrm{V}. A proton (q=1.6×1019Cq = 1.6 \times 10^{-19}\,\mathrm{C}, mp=1.67×1027kgm_p = 1.67 \times 10^{-27}\,\mathrm{kg}) is placed at rest next to the positive plate.

Find the acceleration of the proton and the time to reach the negative plate.

Electric field:

E=Vd=6000.030=2.0×104V/mE = \frac{V}{d} = \frac{600}{0.030} = 2.0 \times 10^4\,\mathrm{V/m}

Force on the proton:

F=qE=(1.6×1019)(2.0×104)=3.2×1015NF = qE = (1.6 \times 10^{-19})(2.0 \times 10^4) = 3.2 \times 10^{-15}\,\mathrm{N}

Acceleration:

a=Fmp=3.2×10151.67×1027=1.92×1012m/s2a = \frac{F}{m_p} = \frac{3.2 \times 10^{-15}}{1.67 \times 10^{-27}} = 1.92 \times 10^{12}\,\mathrm{m/s}^2

Time to cross the gap (constant acceleration from rest):

d=12at2    t=2da=2(0.030)1.92×1012=1.77×108sd = \frac{1}{2}at^2 \implies t = \sqrt{\frac{2d}{a}} = \sqrt{\frac{2(0.030)}{1.92 \times 10^{12}}} = 1.77 \times 10^{-8}\,\mathrm{s}

The proton takes approximately 17.7ns17.7\,\mathrm{ns} to cross the gap.

1.4 Motion of Charged Particles in Uniform Electric Fields

Consider a charged particle of mass mm and charge qq entering a uniform electric field EE perpendicular to its initial velocity vv. This is the electric-field analogue of projectile motion.

The particle experiences a constant force perpendicular to its motion:

F = qE \implies a = \frac`\{qE}`{m}

Since the acceleration is perpendicular to the initial velocity, the motion decomposes into:

Parallel to plates (no force, constant velocity):

x=vtx = v \cdot t

Perpendicular to plates (constant acceleration):

y = \frac{1}{2}\left(\frac`\{qE}`{m}\right)t^2

Eliminating tt yields the parabolic trajectory:

y = \frac`\{qE}`{2mv^2}\,x^2

The deflection angle upon exiting the field region is:

\tan\theta = \frac{v_y}{v_x} = \frac`\{qEL}`{mv^2}

where LL is the length of the plates.

:::tip[Electron vs Proton Deflection] For the same field and entry speed, a proton is deflected mp/me1836m_p/m_e \approx 1836 times less than an electron. The direction of deflection is opposite for opposite charges. :::

Worked Example: Electron Deflection Between Parallel Plates

An electron enters the region between two horizontal parallel plates at v=3.0×107m/sv = 3.0 \times 10^7 \mathrm{ m/s} horizontally. The plates are 5.0cm5.0\mathrm{ cm} long and 2.0cm2.0\mathrm{ cm} apart, with a potential difference of 400V400\mathrm{ V} across them.

Find the vertical deflection at the point of exit.

The uniform electric field is:

E=Vd=4000.020=2.0×104V/mE = \frac{V}{d} = \frac{400}{0.020} = 2.0 \times 10^4 \mathrm{ V/m}

Time between the plates:

t=Lv=0.0503.0×107=1.67×109st = \frac{L}{v} = \frac{0.050}{3.0 \times 10^7} = 1.67 \times 10^{-9}\mathrm{ s}

Vertical acceleration (note: the electron has charge q=1.6×1019Cq = -1.6 \times 10^{-19}\mathrm{ C}; it is deflected toward the positive plate):

a = \frac`\{eE}`{m_e} = \frac{(1.6 \times 10^{-19})(2.0 \times 10^4)}{9.11 \times 10^{-31}} = 3.51 \times 10^{15}\mathrm{ m/s}^2

Vertical deflection:

y=12at2=12(3.51×1015)(1.67×109)2=4.9×103m=4.9mmy = \frac{1}{2}at^2 = \frac{1}{2}(3.51 \times 10^{15})(1.67 \times 10^{-9})^2 = 4.9 \times 10^{-3}\mathrm{ m} = 4.9\mathrm{ mm}

The electron deflects 4.9mm4.9\mathrm{ mm} toward the positive plate. Since y=4.9mmy = 4.9\mathrm{ mm} is less than the half-separation of 10mm10\mathrm{ mm}, the electron exits the plates without striking them.


2. Electric Current

2.1 Defining Current

Electric current is the rate of flow of charge through a cross-section of a conductor:

I=ΔQΔtI = \frac{\Delta Q}{\Delta t}

The SI unit is the ampere (A\mathrm{A}), where 1A=1Cs11\mathrm{ A} = 1\mathrm{ C s}^{-1}. Conventional current flows from positive to negative terminal, opposite to the drift direction of electrons.

2.2 Derivation of I=nAevdI = nAev_d

This is a fundamental derivation that connects microscopic charge carrier behaviour to the macroscopic observable we call current.

Consider a cylindrical conductor of cross-sectional area AA. The free electron number density is nn (number of free electrons per unit volume). Each electron carries charge e=1.60×1019Ce = 1.60 \times 10^{-19}\mathrm{ C} and drifts with velocity vdv_d.

In time Δt\Delta t, the volume swept by electrons crossing a given cross-section is:

Volume=AvdΔt\mathrm{Volume} = A \cdot v_d \cdot \Delta t

The number of free electrons in this volume:

N=nAvdΔtN = n \cdot A \cdot v_d \cdot \Delta t

Total charge crossing the cross-section in Δt\Delta t:

ΔQ=Ne=nAevdΔt\Delta Q = N \cdot e = nAev_d\,\Delta t

Therefore:

I=ΔQΔt=nAevdI = \frac{\Delta Q}{\Delta t} = nAev_d

:::info[Typical Values] For copper, n8.5×1028m3n \approx 8.5 \times 10^{28}\mathrm{ m}^{-3}. For a 1mm21\mathrm{ mm}^2 copper wire carrying 1A1\mathrm{ A}, the drift velocity is:

v_d = \frac{I}`\{nAe}` = \frac{1.0}{(8.5 \times 10^{28})(10^{-6})(1.6 \times 10^{-19})} \approx 7.4 \times 10^{-5}\mathrm{ m/s}

This is extraordinarily slow. The signal (the electric field) propagates at a significant fraction of cc, but the electrons themselves crawl. :::

Worked Example: Drift Velocity in Aluminium

An aluminium wire of diameter 0.50mm0.50\mathrm{ mm} carries a current of 2.0A2.0\mathrm{ A}. For aluminium, the free electron density is n=6.0×1028m3n = 6.0 \times 10^{28}\mathrm{ m}^{-3}.

Cross-sectional area:

A=πr2=π(0.25×103)2=1.96×107m2A = \pi r^2 = \pi(0.25 \times 10^{-3})^2 = 1.96 \times 10^{-7}\mathrm{ m}^2

Drift velocity:

v_d = \frac{I}`\{nAe}` = \frac{2.0}{(6.0 \times 10^{28})(1.96 \times 10^{-7})(1.6 \times 10^{-19})} = 1.06 \times 10^{-3}\mathrm{ m/s}

The drift velocity is approximately 1.1mm/s1.1\mathrm{ mm/s}.

Worked Example: Charge Flow and Current

A lamp passes a current of 0.5A0.5\,\mathrm{A} for 22 minutes.

Find the total charge that flows and the number of electrons transferred.

