Circuits & Electrical Power

Formula sheet · learning zone · practice problems with answer key

First-year EE · DC circuits to machines · 75 formulas · 98 practice problems · metric edition 1

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The formula sheet

Ohm's Law
V=IRV = I R
Electric Charge (Q = It)
Q=ItQ = I t
Electrical Power (P = VI)
P=VIP = V I
Electrical Power (P = I²R)
P=I2RP = I^{2} R
Electrical Power (P = V²/R)
P=V2RP = \frac{V^{2}}{R}
Two Resistors in Series
Rt=R1+R2R_{t} = R_{1} + R_{2}
Two Resistors in Parallel
Rt=R1R2R1+R2R_{t} = \frac{R_{1} R_{2}}{R_{1} + R_{2}}
Voltage Divider
Vout=VinR2R1+R2V_{out} = V_{in} \frac{R_{2}}{R_{1} + R_{2}}
Current Divider
I1=ItR2R1+R2I_{1} = I_{t} \frac{R_{2}}{R_{1} + R_{2}}
Resistance of a Wire (R = ρL/A)
R=ρLAR = \frac{\rho L}{A}
Conductor Resistance Temperature Correction
R2=R1[1+α(T2T1)]R_{2} = R_{1} \left[ 1 + \alpha (T_{2} - T_{1}) \right]
Kirchhoff's Voltage Law (Three-Element Loop)
Vs=V1+V2+V3V_{s} = V_{1} + V_{2} + V_{3}
Kirchhoff's Current Law (Node with Three Branches)
Iin=I1+I2+I3I_{in} = I_{1} + I_{2} + I_{3}
Thevenin Resistance from an Open-Circuit and Loaded Measurement
RTh=RL(VOCVL1)R_{Th} = R_{L} \left( \frac{V_{OC}}{V_{L}} - 1 \right)
Norton Current from the Thevenin Equivalent
IN=VThRThI_{N} = \frac{V_{Th}}{R_{Th}}
Maximum Power Transfer to a Matched Load
Pmax=VTh24RThP_{max} = \frac{V_{Th}^{2}}{4 R_{Th}}
Delta to Wye Resistance Transformation
RA=RabRcaRab+Rbc+RcaR_{A} = \frac{R_{ab} R_{ca}}{R_{ab} + R_{bc} + R_{ca}}
Wye to Delta Resistance Transformation
Rab=RARB+RBRC+RCRARCR_{ab} = \frac{R_{A} R_{B} + R_{B} R_{C} + R_{C} R_{A}}{R_{C}}
LED Series Resistor
R=VsVfIR = \frac{V_{s} - V_{f}}{I}
Capacitance (C = Q/V)
C=QVC = \frac{Q}{V}
Energy Stored in a Capacitor
E=12CV2E = \tfrac{1}{2} C V^{2}
Two Capacitors in Series
Ct=C1C2C1+C2C_{t} = \frac{C_{1} C_{2}}{C_{1} + C_{2}}
Two Capacitors in Parallel
Ct=C1+C2C_{t} = C_{1} + C_{2}
RC Time Constant
τ=RC\tau = R C
RC Capacitor Discharge
V=V0et/τV = V_{0} \, e^{-t/\tau}
RL Time Constant (τ = L/R)
τ=LR\tau = \frac{L}{R}
Energy Stored in an Inductor
E=12LI2E = \tfrac{1}{2} L I^{2}
RMS and Peak Voltage
Vrms=Vpeak2V_{rms} = \frac{V_{peak}}{\sqrt{2}}
Inductive Reactance (X_L = 2πfL)
XL=2πfLX_L = 2\pi f L
Capacitive Reactance (X_C = 1/2πfC)
XC=12πfCX_C = \frac{1}{2\pi f C}
Series RL or RC Impedance
Z=R2+X2Z = \sqrt{R^{2} + X^{2}}
Series RLC Impedance
Z=R2+(XLXC)2Z = \sqrt{R^{2} + (X_{L} - X_{C})^{2}}
Phase Angle from Power Factor
φ=arccos(PF)\varphi = \arccos(\text{PF})
LC Resonant Frequency
f=12πLCf = \frac{1}{2\pi\sqrt{LC}}
Q Factor of a Series Resonant Circuit
Q=1RLCQ = \frac{1}{R} \sqrt{\frac{L}{C}}
Bandwidth from Q and Centre Frequency
BW=f0QBW = \frac{f_{0}}{Q}
RC Cutoff Frequency
fc=12πRCf_{c} = \frac{1}{2\pi R C}