Total charge:

Q=It=0.5×120=60CQ = It = 0.5 \times 120 = 60\,\mathrm{C}

Number of electrons:

ne=Qe=601.6×1019=3.75×1020n_e = \frac{Q}{e} = \frac{60}{1.6 \times 10^{-19}} = 3.75 \times 10^{20}

2.3 Potential Difference and Electromotive Force

Potential difference (VV, or p.d.) is the energy transferred per unit charge between two points in a circuit:

V=WQV = \frac{W}{Q}

SI unit: volt (V\mathrm{V}), where 1V=1JC11\mathrm{ V} = 1\mathrm{ J C}^{-1}.

Electromotive force (ε\varepsilon, or emf) is the energy converted from other forms to electrical energy per unit charge by a source:

ε=WQ\varepsilon = \frac{W}{Q}

Although emf has the same unit as potential difference, they are physically distinct. Emf describes energy conversion within the source (chemical to electrical, for instance), while p.d. describes energy transfer to components in the external circuit.


3. Resistance and Ohm's Law

3.1 Ohm's Law

For an ohmic conductor at constant temperature, the current through the conductor is directly proportional to the potential difference across it:

V=IRV = IR

where RR is the resistance measured in ohms (Ω\Omega), with 1Ω=1VA11\,\Omega = 1\mathrm{ V A}^{-1}.

Ohm's law is an empirical relationship. It holds for metallic conductors at constant temperature. It is not a universal law of nature — many materials and devices are non-ohmic.

3.2 Resistivity

The resistance of a uniform conductor depends on its geometry and the intrinsic property of the material called resistivity (ρ\rho):

R=ρLAR = \rho\frac{L}{A}

where LL is the length and AA is the cross-sectional area. The SI unit of resistivity is Ωm\Omega\,\mathrm{m}.

The inverse quantity is conductivity: σ=1/ρ\sigma = 1/\rho, with SI unit Sm1\mathrm{S m}^{-1} (siemens per metre).

:::info[Data Booklet Resistivity Values] Copper: ρ1.7×108Ωm\rho \approx 1.7 \times 10^{-8}\,\Omega\,\mathrm{m}. Nichrome (alloy): ρ1.1×106Ωm\rho \approx 1.1 \times 10^{-6}\,\Omega\,\mathrm{m}. Semiconductors: ρ\rho spans many orders of magnitude. :::

3.3 Factors Affecting Resistance

Temperature. For metallic conductors, resistance increases approximately linearly with temperature (for modest ranges):

RT=R0[1+α(TT0)]R_T = R_0[1 + \alpha(T - T_0)]

where α\alpha is the temperature coefficient of resistance. For copper, α3.9×103K1\alpha \approx 3.9 \times 10^{-3}\mathrm{ K}^{-1}. The physical mechanism is that lattice vibrations (phonons) increase with temperature, scattering conduction electrons more frequently and reducing their mean free path.

For semiconductors, resistance decreases with temperature because more charge carriers are promoted across the band gap into the conduction band.

Material. Different materials have vastly different resistivities. Conductors (ρ<104Ωm\rho \lt 10^{-4}\,\Omega\,\mathrm{m}), semiconductors (ρ\rho between roughly 10410^{-4} and 106Ωm10^{6}\,\Omega\,\mathrm{m}), and insulators (ρ>106Ωm\rho \gt 10^{6}\,\Omega\,\mathrm{m}) form a continuum.

Worked Example: Resistance and Resistivity

A nichrome wire has length 2.5m2.5\,\mathrm{m} and diameter 0.40mm0.40\,\mathrm{mm}. The resistivity of nichrome is ρ=1.1×106Ωm\rho = 1.1 \times 10^{-6}\,\Omega\,\mathrm{m}.

Find the resistance of the wire.

Cross-sectional area:

A=πd24=π(0.40×103)24=1.26×107m2A = \frac{\pi d^2}{4} = \frac{\pi(0.40 \times 10^{-3})^2}{4} = 1.26 \times 10^{-7}\,\mathrm{m}^2

Resistance:

R=ρLA=(1.1×106)2.51.26×107=21.8ΩR = \rho\frac{L}{A} = (1.1 \times 10^{-6})\frac{2.5}{1.26 \times 10^{-7}} = 21.8\,\Omega

If the wire is stretched to twice its original length (keeping volume constant), what is the new resistance?

When the wire is stretched, volume is conserved: A1L1=A2L2A_1 L_1 = A_2 L_2. If L2=2L1L_2 = 2L_1, then A2=A1/2A_2 = A_1/2.

R2=ρL2A2=ρ2L1A1/2=4ρL1A1=4R1=87.2ΩR_2 = \rho\frac{L_2}{A_2} = \rho\frac{2L_1}{A_1/2} = 4\rho\frac{L_1}{A_1} = 4R_1 = 87.2\,\Omega

Doubling the length quadruples the resistance.

Geometry. Longer conductors have greater resistance (more scattering centres along the path). Thicker conductors have lower resistance (more parallel conduction channels).

3.4 I-V Characteristics

The I-V graph reveals whether a component is ohmic and provides insight into the underlying physics.

Ohmic conductors. A straight line through the origin with constant slope 1/R1/R. Metallic wires at constant temperature behave this way.

Filament lamp. The I-V curve is a steepening curve (non-linear). As current increases, the filament heats up, increasing its resistance. At higher temperatures, the lattice vibrations intensify, and the gradient of the I-V graph increases (more voltage needed per ampere). The curve is symmetric about the origin.

Semiconductor diode. The I-V curve is highly asymmetric. In forward bias (positive voltage across the diode in the direction of easy current flow), negligible current flows until the threshold voltage is reached (approximately 0.7V0.7\mathrm{ V} for silicon diodes), after which current rises steeply. In reverse bias, only a tiny leakage current flows until breakdown occurs.

Thermistor. An NTC (negative temperature coefficient) thermistor has a resistance that decreases as temperature increases. As more current flows, self-heating reduces resistance, so the I-V curve is a shallowing curve (opposite behaviour to a filament lamp).

Light-dependent resistor (LDR). Resistance decreases with increasing light intensity. More photons promote more electrons into the conduction band, increasing the number of charge carriers.

3.5 Common Pitfalls: Resistance

A frequent error is assuming Ohm's law applies universally. Ohm's law is a property of specific materials under specific conditions (constant temperature), not a fundamental law. A filament lamp obeying V=IRV = IR at every instant (with RR varying) does not satisfy Ohm's law, because Ohm's law requires RR to be constant.

Another pitfall is confusing resistance with resistivity. Resistance depends on both the material and the geometry; resistivity is an intrinsic property of the material alone.


4. Circuit Analysis

Circuit Construction Kit: DC

Build series and parallel circuits with resistors, light bulbs, and switches. Measure current and voltage at different points to verify Kirchhoff's laws and Ohm's law.