RL Cutoff Frequency
fc=R2πLf_{c} = \frac{R}{2\pi L}
Decibel Voltage Gain
GdB=20log10 ⁣(V2V1)G_{dB} = 20 \log_{10}\!\left(\frac{V_{2}}{V_{1}}\right)
Decibel Power Gain
GdB=10log10 ⁣(P2P1)G_{dB} = 10 \log_{10}\!\left(\frac{P_{2}}{P_{1}}\right)
Single-Phase Real Power with Power Factor
P=VIPFP = V I \, \text{PF}
Power Factor from Real and Apparent Power
PF=PS\text{PF} = \frac{P}{S}
Reactive Power (Power Triangle)
Q=S2P2Q = \sqrt{S^{2} - P^{2}}
Three-Phase Real Power
P=3VLILPFP = \sqrt{3} \, V_{L} I_{L} \, \text{PF}
Three-Phase Apparent Power
S=3VLILS = \sqrt{3} \, V_{L} I_{L}
Wye Line and Phase Voltage
VL=3VφV_{L} = \sqrt{3} \, V_{\varphi}
Delta Line and Phase Current
IL=3IφI_{L} = \sqrt{3} \, I_{\varphi}
Power-Factor Correction kvar
Qc=P(tanφ1tanφ2)Q_{c} = P \left( \tan\varphi_{1} - \tan\varphi_{2} \right)
Power-Factor Correction Capacitance
C=Qc2πfV2C = \frac{Q_{c}}{2\pi f V^{2}}
Electrical Energy (E = Pt)
E=PtE = P t
Energy Cost from a Utility Rate
Ce=EpeC_e = E \, p_e
Voltage Drop, Single Phase
Vd=2ρLIAV_{d} = \frac{2 \rho L I}{A}
Voltage Drop, Three Phase
Vd=3ρLIAV_{d} = \frac{\sqrt{3} \, \rho L I}{A}
Percent Voltage Drop
%Vd=100VdVs\%V_{d} = \frac{100 \, V_{d}}{V_{s}}
Peukert's Law (Battery Runtime)
t=H(CIH)kt = H \left( \frac{C}{I H} \right)^{k}
Synchronous Speed from Frequency and Poles
Ns=2fpN_{s} = \frac{2f}{p}
Induction Motor Slip
s=100(NsNr)Nss = \frac{100 \, (N_{s} - N_{r})}{N_{s}}
Motor Torque from Power and Speed
T=P2πNT = \frac{P}{2\pi N}
Motor Efficiency
η=100PoutPin\eta = \frac{100 \, P_{out}}{P_{in}}
Three-Phase Motor Full-Load Current
I=Pout3VPFηI = \frac{P_{out}}{\sqrt{3} \, V \, \text{PF} \, \eta}
Motor Locked-Rotor Starting Current
ILR=1000kP3VI_{LR} = \frac{1000 \, k \, P}{\sqrt{3} \, V}
Transformer Voltage Ratio
VsVp=NsNp\frac{V_{s}}{V_{p}} = \frac{N_{s}}{N_{p}}
Transformer Full-Load Current
IFL=SkVI_{FL} = \frac{S}{k \, V}
Voltage Regulation
%VR=100(VnlVfl)Vfl\%VR = \frac{100 \, (V_{nl} - V_{fl})}{V_{fl}}
Transformer Percent-Impedance Voltage Drop
Vd=%Z100SLSRVRV_{d} = \frac{\%Z}{100} \cdot \frac{S_{L}}{S_{R}} \cdot V_{R}
Available Short-Circuit Current from Percent Impedance
ISC=100IFL%ZI_{SC} = \frac{100 \, I_{FL}}{\%Z}
Generator Sizing from Connected Load
Pg=PcDf(1+m)P_{g} = P_{c} \, D_{f} \left( 1 + m \right)
Coulomb's Law
F=keq1q2r2F = \frac{k_e \, q_{1} q_{2}}{r^{2}}
Magnetic Force on a Moving Charge
F=qvBsinθF = q v B \sin\theta
Magnetic Force on a Current-Carrying Wire
F=BILsinθF = B I L \sin\theta
Force Between Parallel Wires
F=μ0I1I22πdF = \frac{\mu_0 I_1 I_2 \ell}{2\pi d}
Magnetic Field of a Solenoid
B=μ0NILB = \frac{\mu_0 N I}{L}
Magnetic Flux (Φ = BA cos θ)
Φ=BAcosθ\Phi = B A \cos\theta
Faraday's Law of Induction
ε=NΔΦΔt\varepsilon = N \frac{\Delta\Phi}{\Delta t}
Motional EMF (ε = BLv)
ε=BLv\varepsilon = B L v