4.1 Series Circuits

For components connected in series, the same current flows through each component. The total resistance is the sum of individual resistances:

Rtotal=R1+R2+R3+R_{\mathrm{total}} = R_1 + R_2 + R_3 + \cdots

The total p.d. is distributed among components in proportion to their resistances:

Vtotal=V1+V2+V3+V_{\mathrm{total}} = V_1 + V_2 + V_3 + \cdots

For two resistors in series, the voltage divider relationship gives:

V1=VtotalR1R1+R2V_1 = V_{\mathrm{total}} \cdot \frac{R_1}{R_1 + R_2}

4.2 Parallel Circuits

For components connected in parallel, the p.d. across each branch is the same. The reciprocal of the total resistance equals the sum of reciprocals:

1Rtotal=1R1+1R2+1R3+\frac{1}{R_{\mathrm{total}}} = \frac{1}{R_1} + \frac{1}{R_2} + \frac{1}{R_3} + \cdots

For two resistors in parallel:

Rtotal=R1R2R1+R2R_{\mathrm{total}} = \frac{R_1 R_2}{R_1 + R_2}

The total current splits between branches in inverse proportion to their resistances:

I1I2=R2R1\frac{I_1}{I_2} = \frac{R_2}{R_1}
Worked Example: Parallel and Series Combinations

A 6Ω6\,\Omega and a 12Ω12\,\Omega resistor are connected in parallel, and this combination is connected in series with a 4Ω4\,\Omega resistor across a 24V24\,\mathrm{V} supply.

Find the total resistance, the current from the supply, and the p.d. across each component.

Parallel combination:

Rpar=6×126+12=7218=4ΩR_{\mathrm{par}} = \frac{6 \times 12}{6 + 12} = \frac{72}{18} = 4\,\Omega

Total resistance:

Rtotal=Rpar+4=4+4=8ΩR_{\mathrm{total}} = R_{\mathrm{par}} + 4 = 4 + 4 = 8\,\Omega

Current from the supply:

I=VRtotal=248=3.0AI = \frac{V}{R_{\mathrm{total}}} = \frac{24}{8} = 3.0\,\mathrm{A}

P.d. across the series resistor:

Vseries=IR=3.0×4=12VV_{\mathrm{series}} = IR = 3.0 \times 4 = 12\,\mathrm{V}

P.d. across the parallel combination (same as p.d. across each parallel branch):

Vpar=2412=12VV_{\mathrm{par}} = 24 - 12 = 12\,\mathrm{V}

Current through the 6Ω6\,\Omega resistor: I6=12/6=2.0AI_6 = 12/6 = 2.0\,\mathrm{A}

Current through the 12Ω12\,\Omega resistor: I12=12/12=1.0AI_{12} = 12/12 = 1.0\,\mathrm{A}

Check: I6+I12=2.0+1.0=3.0AI_6 + I_{12} = 2.0 + 1.0 = 3.0\,\mathrm{A} (matches supply current).

4.3 Kirchhoff's Laws

Kirchhoff's two laws are conservation statements that allow systematic analysis of any circuit.

Kirchhoff's Current Law (KCL) — the Junction Rule. The sum of currents entering any junction equals the sum of currents leaving it. This is conservation of charge:

Iin=Iout\sum I_{\mathrm{in}} = \sum I_{\mathrm{out}}

Kirchhoff's Voltage Law (KVL) — the Loop Rule. The sum of all potential differences around any closed loop is zero. This is conservation of energy:

V=0\sum V = 0

When applying KVL, adopt a consistent sign convention. A common convention: assign a sign based on whether you encounter a potential rise or drop as you traverse the loop. Emf is a rise (positive), and potential drops across resistors are negative.

Worked Example: Kirchhoff's Laws

Consider a circuit with two cells and three resistors. Cell 1 has emf ε1=12V\varepsilon_1 = 12\mathrm{ V} and cell 2 has emf ε2=6V\varepsilon_2 = 6\mathrm{ V} (opposing). The resistors are R1=4ΩR_1 = 4\,\Omega, R2=6ΩR_2 = 6\,\Omega, and R3=2ΩR_3 = 2\,\Omega, all in series with the cells.

Applying KVL around the single loop (travelling clockwise):

ε1ε2IR1IR2IR3=0\varepsilon_1 - \varepsilon_2 - IR_1 - IR_2 - IR_3 = 0126I(4)I(6)I(2)=012 - 6 - I(4) - I(6) - I(2) = 06=12I6 = 12II=0.50AI = 0.50\mathrm{ A}

The p.d. across each resistor: V1=2.0VV_1 = 2.0\mathrm{ V}, V2=3.0VV_2 = 3.0\mathrm{ V}, V3=1.0VV_3 = 1.0\mathrm{ V}. These sum to 6V6\mathrm{ V}, which equals the net emf of 126=6V12 - 6 = 6\mathrm{ V}, confirming energy conservation.

4.4 The Potential Divider

A potential divider (or voltage divider) consists of two or more resistors in series across a supply. The output voltage is tapped from the junction between resistors.

For two resistors R1R_1 (upper) and R2R_2 (lower) across supply VinV_{\mathrm{in}}:

Vout=VinR2R1+R2V_{\mathrm{out}} = V_{\mathrm{in}} \cdot \frac{R_2}{R_1 + R_2}

If R2R_2 is replaced by a variable component (thermistor, LDR), the output voltage becomes a function of the physical quantity being sensed.

Sensing circuits. An NTC thermistor in the lower position produces a p.d. that rises with temperature (since R2R_2 falls, but more current flows, and the voltage drop across the upper fixed resistor increases, so VoutV_{\mathrm{out}} measured across R2R_2 actually decreases). Careful analysis is needed depending on which component the output is measured across.

A common configuration places the variable resistor (e.g., thermistor) as R1R_1 and measures VoutV_{\mathrm{out}} across R2R_2 (fixed). As temperature rises, R1R_1 decreases, so more of VinV_{\mathrm{in}} drops across R2R_2, and VoutV_{\mathrm{out}} increases.

Worked Example: Potential Divider with Thermistor

A potential divider consists of a 10kΩ10\,\mathrm{k}\Omega fixed resistor (R1R_1) and an NTC thermistor (R2R_2) connected across a 9.0V9.0\,\mathrm{V} supply. The output is measured across the thermistor. At 20C20^\circ\mathrm{C}, the thermistor has resistance 5.0kΩ5.0\,\mathrm{k}\Omega; at 60C60^\circ\mathrm{C}, its resistance is 1.0kΩ1.0\,\mathrm{k}\Omega.

Find the output voltage at each temperature.

At 20C20^\circ\mathrm{C}:

Vout=9.0×5.010+5.0=9.0×13=3.0VV_{\mathrm{out}} = 9.0 \times \frac{5.0}{10 + 5.0} = 9.0 \times \frac{1}{3} = 3.0\,\mathrm{V}

At 60C60^\circ\mathrm{C}:

Vout=9.0×1.010+1.0=9.0×1110.82VV_{\mathrm{out}} = 9.0 \times \frac{1.0}{10 + 1.0} = 9.0 \times \frac{1}{11} \approx 0.82\,\mathrm{V}

As temperature increases, the thermistor resistance drops and so does the output voltage across it. The p.d. across the fixed resistor increases from 6.0V6.0\,\mathrm{V} to 8.18V8.18\,\mathrm{V}.

4.5 Wheatstone Bridge

The Wheatstone bridge is a null-detection arrangement of four resistors:

R1R2=R3R4\frac{R_1}{R_2} = \frac{R_3}{R_4}

When this ratio is satisfied, no current flows through the galvanometer connected between the junctions. This condition is used for precise resistance measurement.

If three resistors are known and one is unknown, balance the bridge and solve:

Rx=R2R3R1R_x = R_2 \cdot \frac{R_3}{R_1}

The sensitivity of the bridge is greatest when all four arms have similar resistances.

Worked Example: Wheatstone Bridge

A Wheatstone bridge has R1=100ΩR_1 = 100\,\Omega, R2=200ΩR_2 = 200\,\Omega, and R3=150ΩR_3 = 150\,\Omega. The unknown resistor RxR_x is in the fourth arm. The galvanometer reads zero.

At balance:

R1R2=R3Rx\frac{R_1}{R_2} = \frac{R_3}{R_x}100200=150Rx\frac{100}{200} = \frac{150}{R_x}Rx=200×150100=300ΩR_x = \frac{200 \times 150}{100} = 300\,\Omega

4.6 Common Pitfalls: Circuit Analysis

A common mistake when applying Kirchhoff's voltage law is inconsistent sign conventions. Always define your traversal direction first, then apply signs consistently. Another error is forgetting that the voltage across parallel branches is identical, not the current.

When analysing potential dividers, students often confuse which resistor the output is measured across. Always identify the output terminals clearly before calculating.


5. Internal Resistance

5.1 EMF and Terminal Potential Difference

A real cell has internal resistance rr due to the resistance of the electrolyte, electrodes, and internal connections. The terminal p.d. (VV) is less than the emf (ε\varepsilon) when current is drawn:

V=εIrV = \varepsilon - Ir

When no current flows (open circuit), V=εV = \varepsilon. The terminal p.d. decreases linearly with increasing current.

The "lost volts" is the p.d. across the internal resistance: Vlost=IrV_{\mathrm{lost}} = Ir.

5.2 Measuring Internal Resistance

Method 1: Vary the external load. Connect a variable resistor across the cell. Measure the terminal p.d. VV and current II for a range of load resistances. Plot VV against II.

The graph is a straight line: V=εIrV = \varepsilon - Ir.

The y-intercept equals ε\varepsilon. The gradient equals r-r (so r=gradientr = |\mathrm{gradient}|).

The x-intercept gives the short-circuit current Isc=ε/rI_{\mathrm{sc}} = \varepsilon / r.

Method 2: Two-reading method. Measure V1V_1 and I1I_1 for one load, and V2V_2 and I2I_2 for another. Solve simultaneously:

V1=εI1rV_1 = \varepsilon - I_1 r V2=εI2rV_2 = \varepsilon - I_2 r

Subtracting: V1V2=(I2I1)rV_1 - V_2 = (I_2 - I_1)r, giving r=(V1V2)/(I2I1)r = (V_1 - V_2)/(I_2 - I_1).

Worked Example: Internal Resistance

A cell with unknown emf and internal resistance is connected to a 4.0Ω4.0\,\Omega resistor. The terminal p.d. is measured as 5.8V5.8\mathrm{ V} and the current is 1.2A1.2\mathrm{ A}.

Using V=εIrV = \varepsilon - Ir:

ε=V+Ir=5.8+(1.2)r\varepsilon = V + Ir = 5.8 + (1.2)r

When the external resistor is changed to 9.0Ω9.0\,\Omega, the current becomes 0.65A0.65\mathrm{ A}:

V=εIr=(5.8+1.2r)0.65r=5.8+0.55rV' = \varepsilon - I'r = (5.8 + 1.2r) - 0.65r = 5.8 + 0.55r

But also V=IR=0.65×9.0=5.85VV' = I'R' = 0.65 \times 9.0 = 5.85\mathrm{ V}:

5.85=5.8+0.55r5.85 = 5.8 + 0.55rr=0.050.55=0.091Ωr = \frac{0.05}{0.55} = 0.091\,\Omegaε=5.8+1.2(0.091)=5.91V\varepsilon = 5.8 + 1.2(0.091) = 5.91\mathrm{ V}

5.3 Maximum Power Transfer Theorem

The power delivered to the external load RLR_L is:

P=I2RL=(εRL+r)2RL=ε2RL(RL+r)2P = I^2 R_L = \left(\frac{\varepsilon}{R_L + r}\right)^2 R_L = \frac{\varepsilon^2 R_L}{(R_L + r)^2}

To find the maximum, differentiate with respect to RLR_L and set to zero:

\frac`\{dP}`{dR_L} = \varepsilon^2 \frac{(R_L + r)^2 - 2R_L(R_L + r)}{(R_L + r)^4} = 0

The numerator simplifies to (RL+r)(rRL)(R_L + r)(r - R_L), giving RL=rR_L = r.

Maximum power is delivered to the load when the load resistance equals the internal resistance. At this condition:

Pmax=ε24rP_{\max} = \frac{\varepsilon^2}{4r}

:::warning[Efficiency at Maximum Power] At RL=rR_L = r, the efficiency is only 50% (half the power is dissipated in the internal resistance). In power distribution systems, RL>rR_L \gt r is preferred for higher efficiency, even though less total power is delivered. :::

5.4 Battery Configurations

Series. Identical cells in series: total emf adds, total internal resistance adds.

εtotal=nε,rtotal=nr\varepsilon_{\mathrm{total}} = n\varepsilon, \quad r_{\mathrm{total}} = nr

where nn is the number of cells.

Parallel. Identical cells in parallel: total emf equals that of one cell, total internal resistance decreases.

εtotal=ε,rtotal=rn\varepsilon_{\mathrm{total}} = \varepsilon, \quad r_{\mathrm{total}} = \frac{r}{n}

Parallel configuration provides the same voltage but can deliver nn times the current of a single cell.

Mixed (series-parallel) banks. For nn rows of mm cells each (all identical):

\varepsilon_{\mathrm{total}} = m\varepsilon, \quad r_{\mathrm{total}} = \frac`\{mr}`{n}

The configuration is chosen based on whether the load requires higher voltage (more cells in series) or higher current capacity (more cells in parallel).

Worked Example: Battery Configurations

Six identical cells, each with emf 1.5V1.5\,\mathrm{V} and internal resistance 0.5Ω0.5\,\Omega, are connected to a 3.0Ω3.0\,\Omega external load.

Compare the current when the cells are (a) all in series, (b) two rows of three in series.

(a) All six in series:

εtotal=6(1.5)=9.0V,rtotal=6(0.5)=3.0Ω\varepsilon_{\mathrm{total}} = 6(1.5) = 9.0\,\mathrm{V}, \quad r_{\mathrm{total}} = 6(0.5) = 3.0\,\Omega

I=9.03.0+3.0=1.5AI = \frac{9.0}{3.0 + 3.0} = 1.5\,\mathrm{A}

(b) Two rows of three (3 series, 2 parallel):

εtotal=3(1.5)=4.5V,rtotal=3(0.5)2=0.75Ω\varepsilon_{\mathrm{total}} = 3(1.5) = 4.5\,\mathrm{V}, \quad r_{\mathrm{total}} = \frac{3(0.5)}{2} = 0.75\,\Omega

I=4.53.0+0.75=4.53.75=1.2AI = \frac{4.5}{3.0 + 0.75} = \frac{4.5}{3.75} = 1.2\,\mathrm{A}

The series arrangement delivers more current to this particular load because the higher voltage outweighs the increased internal resistance.


6. Power in Circuits

6.1 Power Equations

Electrical power is the rate of energy transfer:

P=IVP = IV

Using Ohm's law (V=IRV = IR), two equivalent forms follow:

P=I2RP = I^2 R P=V2RP = \frac{V^2}{R}

These are all algebraically equivalent for ohmic conductors. The form to use depends on what is held constant in the problem. If current is constant (series circuit), use P=I2RP = I^2 R. If voltage is constant (parallel circuit), use P=V2/RP = V^2/R.