DC Circuit Foundations

Ohm's Law

V=IRV = I R
IRV
Where
  • VV= Voltage (V)
  • II= Current (A)
  • RR= Resistance (Ω)

Georg Ohm published this relation in 1827 after painstaking experiments with wires of different lengths and thicknesses — and was initially ridiculed for reducing electricity to arithmetic. The idea is simple: voltage is the electrical push, resistance is the opposition, and current is what results. Double the push and you double the flow; double the opposition and you halve it. A 12 V car battery connected across a 6 Ω lamp drives 12/6 = 2 A through it; swap in a 3 Ω lamp and the current doubles to 4 A.

The law holds for ohmic conductors at constant temperature — metals, resistors, most wiring. Components like diodes, filament bulbs, and thermistors bend the rule because their resistance shifts as they heat up or as voltage changes. The classic V–I–R triangle mnemonic works because every rearrangement here is a single multiplication or division.

Worked example: 2 A through 6 Ω → 12 V

Electric Charge (Q = It)

Q=ItQ = I t
IQt
Where
  • QQ= Charge (C)
  • II= Current (A)
  • tt= Time (s)

Current is not a thing that flows. It is a rate — the amount of charge passing a chosen cross-section of the conductor each second — and one ampere means one coulomb per second. Once that is clear, Q=ItQ = It needs no proof, because it is the definition read backwards: if charge crosses at a steady rate, the total that crossed is the rate multiplied by how long it kept up. The only condition the equation imposes is the word steady. A current that varies has to be integrated, Q=IdtQ = \int I\,dt, and this page is the special case where the integral collapses to a rectangle.

A 2 A charger running for one hour moves 2×3600=7200 C2 \times 3600 = 7200\ \text{C}. Battery ratings are the same arithmetic wearing different units: a phone cell marked 3000 mAh holds 3 Ah, and 3×3600=10800 C3 \times 3600 = 10\,800\ \text{C} of deliverable charge. Divide by the elementary charge, 1.602×10191.602 \times 10^{-19} C, and that is about 6.7×10226.7 \times 10^{22} electrons — a number that only sounds absurd until you remember a gram of copper contains ten times as many free ones already sitting in the metal, drifting at well under a millimetre per second.

Since the 2019 redefinition of the SI, this relation is closer to the foundation than it used to be. The ampere is now fixed by declaring the elementary charge to be exactly 1.602176634×10191.602176634 \times 10^{-19} C, which makes the coulomb a count of charges and the ampere a count per second. Michael Faraday got there experimentally in the 1830s: his laws of electrolysis measure the charge needed to plate out a mole of a substance, and that constant — 96 485 C per mole — is nothing but Q=ItQ = It run on a plating tank. Electroplating, anodising and battery capacity testing all still bill in ampere-hours for exactly this reason.

Two errors are worth naming, and one convention deserves an apology. The first error is treating milliamp-hours as energy. They are charge; a 3000 mAh cell at 3.7 V holds 3×3.7=11.1 Wh3 \times 3.7 = 11.1\ \text{Wh}, and the same 3000 mAh at 1.2 V holds a third of that, so comparing two batteries by mAh alone tells you very little. The second is applying the equation to a current that is not constant — a motor's inrush, a switching supply's chopped input, or anything on AC, where over a full cycle the net charge transferred is zero even though the current is real all along. As for the convention: current is drawn flowing from plus to minus, while in a metal the electrons actually travel the other way. Benjamin Franklin guessed the sign in the 1750s, a century before anyone knew a charge carrier existed, and he guessed wrong. Nothing in the physics breaks — a deficit of negatives moving left is indistinguishable from positives moving right — but it is a historical accident, not a discovery, and it is worth knowing that it is one.

Worked example: 2 A for 30 s → 60 C

Electrical Power (P = VI)

P=VIP = V I
PIV
Where
  • PP= Power (W)
  • VV= Voltage (V)
  • II= Current (A)

This formula falls straight out of the definitions. A volt is a joule per coulomb — the energy each unit of charge carries — and an ampere is a coulomb per second — how many units of charge arrive each second. Multiply them and the coulombs cancel, leaving joules per second: watts. A 1500 W space heater on a 120 V household circuit draws 1500/120 = 12.5 A, which is why it crowds a standard 15 A breaker and shouldn't share the circuit with much else.

Unlike the resistor-specific forms P = I²R and P = V²/R, this version works for any component — ohmic or not — including motors, LEDs, and batteries, because it comes from the definitions of voltage and current rather than from Ohm's law. Electric utilities meter exactly this product, accumulated over time, when they bill you for energy.

Worked example: 120 V at 0.5 A → 60 W

Electrical Power (P = I²R)

P=I2RP = I^{2} R
IRP
Where
  • PP= Power (W)
  • II= Current (A)
  • RR= Resistance (Ω)

This is the heat form of electrical power, and the square is the whole point of it. Start from P=VIP = VI, substitute Ohm's law for the voltage across the resistance, V=IRV = IR, and you get P=I2RP = I^2 R. Because the current appears twice, the heat does not track the load — it tracks the square of the load. Double the current and a conductor dissipates four times the heat; triple it and nine times. Nothing else in ordinary wiring punishes a modest overload so hard, and it is the reason a circuit that runs warm at rated current runs dangerously hot at 150% of it.

Take a 30 m branch circuit run in 12 AWG copper. The conductor is about 3.31 mm², copper's resistivity is 1.68×1081.68 \times 10^{-8} Ω·m, so each metre is roughly 5.1 mΩ — and the current has to go out and come back, so the loop is 60 m and about 0.30 Ω. At 15 A the copper dissipates 152×0.30=68 W15^2 \times 0.30 = 68\ \text{W}, spread along the run, and drops 15×0.30=4.6 V15 \times 0.30 = 4.6\ \text{V} of the supply before it ever reaches the load. Drop the current to 5 A and the loss falls to 7.5 W, not to a third: that is the square doing its work.

James Joule established the law in 1841 by immersing coils in water and measuring the temperature rise, which was also his route to the mechanical equivalent of heat and thence to the first law of thermodynamics. The same relation is the reason the grid transmits at hundreds of kilovolts. Delivered power is VIVI, so raising the voltage a hundredfold cuts the current a hundredfold for the same power, and cuts the line loss by ten thousand. Every transformer between a generating station and a house exists to move a fixed quantity of watts into a lower current, purely so that this equation returns a smaller number.