6.2 Energy Dissipated

The energy dissipated by a resistor over time tt is:

E=Pt=IVt=I2Rt=V2RtE = Pt = IVt = I^2 Rt = \frac{V^2}{R}t

This energy appears as thermal energy in the resistor (Joule heating).

6.3 Power and Internal Resistance

The total power output of a cell is:

Ptotal=εIP_{\mathrm{total}} = \varepsilon I

The power delivered to the external circuit:

Pext=VI=I2RLP_{\mathrm{ext}} = VI = I^2 R_L

The power wasted in the internal resistance:

Pint=I2rP_{\mathrm{int}} = I^2 r

Conservation of energy requires Ptotal=Pext+PintP_{\mathrm{total}} = P_{\mathrm{ext}} + P_{\mathrm{int}}.

The efficiency of the cell:

η=PextPtotal=RLRL+r\eta = \frac{P_{\mathrm{ext}}}{P_{\mathrm{total}}} = \frac{R_L}{R_L + r}
Worked Example: Power Transfer

A battery with emf 12V12\mathrm{ V} and internal resistance 2.0Ω2.0\,\Omega is connected to an external resistor of 4.0Ω4.0\,\Omega.

Current:

I=εRL+r=124.0+2.0=2.0AI = \frac{\varepsilon}{R_L + r} = \frac{12}{4.0 + 2.0} = 2.0\mathrm{ A}

Power to external resistor:

Pext=I2RL=(2.0)2(4.0)=16WP_{\mathrm{ext}} = I^2 R_L = (2.0)^2(4.0) = 16\mathrm{ W}

Power wasted internally:

Pint=I2r=(2.0)2(2.0)=8WP_{\mathrm{int}} = I^2 r = (2.0)^2(2.0) = 8\mathrm{ W}

Total power: Ptotal=16+8=24WP_{\mathrm{total}} = 16 + 8 = 24\mathrm{ W}.

Check: Ptotal=εI=12×2.0=24WP_{\mathrm{total}} = \varepsilon I = 12 \times 2.0 = 24\mathrm{ W}.

Efficiency: η=4.0/(4.0+2.0)=66.7%\eta = 4.0/(4.0 + 2.0) = 66.7\%.

6.4 Common Pitfalls: Power

A critical error is using P=V2/RP = V^2/R when VV refers to the terminal p.d. of a cell (which differs from the emf due to internal resistance) and RR refers to the external load. Always be explicit about which voltage and which resistance you are using. If the problem involves internal resistance, track the terminal p.d. separately from the emf.

Another mistake is confusing power (rate of energy transfer, watts) with energy (joules). To find total energy transferred, always multiply power by time.


7. Measuring Instruments

7.1 Ideal vs Real Instruments

Ammeter. Measures current. Connected in series with the component. An ideal ammeter has zero resistance so it does not alter the current it measures. A real ammeter has a small but finite resistance (typically a fraction of an ohm for analogue, or a very small resistance for digital meters based on shunt resistors).

Voltmeter. Measures potential difference. Connected in parallel across the component. An ideal voltmeter has infinite resistance so it draws no current from the circuit. A real voltmeter has a large but finite resistance (typically 10410^4 to 107Ω10^7\,\Omega).

7.2 Impact of Non-Ideal Instruments

A non-ideal ammeter in series adds its resistance to the circuit, reducing the current below the true value. The measured current is:

Imeasured=εR+RA+rI_{\mathrm{measured}} = \frac{\varepsilon}{R + R_A + r}

which is less than the true current Itrue=ε/(R+r)I_{\mathrm{true}} = \varepsilon/(R + r).

A non-ideal voltmeter in parallel acts as an additional current path, effectively reducing the resistance of the component being measured. The equivalent resistance of the parallel combination is:

Req=RRVR+RVR_{\mathrm{eq}} = \frac{R \cdot R_V}{R + R_V}

which is always less than RR. The measured p.d. is lower than the true p.d.

:::tip[Minimising Measurement Error] For ammeters: use instruments with the smallest possible internal resistance. For voltmeters: use instruments with the largest possible internal resistance. A voltmeter is considered sufficiently ideal if RV>100RR_V \gt 100R, where RR is the resistance across which it is connected. :::

7.3 Galvanometer as Ammeter and Voltmeter

A galvanometer is a sensitive current-measuring device. A typical galvanometer might have a full-scale deflection current Ig=100μAI_g = 100\,\mu\mathrm{A} and internal resistance Rg=50ΩR_g = 50\,\Omega.

Converting to ammeter. A shunt resistor RsR_s is connected in parallel to bypass excess current:

Rs=IgRgIIgR_s = \frac{I_g R_g}{I - I_g}

For a galvanometer to measure up to I=1AI = 1\mathrm{ A}: Rs=(100×106×50)/(1100×106)5.0×103ΩR_s = (100 \times 10^{-6} \times 50)/(1 - 100 \times 10^{-6}) \approx 5.0 \times 10^{-3}\,\Omega.

Converting to voltmeter. A multiplier resistor RmR_m is connected in series to limit current:

Rm=VIgRgR_m = \frac{V}{I_g} - R_g

For a galvanometer to measure up to V=10VV = 10\mathrm{ V}: Rm=10/(100×106)50=99950Ω100kΩR_m = 10/(100 \times 10^{-6}) - 50 = 99950\,\Omega \approx 100\,\mathrm{k}\Omega.

Worked Example: Converting a Galvanometer to an Ammeter

A galvanometer has full-scale deflection current Ig=50μAI_g = 50\,\mu\mathrm{A} and internal resistance Rg=100ΩR_g = 100\,\Omega.

Find the shunt resistor needed for an ammeter measuring up to 5A5\,\mathrm{A}.

Using the shunt resistor formula:

Rs=IgRgIIg=(50×106)(100)550×1065.0×1035.0=1.0×103ΩR_s = \frac{I_g R_g}{I - I_g} = \frac{(50 \times 10^{-6})(100)}{5 - 50 \times 10^{-6}} \approx \frac{5.0 \times 10^{-3}}{5.0} = 1.0 \times 10^{-3}\,\Omega

The shunt resistor is 1.0mΩ1.0\,\mathrm{m}\Omega -- a very small resistance, as expected for an ammeter that must carry large currents while bypassing the sensitive galvanometer.


8. Cells and Batteries: Deeper Analysis

8.1 EMF as Energy per Charge

The emf of a cell is the total energy converted per unit charge:

ε=EchemicalQ\varepsilon = \frac{E_{\mathrm{chemical}}}{Q}

For a cell that converts EchemicalE_{\mathrm{chemical}} joules of chemical energy when QQ coulombs of charge flow, the emf is ε=Echemical/Q\varepsilon = E_{\mathrm{chemical}}/Q.

A rechargeable cell can reverse this process: during charging, electrical energy is converted back to chemical energy. The charging voltage must exceed the emf to drive current through the cell against its emf.

8.2 Discharge Characteristics

As a battery discharges, its emf gradually decreases and its internal resistance increases. This is because the concentration of reactants decreases and reaction products accumulate, affecting the electrochemistry at the electrodes.

For a lead-acid battery, the emf drops from about 12.6V12.6\mathrm{ V} (fully charged) to approximately 11.9V11.9\mathrm{ V} (discharged), while internal resistance can increase by an order of magnitude.

8.3 Combining Cells with Different EMFs

When cells with different emfs are connected in parallel, current can circulate between them even with no external load. This is generally avoided in practice unless a diode is used to prevent reverse current.

For cells in series, the total emf is the algebraic sum (taking polarity into account), and the total internal resistance is the sum of individual internal resistances regardless of polarity.


9. Systematic Circuit Analysis: A Framework

When faced with an arbitrary circuit, apply the following systematic approach:

  1. Label all known and unknown quantities (currents, voltages, resistances, emfs).
  2. Assign current directions (if the actual direction is unknown, assume one; a negative result indicates the current flows in the opposite direction).
  3. Apply KCL at each junction to write current equations.
  4. Apply KVL around each independent loop to write voltage equations.
  5. Solve the resulting system of simultaneous equations.

This method works for any circuit topology, regardless of complexity.

Worked Example: Multi-Loop Circuit

Two cells are connected in parallel across a common load. Cell 1 has ε1=12V\varepsilon_1 = 12\mathrm{ V}, r1=1.0Ωr_1 = 1.0\,\Omega. Cell 2 has ε2=10V\varepsilon_2 = 10\mathrm{ V}, r2=2.0Ωr_2 = 2.0\,\Omega. The load resistor is RL=5.0ΩR_L = 5.0\,\Omega.

Let I1I_1 be the current from cell 1, I2I_2 from cell 2, and ILI_L through the load (all assumed clockwise through the load).

KCL at the top junction: I1+I2=ILI_1 + I_2 = I_L.

KVL around loop 1 (cell 1, load): ε1I1r1ILRL=0\varepsilon_1 - I_1 r_1 - I_L R_L = 0, giving 12I15IL=012 - I_1 - 5I_L = 0, so I1=125ILI_1 = 12 - 5I_L.

KVL around loop 2 (cell 2, load): ε2I2r2ILRL=0\varepsilon_2 - I_2 r_2 - I_L R_L = 0, giving 102I25IL=010 - 2I_2 - 5I_L = 0, so I2=52.5ILI_2 = 5 - 2.5I_L.

Substituting into KCL: (125IL)+(52.5IL)=IL(12 - 5I_L) + (5 - 2.5I_L) = I_L.

177.5IL=IL17 - 7.5I_L = I_L17=8.5IL17 = 8.5I_LIL=2.0AI_L = 2.0\mathrm{ A}

Then I1=125(2.0)=2.0AI_1 = 12 - 5(2.0) = 2.0\mathrm{ A} and I2=52.5(2.0)=0AI_2 = 5 - 2.5(2.0) = 0\mathrm{ A}.

In this specific case, cell 2 contributes no current. The terminal p.d. of cell 2 is V2=ε2=10VV_2 = \varepsilon_2 = 10\mathrm{ V} (no current, so no internal drop), which equals the terminal p.d. of cell 1: V1=122.0(1.0)=10VV_1 = 12 - 2.0(1.0) = 10\mathrm{ V}. The p.d. across the load is VL=ILRL=2.0×5.0=10VV_L = I_L R_L = 2.0 \times 5.0 = 10\mathrm{ V}. This is consistent.


10. Resistivity Experiments

10.1 Determining Resistivity Experimentally

To determine the resistivity of a material:

  1. Measure the length LL of the wire with a metre rule.
  2. Measure the diameter with a micrometer screw gauge at several points and average to find cross-sectional area A=πd2/4A = \pi d^2/4.
  3. Connect the wire in a circuit with a variable resistor, ammeter, and voltmeter.
  4. Record VV and II for a range of currents (keeping the current low to minimise heating).
  5. Calculate R=V/IR = V/I for each reading and average.
  6. Compute ρ=RA/L\rho = RA/L.

10.2 Sources of Error

Systematic errors include contact resistance at the clips (use four-terminal sensing for high precision), the assumption of uniform wire diameter, and the ammeter/voltmeter resistance effects discussed in Section 7.2.

Random errors are reduced by taking multiple readings and averaging. Temperature control is critical: even small temperature changes during the experiment alter resistivity.

10.3 I-V Characteristic Experiments

To obtain I-V characteristics:

  1. Connect the component in series with a variable resistor, ammeter, and power supply.
  2. Connect a voltmeter in parallel across the component.
  3. Vary the current and record corresponding VV-II pairs.
  4. Plot II (y-axis) against VV (x-axis) — this is the IB convention.

For a diode, use both forward and reverse bias. In forward bias, include a protective resistor in series to prevent excessive current when the diode conducts.


11. Summary of Key Equations

:::info[IB Physics Data Booklet — Topic 5] The following are the key equations for current electricity found in the IB Physics data booklet:

QuantityEquation
Coulomb's lawF=q1q24πε0r2F = \dfrac{q_1 q_2}{4\pi\varepsilon_0 r^2}
Electric field (point charge)E=q4πε0r2E = \dfrac{q}{4\pi\varepsilon_0 r^2}
Electric field (parallel plates)E=VdE = \dfrac{V}{d}
Current (drift velocity)I=nAevdI = nAev_d
Ohm's lawV=IRV = IR
Resistance and resistivityR=ρLAR = \dfrac{\rho L}{A}
PowerP=IV=I2R=V2RP = IV = I^2R = \dfrac{V^2}{R}
Internal resistanceV=εIrV = \varepsilon - Ir
Potential dividerVout=VinR2R1+R2V_{\mathrm{out}} = V_{\mathrm{in}} \dfrac{R_2}{R_1 + R_2}
Wheatstone bridgeR1R2=R3R4\dfrac{R_1}{R_2} = \dfrac{R_3}{R_4}

:::


12. Common Pitfalls: Consolidated

Sign conventions in KVL. The single most common source of error in circuit problems. Define your loop direction, assign ++ to emf rises and - to potential drops across resistors (or vice versa, as long as you are consistent), and stick to it.

Confusing emf with terminal p.d. Emf is the open-circuit voltage. Terminal p.d. is always less than or equal to emf (for a cell supplying current). The difference is the "lost volts" IrIr.

Assuming all conductors are ohmic. Diodes, thermistors, LDRs, and filament lamps are all non-ohmic. Ohm's law applies only to metallic conductors at constant temperature.

Drift velocity confusion. Electrons drift slowly, but the electric field (and hence the signal) propagates at near light speed. These are completely different phenomena.

Series vs parallel formulas. In series, resistances add directly. In parallel, reciprocals add. Students frequently mix these up. A useful mnemonic: series is "additive" (path is single), parallel is "reciprocal-additive" (paths multiply).

Power formula selection. P=I2RP = I^2 R assumes current is held constant (series). P=V2/RP = V^2/R assumes voltage is held constant (parallel). In circuits with internal resistance, neither may be directly applicable without careful identification of the relevant VV and II.

Ammeter in parallel, voltmeter in series. Connecting an ammeter in parallel creates a short circuit through the ammeter (potentially damaging it). Connecting a voltmeter in series means the circuit is effectively open (the voltmeter's high resistance blocks current). Always connect ammeters in series and voltmeters in parallel.


Problem Set

Problem 1

Two point charges, q1=+3.0nCq_1 = +3.0\,\mathrm{nC} and q2=5.0nCq_2 = -5.0\,\mathrm{nC}, are separated by 0.10m0.10\,\mathrm{m} in a vacuum. Find the magnitude of the electrostatic force between them and state whether it is attractive or repulsive.

Solution

F=kq1q2r2=(8.99×109)(3.0×109)(5.0×109)(0.10)2F = k\frac{|q_1||q_2|}{r^2} = (8.99 \times 10^9)\frac{(3.0 \times 10^{-9})(5.0 \times 10^{-9})}{(0.10)^2}

F=(8.99×109)1.5×10170.010=1.35×105NF = (8.99 \times 10^9)\frac{1.5 \times 10^{-17}}{0.010} = 1.35 \times 10^{-5}\,\mathrm{N}

The force is attractive (opposite charges).