Three traps, in rising order of consequence. First, RR is the resistance of the thing dissipating the heat, and II is the current through that same thing — mixing the conductor's resistance with the load's current is fine only because they are in series, and on a branched circuit it is not fine at all. Second, on AC the current must be RMS. A peak reading gives twice the power for a sine wave, and using it is one of the most common ways to double an answer without noticing. Third, and the one that bites in the field: this equation uses resistance, and on an AC circuit the opposition to current is impedance. A long run of steel-armoured cable, a coil, or a motor feeder has reactance as well as resistance, and the voltage drop computed from DC resistance alone will understate the real drop. The heat, though, still comes only from the resistive part — reactance stores energy and hands it back, so it moves voltage around without ever warming the copper.

Worked example: 3 A through 10 Ω → 90 W

Electrical Power (P = V²/R)

P=V2RP = \frac{V^{2}}{R}
RPV
Where
  • PP= Power (W)
  • VV= Voltage (V)
  • RR= Resistance (Ω)

This is the same power as P=VIP = VI, written for the situation you actually meet at a wall outlet: the voltage is fixed and the resistance is what you choose. Substitute I=V/RI = V/R into P=VIP = VI and the current disappears, leaving P=V2/RP = V^2/R. Read it carefully, because the two variables behave in opposite directions. Power rises with the square of the voltage but falls inversely with resistance — so halving the resistance doubles the power, while doubling the voltage quadruples it.

A 1500 W kettle on a 120 V supply must therefore be built with R=V2/P=14400/1500=9.6 ΩR = V^2/P = 14\,400/1500 = 9.6\ \Omega of element. The same element plugged into 240 V would try to deliver 57600/9.6=6000 W57\,600/9.6 = 6000\ \text{W} — four times its rating — which is why travel appliances fail spectacularly rather than gradually. Run the arithmetic the other way for a 1000 W element on 230 V mains and you need about 53 Ω. Notice that the element's resistance is a design choice made to hit a wattage at one particular voltage; the wattage on the label is not a property of the element, it is a property of the element and the supply it was designed for.

The three power forms, P=VIP = VI, P=I2RP = I^2R and P=V2/RP = V^2/R — are one equation seen from three sides, and picking the right one is mostly about which quantity is being held constant. Devices in parallel across a fixed supply are the V2/RV^2/R case: every extra appliance you plug in adds power, because it adds a path, and lowering the effective resistance raises the total draw. Devices in series carrying a common current are the I2RI^2R case. Only P=VIP = VI makes no assumption at all, which is why it is the one that still works for motors, LEDs and batteries where Ohm's law does not.

Where this goes wrong. The resistance to use is the resistance at operating temperature, and for anything that glows that is not what an ohmmeter reads on the bench. A tungsten filament's resistance climbs by roughly a factor of fifteen between room temperature and incandescence, so a 60 W lamp measuring 20 Ω cold does not draw 720 W — it draws a large inrush for a few milliseconds and then settles near 240 Ω. The second error is the mains one: use RMS voltage, always. Plugging the 170 V peak of a 120 V circuit into this formula doubles the answer. The third is applying it to a load that is not resistive. A motor at 120 V drawing 5 A is not a 24 Ω resistor; most of that opposition is reactance, which stores and returns energy rather than turning it into heat, and V2/RV^2/R with an impedance in the denominator will overstate the watts by exactly the power factor.

Worked example: 120 V across 240 Ω → 60 W

Two Resistors in Series

Rt=R1+R2R_{t} = R_{1} + R_{2}
R1R2Rt
Where
  • RtR_{t}= Total resistance (Ω)
  • R1R_{1}= Resistance 1 (Ω)
  • R2R_{2}= Resistance 2 (Ω)

Two resistors wired end to end sit on one path, and that single fact settles everything else. Charge has nowhere to go but forward, so the same current passes through both — it is not divided between them and it is not shared out according to size. Each resistor then takes its own voltage drop, V1=IR1V_1 = I R_1 and V2=IR2V_2 = I R_2, and the two drops must add up to whatever the supply provides. Divide that sum by the current they have in common and the resistances add: Rt=R1+R2R_t = R_1 + R_2. This is not a rule to memorise. It is Ohm's law applied twice in a circuit that has only one loop.

Put a 47 Ω resistor in series with a 220 Ω resistor across a 12 V supply. The total is 267 Ω, so the current is 12/267=45 mA12/267 = 45\ \text{mA}, and it is 45 mA at every point in the loop — before the first resistor, between them, and after the second. The 47 Ω part drops 0.045×47=2.1 V0.045 \times 47 = 2.1\ \text{V}; the 220 Ω part drops 0.045×220=9.9 V0.045 \times 220 = 9.9\ \text{V}; and 2.1 + 9.9 gives back the 12 V we started with. Adding the drops as a check costs nothing and catches most arithmetic errors on the spot.

The bookkeeping behind that check is Kirchhoff's voltage law, published by Gustav Kirchhoff in 1845 while he was still a student: go once around any closed loop and the voltage rises equal the voltage falls, because the loop returns you to the potential you started at. Every series result descends from it. The voltage divider is the same equation rearranged — each resistor claims the fraction R1/(Rt)R_1/(R_t) of the supply — and that is how a potentiometer, a thermistor bridge and a sensor's biasing network all work. Solving this page backwards for one resistor is subtraction, R1=RtR2R_1 = R_t - R_2, which is why the total must exceed the branch you already know.

The mistakes cluster in three places. The first is reaching for the wrong combination rule: series resistors add, parallel resistors combine as product over sum, and capacitors do exactly the reverse — series capacitors are the reciprocal case. Whenever you find yourself using product-over-sum on a series string, stop and ask which component you are holding. The second is assuming the larger resistor gets the larger current; it gets the larger voltage drop at the same current, and confusing those two makes a mess of any divider. The third only appears on AC: a coil or a capacitor in series with a resistor cannot be added arithmetically to it. Reactance is 90° out of phase with resistance, so a 30 Ω resistor in series with 40 Ω of reactance presents 302+402=50 Ω\sqrt{30^2 + 40^2} = 50\ \Omega, not 70. This page adds resistances, and resistances are what it will add — the quadrature sum belongs on the impedance pages.

Worked example: 220 Ω + 330 Ω in series → 550 Ω

Two Resistors in Parallel

Rt=R1R2R1+R2R_{t} = \frac{R_{1} R_{2}}{R_{1} + R_{2}}
R1R2Rt
Where
  • RtR_{t}= Total resistance (Ω)
  • R1R_{1}= Resistance 1 (Ω)
  • R2R_{2}= Resistance 2 (Ω)

Wired side by side, two resistors give the current two paths at once, so more current flows for the same voltage and the combination resists less than either branch alone. The tidy product-over-sum form is just 1/Rt = 1/R1 + 1/R2 rearranged — conductances, not resistances, are what add in parallel. Worked example: 100 Ω in parallel with 25 Ω gives (100 × 25)/(100 + 25) = 2500/125 = 20 Ω, comfortably below the smaller branch.

Two handy special cases: equal resistors in parallel halve (two 100 Ω resistors make 50 Ω), and a much smaller resistor dominates — 10 Ω in parallel with 10 kΩ is essentially 10 Ω. Household outlets are wired in parallel so every appliance sees full mains voltage. When solving for a branch, the other resistance must exceed the total, since the total is always the smallest value in the circuit.

Worked example: 4 Ω ∥ 12 Ω → 3 Ω

Voltage Divider

Vout=VinR2R1+R2V_{out} = V_{in} \frac{R_{2}}{R_{1} + R_{2}}
R₁R₂VinVout
Where
  • VoutV_{out}= Output voltage (V)
  • VinV_{in}= Input voltage (V)
  • R1R_{1}= Upper resistance (Ω)
  • R2R_{2}= Lower resistance (Ω)

Series resistors carry the same current, so each takes a share of the voltage in proportion to its resistance — the divider is Ohm's law applied twice. Twelve volts across 10 kΩ over 5 kΩ puts 12 × 5/15 = 4 V at the junction. It is the most-used circuit in electronics: bias networks, level shifters, the feedback string that sets a regulator's output, and every potentiometer, which is just a divider with a movable tap.

The trap is loading. This formula assumes nothing draws current from the tap; connect a load comparable to R₂ and the output sags, because the load parallels R₂. The rule of thumb is to make the divider current at least ten times the load current — but not so low-resistance that it wastes power. That trade-off is why high-impedance dividers pair with op-amp buffers, and why measuring a 1 MΩ divider with a cheap 1 MΩ-input meter reads badly wrong.

Worked example: 12 V over 10 kΩ + 5 kΩ → 4 V

Current Divider

I1=ItR2R1+R2I_{1} = I_{t} \frac{R_{2}}{R_{1} + R_{2}}
ItI₁R₁R₂
Where
  • I1I_{1}= Current in branch 1 (A)
  • ItI_{t}= Total current (A)
  • R1R_{1}= Branch 1 resistance (Ω)
  • R2R_{2}= Branch 2 resistance (Ω)

Parallel branches share a voltage, so current splits inversely with resistance — and that inversion is why the opposite resistor appears on top. Six amps entering a 4 Ω branch paralleled with a 2 Ω branch sends 6 × 2/6 = 2 A through the 4 Ω path and 4 A through the 2 Ω path: the easier road takes the most traffic.

Electricians meet this as the reason parallel feeders must be identical in size, length and material — a run even slightly shorter hogs current and overheats while its twin loafs, which is exactly what the NEC's paralleling rules exist to prevent. Benchtop electronics meets it as the ammeter shunt: send 99% of the current through a milliohm resistor and measure the small remainder. Note that for more than two branches the tidy two-resistor form fails; use conductance ratios instead.