If you get this wrong, revise: Section 1.1 Coulomb's Law.

Problem 2

An electron (me=9.11×1031kgm_e = 9.11 \times 10^{-31}\,\mathrm{kg}, e=1.6×1019Ce = 1.6 \times 10^{-19}\,\mathrm{C}) is suspended stationary between two horizontal parallel plates. The plates are 8.0mm8.0\,\mathrm{mm} apart. Find the potential difference across the plates.

Solution

For the electron to be stationary, the electric force must balance the weight:

eE=meg    E=mege=(9.11×1031)(9.81)1.6×1019=5.59×1011V/meE = m_e g \implies E = \frac{m_e g}{e} = \frac{(9.11 \times 10^{-31})(9.81)}{1.6 \times 10^{-19}} = 5.59 \times 10^{-11}\,\mathrm{V/m}

V=Ed=(5.59×1011)(8.0×103)=4.47×1013VV = Ed = (5.59 \times 10^{-11})(8.0 \times 10^{-3}) = 4.47 \times 10^{-13}\,\mathrm{V}

This is an extremely small voltage -- in practice, the electric force is far too weak to suspend an electron against gravity.

If you get this wrong, revise: Sections 1.3 and 1.4.

Problem 3

A copper wire of length 50m50\,\mathrm{m} and cross-sectional area 1.0mm21.0\,\mathrm{mm}^2 carries a current of 3.0A3.0\,\mathrm{A}. The resistivity of copper is 1.7×108Ωm1.7 \times 10^{-8}\,\Omega\,\mathrm{m}. Calculate the resistance of the wire, the p.d. across it, and the drift velocity of the electrons (n=8.5×1028m3n = 8.5 \times 10^{28}\,\mathrm{m}^{-3}).

Solution

R=ρLA=(1.7×108)501.0×106=0.85ΩR = \rho\frac{L}{A} = (1.7 \times 10^{-8})\frac{50}{1.0 \times 10^{-6}} = 0.85\,\Omega

V=IR=3.0×0.85=2.55VV = IR = 3.0 \times 0.85 = 2.55\,\mathrm{V}

vd=InAe=3.0(8.5×1028)(1.0×106)(1.6×1019)=2.21×104m/sv_d = \frac{I}{nAe} = \frac{3.0}{(8.5 \times 10^{28})(1.0 \times 10^{-6})(1.6 \times 10^{-19})} = 2.21 \times 10^{-4}\,\mathrm{m/s}

The drift velocity is approximately 0.22mm/s0.22\,\mathrm{mm/s}.

If you get this wrong, revise: Sections 2.2 and 3.2.

Problem 4

A cell with emf 12V12\,\mathrm{V} and internal resistance 0.50Ω0.50\,\Omega is connected to two 6.0Ω6.0\,\Omega resistors in parallel. Find the current through each resistor, the terminal p.d., and the power dissipated in the external circuit.

Solution

External resistance:

Rext=6.0×6.06.0+6.0=3.0ΩR_{\mathrm{ext}} = \frac{6.0 \times 6.0}{6.0 + 6.0} = 3.0\,\Omega

Total current:

I=εRext+r=123.0+0.50=123.53.43AI = \frac{\varepsilon}{R_{\mathrm{ext}} + r} = \frac{12}{3.0 + 0.50} = \frac{12}{3.5} \approx 3.43\,\mathrm{A}

Terminal p.d.:

V=εIr=123.43(0.50)=10.29VV = \varepsilon - Ir = 12 - 3.43(0.50) = 10.29\,\mathrm{V}

Current through each 6Ω6\,\Omega resistor (equal since they are identical):

Ieach=I2=1.71AI_{\mathrm{each}} = \frac{I}{2} = 1.71\,\mathrm{A}

Power in external circuit:

Pext=I2Rext=(3.43)2(3.0)=35.3WP_{\mathrm{ext}} = I^2 R_{\mathrm{ext}} = (3.43)^2(3.0) = 35.3\,\mathrm{W}

If you get this wrong, revise: Sections 4.2 and 5.1.

Problem 5

A battery of unknown emf ε\varepsilon and internal resistance rr is connected to a variable resistor. When the external resistance is 8.0Ω8.0\,\Omega, the current is 0.75A0.75\,\mathrm{A}. When the external resistance is 18Ω18\,\Omega, the current is 0.40A0.40\,\mathrm{A}. Find ε\varepsilon and rr.

Solution

ε=I1(R1+r)=0.75(8.0+r)=6.0+0.75r\varepsilon = I_1(R_1 + r) = 0.75(8.0 + r) = 6.0 + 0.75r

ε=I2(R2+r)=0.40(18+r)=7.2+0.40r\varepsilon = I_2(R_2 + r) = 0.40(18 + r) = 7.2 + 0.40r

Setting equal:

6.0+0.75r=7.2+0.40r    0.35r=1.2    r=3.43Ω6.0 + 0.75r = 7.2 + 0.40r \implies 0.35r = 1.2 \implies r = 3.43\,\Omega

ε=6.0+0.75(3.43)=8.57V\varepsilon = 6.0 + 0.75(3.43) = 8.57\,\mathrm{V}

If you get this wrong, revise: Section 5.2.

Problem 6

A potential divider circuit consists of a 2000Ω2000\,\Omega and a 3000Ω3000\,\Omega resistor in series across a 12V12\,\mathrm{V} supply. A voltmeter with resistance 10kΩ10\,\mathrm{k}\Omega is connected across the 3000Ω3000\,\Omega resistor. Find the reading on the voltmeter.

Solution

The voltmeter is in parallel with the 3000Ω3000\,\Omega resistor:

Rparallel=3000×100003000+10000=3.0×10713000=2308ΩR_{\mathrm{parallel}} = \frac{3000 \times 10000}{3000 + 10000} = \frac{3.0 \times 10^7}{13000} = 2308\,\Omega

Total circuit resistance:

Rtotal=2000+2308=4308ΩR_{\mathrm{total}} = 2000 + 2308 = 4308\,\Omega

Current:

I=124308=2.79×103AI = \frac{12}{4308} = 2.79 \times 10^{-3}\,\mathrm{A}

Voltmeter reading (p.d. across parallel combination):

V=IRparallel=(2.79×103)(2308)=6.43VV = IR_{\mathrm{parallel}} = (2.79 \times 10^{-3})(2308) = 6.43\,\mathrm{V}

Without the voltmeter, the ideal reading would be 12×3000/5000=7.20V12 \times 3000/5000 = 7.20\,\mathrm{V}. The non-ideal voltmeter loads the circuit and gives a lower reading.

If you get this wrong, revise: Sections 4.4 and 7.2.

Problem 7

Three identical cells, each with emf 6.0V6.0\,\mathrm{V} and internal resistance 1.0Ω1.0\,\Omega, are connected in series to a 7.0Ω7.0\,\Omega resistor. Calculate the total power output of the cells and the efficiency of power transfer to the external resistor.