Worked example: 6 A into 4 Ω ∥ 2 Ω → 2 A in the 4 Ω branch

Resistance of a Wire (R = ρL/A)

R=ρLAR = \frac{\rho L}{A}
AρRL
Where
  • RR= Resistance (Ω)
  • ρ\rho= Resistivity (Ω·m)
  • LL= Wire length (m)
  • AA= Cross-sectional area ()

Resistance behaves like a road: make it longer and the journey costs more; make it wider and traffic moves more easily. Doubling the length of a conductor puts twice as many collisions between the electron and the far end, so resistance doubles. Doubling the cross-sectional area gives the current twice as many parallel paths, so resistance halves. What is left over — the part that depends on the material rather than its shape — is the resistivity ρ\rho, and R=ρL/AR = \rho L/A is nothing more than those three statements written together. Copper's 1.68×1081.68 \times 10^{-8} Ω·m is the reason it wires the world; aluminium is about 1.6 times higher, silver marginally lower, and a good insulator is some twenty orders of magnitude higher than any of them.

A hundred metres of 2.5 mm² copper comes to (1.68×108×100)/(2.5×106)=0.67 Ω(1.68 \times 10^{-8} \times 100)/(2.5 \times 10^{-6}) = 0.67\ \Omega. Carrying 16 A, that single conductor drops 16×0.67=10.7 V16 \times 0.67 = 10.7\ \text{V} and dissipates 172 W along its length. Both figures matter, and both are why a long run is specified thicker than the load current alone would suggest — the ampacity keeps the cable from overheating, but it is the voltage drop that usually decides the size.

Resistivity is a bulk property of the material, and the reciprocal quantity, conductivity, is what materials people usually quote. The relation also underpins the strain gauge, whose resistance changes as stretching lengthens it and narrows it; the shunt, a precisely dimensioned low-resistance bar used to measure large currents; and the whole logic of high-voltage transmission, where a fixed ρL/A\rho L/A in the line means the only way to cut the I2RI^2R loss is to cut II.

Four errors, and the first one is nearly universal. When you are computing voltage drop on a circuit, LL is the total length of conductor the current traverses, which for an ordinary two-wire supply is twice the run distance — out along one conductor and back along the other. A 30 m run is 60 m of copper, and using 30 halves the answer. Second, resistivity is strongly temperature-dependent: copper rises about 0.39% per degree, so a conductor at 75 °C has roughly 22% more resistance than the 20 °C handbook figure, and electrical codes tabulate drop at operating temperature for exactly this reason. Third, watch the area units. Wire gauges are not areas — 12 AWG is 3.31 mm², 10 AWG is 5.26 mm² — and a diameter must be squared and taken through πd2/4\pi d^2/4 before it can go in the denominator. Fourth, this is a DC resistance. On AC the current crowds toward the surface of the conductor, and above a few hundred hertz, or in large conductors at mains frequency, that skin effect raises the effective resistance measurably; and a long AC run has reactance as well, so the drop you actually measure will exceed what ρL/A\rho L/A alone predicts.

Worked example: 100 m of 2.5 mm^2 copper → R = 0.672 ohm

Conductor Resistance Temperature Correction

R2=R1[1+α(T2T1)]R_{2} = R_{1} \left[ 1 + \alpha (T_{2} - T_{1}) \right]
R₁T₁αR₂T₂
Where
  • R2R_{2}= Resistance at T₂ (Ω)
  • R1R_{1}= Resistance at T₁ (Ω)
  • α\alpha= Temperature coefficient (1/K)
  • T2T_{2}= New temperature (°C)
  • T1T_{1}= Reference temperature (°C)

Metals conduct worse when hot: heat jostles the lattice and scatters the electrons. Copper's coefficient is about 0.00393 per kelvin referenced to 20 °C, aluminium's about 0.00403, so a 10 Ω copper winding at 20 °C measures 10 × (1 + 0.00393 × 55) = 12.16 Ω at 75 °C — a 22% rise. Because a kelvin and a Celsius degree are the same size, only the temperature difference matters; if your α is quoted per °F, choose that unit and the solver handles it.

This relation is quietly one of the most useful in the trade. It turns a winding's cold and hot resistance into a motor's average winding temperature, the basis of the standard heat-run test — no thermocouple can reach the middle of a coil, but its resistance always can. It is also why cable ampacity tables assume a conductor temperature, why voltage-drop constants differ between 20 °C and 75 °C, and why platinum's clean, repeatable version of this curve makes the RTD the workhorse of industrial temperature measurement.

Worked example: 10 Ω copper, 20 °C → 75 °C gives 12.1615 Ω

Kirchhoff & the Network Theorems

Kirchhoff's Voltage Law (Three-Element Loop)

Vs=V1+V2+V3V_{s} = V_{1} + V_{2} + V_{3}
V₁V₂V₃Vs
Where
  • VsV_{s}= Source voltage (V)
  • V1V_{1}= Drop across element 1 (V)
  • V2V_{2}= Drop across element 2 (V)
  • V3V_{3}= Drop across element 3 (V)

Gustav Kirchhoff published this in 1845 while still a student, and it is nothing more than energy conservation dressed for a circuit: carry a charge all the way around a loop and back to where it started, and it must return to the same potential. Every rise has to be paid for by drops. So a 24 V supply feeding three series elements that drop 5.5 V and 12.1 V must be dropping the remaining 6.4 V across the third, whatever that third element happens to be.

The trap is sign, not arithmetic. Two sources fighting each other in a loop — a battery charging another battery, a generator paralleled slightly out of phase — subtract rather than add, and a loop containing a reversed source needs Vs=V1+V2V3V_s = V_1 + V_2 - V_3. This solver assumes all three elements drop in the same direction, so enter an opposing source as a negative number and the algebra still comes out right.

What people rarely notice is that KVL is an approximation, and a good one only because circuits are small. The law follows from the electric field being conservative, which stops being true the moment a changing magnetic field threads your loop. Move a scope probe's ground lead near a transformer and the "same" two points read different voltages — not a bad measurement, but a real induced EMF in the loop the probe lead just formed.

Worked example: 5.5 V + 12.1 V + 6.4 V → 24 V source

Kirchhoff's Current Law (Node with Three Branches)

Iin=I1+I2+I3I_{in} = I_{1} + I_{2} + I_{3}
IinI₁I₂I₃
Where
  • IinI_{in}= Current into the node (A)
  • I1I_{1}= Branch 1 current (A)
  • I2I_{2}= Branch 2 current (A)
  • I3I_{3}= Branch 3 current (A)

The node rule is the charge-conservation twin of the loop rule: charge cannot pile up at a junction, so whatever flows in must flow out. Ten amps arriving at a splice feeding three branches, two of which are carrying 2.5 A and 3.5 A, leaves exactly 4 A for the third. No knowledge of the loads is needed, which is what makes it so useful — it is a constraint you get for free before any analysis begins.

The classic mistake is treating current as something a source "sends" to a load rather than something that circulates. A branch drawing less current does not leave the surplus somewhere; the source simply produces less. That is why removing a lamp from a parallel lighting circuit dims nothing else, and why removing one from a series string kills everything: the series case has one node current, so it is KCL that says they all must be equal.

In the field this is the arithmetic behind every panel schedule and every neutral calculation. It is also the basis of nodal analysis, the method every circuit simulator actually runs — SPICE writes one KCL equation per node, solves the matrix, and never touches KVL at all. And the counter-intuitive part for electricians: on a balanced three-phase four-wire system, three currents of 100 A each sum to zero in the neutral, because KCL sums phasors, not magnitudes.

Worked example: 250 mA + 0.4 A + 150 mA → 0.8 A into the node

Thevenin Resistance from an Open-Circuit and Loaded Measurement

RTh=RL(VOCVL1)R_{Th} = R_{L} \left( \frac{V_{OC}}{V_{L}} - 1 \right)
RThVOCRLVL
Where
  • RThR_{Th}= Thevenin resistance (Ω)
  • VOCV_{OC}= Open-circuit voltage (V)
  • VLV_{L}= Loaded terminal voltage (V)
  • RLR_{L}= Load resistance (Ω)

Léon Thévenin's 1883 theorem says something extravagant: any tangle of sources and resistors, seen from two terminals, behaves exactly like one voltage source behind one resistor. You never have to know what is inside. And you can measure both numbers with a voltmeter and one known resistor — read the open-circuit voltage, hang the load, read the sagged voltage, and the internal resistance falls out of the droop.

Work an example the long way and the formula becomes obvious. A 9 V cell reads 9.00 V open and 8.10 V across 100 Ω. That load is drawing 8.10/100=0.0818.10/100 = 0.081 A, and the 0.90 V that went missing was dropped inside the cell, so RTh=0.90/0.081=11.1R_{Th} = 0.90/0.081 = 11.1 Ω. A fresh alkaline should be well under 2 Ω, so this one is tired — which is exactly how a battery tester works.

The mistake to avoid is shorting the terminals to find the internal resistance directly. On a cell that is merely rude; on a car battery or a lithium pack it is a welding accident. Use a load that draws a sensible current and let the droop tell you. One caution on the theorem itself: it holds for linear circuits only. Put a diode, a lamp filament or a switching supply behind the terminals and RTh becomes a number that changes with the load you used to measure it.

Worked example: 9.00 V open, 8.10 V into 100 Ω → 11.11 Ω internal

Norton Current from the Thevenin Equivalent

IN=VThRThI_{N} = \frac{V_{Th}}{R_{Th}}
VThRThINRTh
Where
  • INI_{N}= Norton current (A)
  • VThV_{Th}= Thevenin voltage (V)
  • RThR_{Th}= Thevenin resistance (Ω)

Edward Norton at Bell Labs described the dual of Thévenin's result in 1926: the same two terminals can equally be modelled as a current source with a resistor in parallel. The two models are interchangeable, and the bridge between them is Ohm's law — a 12 V source behind 4 Ω is a 3 A source across 4 Ω, and no measurement made at the terminals can tell them apart.

Which one you pick is pure convenience. Norton form makes parallel branches trivial, because current sources in parallel simply add, so it is the natural language of nodal analysis and of transistor models. Thevenin form makes series chains trivial. Experienced analysts flip back and forth mid-problem — that flip is called a source transformation, and it is often the single step that turns an ugly network into an obvious one.