Solution

εtotal=3(6.0)=18.0V,rtotal=3(1.0)=3.0Ω\varepsilon_{\mathrm{total}} = 3(6.0) = 18.0\,\mathrm{V}, \quad r_{\mathrm{total}} = 3(1.0) = 3.0\,\Omega

I=18.07.0+3.0=1.8AI = \frac{18.0}{7.0 + 3.0} = 1.8\,\mathrm{A}

Total power:

Ptotal=εI=18.0×1.8=32.4WP_{\mathrm{total}} = \varepsilon I = 18.0 \times 1.8 = 32.4\,\mathrm{W}

Power to external resistor:

Pext=I2R=(1.8)2(7.0)=22.7WP_{\mathrm{ext}} = I^2 R = (1.8)^2(7.0) = 22.7\,\mathrm{W}

Efficiency:

η=RR+r=7.07.0+3.0=70%\eta = \frac{R}{R + r} = \frac{7.0}{7.0 + 3.0} = 70\%

If you get this wrong, revise: Sections 5.4 and 6.3.

Problem 8

In a Wheatstone bridge, R1=100ΩR_1 = 100\,\Omega, R2=200ΩR_2 = 200\,\Omega, and R3=50ΩR_3 = 50\,\Omega. Find the value of the unknown resistance R4R_4 for which the galvanometer reads zero. If R4R_4 is instead 120Ω120\,\Omega, in which direction does current flow through the galvanometer?

Solution

At balance:

R1R2=R3R4    100200=50R4    R4=200×50100=100Ω\frac{R_1}{R_2} = \frac{R_3}{R_4} \implies \frac{100}{200} = \frac{50}{R_4} \implies R_4 = \frac{200 \times 50}{100} = 100\,\Omega

If R4=120ΩR_4 = 120\,\Omega, the bridge is unbalanced. The ratio R3/R4=50/120=0.417R_3/R_4 = 50/120 = 0.417 is less than R1/R2=0.5R_1/R_2 = 0.5, so the p.d. at the R1R_1-R3R_3 junction is higher than at the R2R_2-R4R_4 junction. Current flows from the R1R_1-R3R_3 junction through the galvanometer to the R2R_2-R4R_4 junction.

If you get this wrong, revise: Section 4.5.

Problem 9

A 200W200\,\mathrm{W} lamp is connected to a 240V240\,\mathrm{V} supply. A second identical lamp is connected in parallel. Find the current drawn by each lamp and the total current from the supply.

Solution

Resistance of each lamp:

R=V2P=2402200=288ΩR = \frac{V^2}{P} = \frac{240^2}{200} = 288\,\Omega

Current per lamp:

I=VR=240288=0.833AI = \frac{V}{R} = \frac{240}{288} = 0.833\,\mathrm{A}

Total current (two identical lamps in parallel):

Itotal=2×0.833=1.67AI_{\mathrm{total}} = 2 \times 0.833 = 1.67\,\mathrm{A}

Total power: Ptotal=2×200=400WP_{\mathrm{total}} = 2 \times 200 = 400\,\mathrm{W}.

Check: Ptotal=VItotal=240×1.67=400WP_{\mathrm{total}} = VI_{\mathrm{total}} = 240 \times 1.67 = 400\,\mathrm{W}.

If you get this wrong, revise: Sections 6.1 and 4.2.

Problem 10

A student connects a cell to a resistor and measures a terminal p.d. of 4.5V4.5\,\mathrm{V} with a current of 1.5A1.5\,\mathrm{A}. The student then removes the resistor and measures the open-circuit p.d. as 5.4V5.4\,\mathrm{V}. Calculate the internal resistance of the cell and the value of the external resistor.

Solution

The open-circuit p.d. equals the emf: ε=5.4V\varepsilon = 5.4\,\mathrm{V}.

Using V=εIrV = \varepsilon - Ir:

4.5=5.41.5r    1.5r=0.9    r=0.60Ω4.5 = 5.4 - 1.5r \implies 1.5r = 0.9 \implies r = 0.60\,\Omega

External resistor:

R=VI=4.51.5=3.0ΩR = \frac{V}{I} = \frac{4.5}{1.5} = 3.0\,\Omega

If you get this wrong, revise: Section 5.1.

Problem 11

A circuit contains two loops sharing a common branch. Loop 1 has a 10V10\,\mathrm{V} cell with internal resistance 1.0Ω1.0\,\Omega and a 4.0Ω4.0\,\Omega resistor. Loop 2 has a 6.0V6.0\,\mathrm{V} cell (with polarity opposing the 10V10\,\mathrm{V} cell) with internal resistance 2.0Ω2.0\,\Omega and a 5.0Ω5.0\,\Omega resistor. The shared branch has a 3.0Ω3.0\,\Omega resistor. Use Kirchhoff's laws to find the current in the shared branch.

Solution

Let I1I_1 flow clockwise in loop 1, I2I_2 flow clockwise in loop 2, and I3=I1I2I_3 = I_1 - I_2 flow through the shared 3.0Ω3.0\,\Omega resistor from top to bottom.

KVL around loop 1:

10I1(1.0)(I1I2)(3.0)I1(4.0)=0    108I1+3I2=0    8I13I2=1010 - I_1(1.0) - (I_1 - I_2)(3.0) - I_1(4.0) = 0 \implies 10 - 8I_1 + 3I_2 = 0 \implies 8I_1 - 3I_2 = 10

KVL around loop 2:

6I2(2.0)(I2I1)(3.0)I2(5.0)=0    6+3I110I2=0    3I110I2=66 - I_2(2.0) - (I_2 - I_1)(3.0) - I_2(5.0) = 0 \implies 6 + 3I_1 - 10I_2 = 0 \implies 3I_1 - 10I_2 = -6

From the first equation: I1=(10+3I2)/8I_1 = (10 + 3I_2)/8.

Substituting into the second:

310+3I2810I2=6    30+9I2810I2=63\frac{10 + 3I_2}{8} - 10I_2 = -6 \implies \frac{30 + 9I_2}{8} - 10I_2 = -6

30+9I280I2=48    71I2=78    I2=1.099A30 + 9I_2 - 80I_2 = -48 \implies -71I_2 = -78 \implies I_2 = 1.099\,\mathrm{A}

I1=10+3(1.099)8=13.308=1.662AI_1 = \frac{10 + 3(1.099)}{8} = \frac{13.30}{8} = 1.662\,\mathrm{A}

I3=I1I2=1.6621.099=0.563AI_3 = I_1 - I_2 = 1.662 - 1.099 = 0.563\,\mathrm{A}

The current in the shared branch is approximately 0.56A0.56\,\mathrm{A}.

If you get this wrong, revise: Sections 4.3 and 9.

Problem 12

A tungsten filament has resistance 20Ω20\,\Omega at 20C20^\circ\mathrm{C}. The temperature coefficient of resistance for tungsten is α=4.5×103K1\alpha = 4.5 \times 10^{-3}\,\mathrm{K}^{-1}. Find the resistance of the filament when operating at 2500C2500^\circ\mathrm{C}.

Solution

RT=R0[1+α(TT0)]=20[1+(4.5×103)(250020)]R_T = R_0[1 + \alpha(T - T_0)] = 20[1 + (4.5 \times 10^{-3})(2500 - 20)]

RT=20[1+(4.5×103)(2480)]=20[1+11.16]=20×12.16=243.2ΩR_T = 20[1 + (4.5 \times 10^{-3})(2480)] = 20[1 + 11.16] = 20 \times 12.16 = 243.2\,\Omega

The resistance increases by a factor of approximately 12, which is why filament lamps draw much more current when first switched on (cold) than during normal operation.

If you get this wrong, revise: Section 3.3.



tip

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