The number IN is the current the source would deliver into a dead short, which is worth respecting. A 12 V car battery with 5 mΩ internal resistance has a Norton current of 2400 A, and that is why a dropped spanner across the terminals vaporises. Note also that both models are fictions from the terminals only: a Norton equivalent burns power in its resistor even at no load, so it tells you nothing true about what the real box is dissipating inside.

Worked example: 12 V behind 4 Ω → 3 A Norton current

Maximum Power Transfer to a Matched Load

Pmax=VTh24RThP_{max} = \frac{V_{Th}^{2}}{4 R_{Th}}
VThRThPmaxRTh
Where
  • PmaxP_{max}= Maximum load power (W)
  • VThV_{Th}= Thevenin voltage (V)
  • RThR_{Th}= Thevenin resistance (Ω)

Sweep a load resistance from zero to infinity across a source and the power it receives rises, peaks, and falls again. Too small and the voltage collapses; too large and the current does. The peak sits exactly where RL=RThR_L = R_{Th}, and there the load takes VTh2/4RThV_{Th}^2/4R_{Th}. Twenty volts behind 5 Ω, matched by a 5 Ω load: the loop carries 2 A, and the load absorbs 22×5=202^2 \times 5 = 20 W.

Notice what else happened in that example — the source dissipated 20 W too. Matched transfer is 50% efficient, always, by construction. That is the classic misreading of this theorem: it maximises power delivered, not power saved. No utility matches its generators to the grid; a power system deliberately runs with source impedance far below load impedance so efficiency approaches 100% and voltage stays stiff. Matching belongs where the signal matters and the watts do not.

So it lives in RF and audio and instrumentation: antennas into 50 Ω feedlines, transmission lines terminated to stop reflections, a solar panel held at its maximum-power point by a tracking converter. And the AC version wants the load impedance to be the complex conjugate of the source, so a source that looks inductive must be met with capacitance — reactance cancelled first, resistance matched second.

Worked example: 20 V behind 5 Ω → 20 W into a matched 5 Ω

Delta to Wye Resistance Transformation

RA=RabRcaRab+Rbc+RcaR_{A} = \frac{R_{ab} R_{ca}}{R_{ab} + R_{bc} + R_{ca}}
RabRcaRbcRA
Where
  • RAR_{A}= Wye arm at node A (Ω)
  • RabR_{ab}= Delta leg a-b (Ω)
  • RbcR_{bc}= Delta leg b-c (Ω)
  • RcaR_{ca}= Delta leg c-a (Ω)

Some networks refuse to be reduced. A Wheatstone bridge has no two resistors in plain series and no two in plain parallel, so the usual tools stall. Arthur Kennelly's 1899 transformation is the way out: swap any triangle of three resistors for an electrically identical star, and the series-parallel structure reappears. The arm of the star at node A is the product of the two triangle legs that touch A, divided by the sum of all three.

The balanced case is worth memorising because it is so clean: three equal 30 Ω legs become three equal 10 Ω arms, RY=RΔ/3R_Y = R_\Delta/3. For the unbalanced case take a 10/20/30 Ω delta — the sum is 60, so the arm at A, touching the 10 and the 30, is 10×30/60=510 \times 30/60 = 5 Ω. Every star arm always comes out smaller than either delta leg it touches, which is a useful sanity check on your own arithmetic.

The trap is bookkeeping: it is dangerously easy to pair an arm with the wrong two legs. Label the nodes on the drawing before you start, and remember the rule in words — the arm at a node uses the two legs meeting at that node, and the leg opposite a node never appears in the numerator. Note also that this is a resistance identity, but it works unchanged for complex impedances, which is how three-phase engineers convert a delta-connected load to its wye equivalent before applying per-phase analysis.

Worked example: Balanced 30 Ω delta → 10 Ω wye arm

Wye to Delta Resistance Transformation

Rab=RARB+RBRC+RCRARCR_{ab} = \frac{R_{A} R_{B} + R_{B} R_{C} + R_{C} R_{A}}{R_{C}}
RARBRCRab
Where
  • RabR_{ab}= Delta leg a-b (Ω)
  • RAR_{A}= Wye arm at node A (Ω)
  • RBR_{B}= Wye arm at node B (Ω)
  • RCR_{C}= Wye arm at node C (Ω)

Going back the other way, the delta leg between two nodes is the sum of the three pairwise products of the star arms, divided by the arm at the node the leg does not touch. A balanced 10 Ω star becomes a 30 Ω delta, the mirror of RΔ=3RYR_\Delta = 3R_Y. Unbalanced: arms of 5, 10 and 20 Ω give pairwise products 50, 200 and 100, summing to 350, so the leg opposite the 20 Ω arm is 350/20=17.5350/20 = 17.5 Ω.

That opposite-arm divisor is where people go wrong. The numerator is the same for all three legs — compute it once — and only the denominator changes, so the leg opposite the smallest arm comes out largest. Another built-in check: every delta leg must exceed the sum of the two star arms it spans, because the direct path has to imitate both the series path and the roundabout one. Here 17.5 Ω comfortably beats 5+10=155 + 10 = 15 Ω.

Practically this direction shows up when a network has a star that blocks reduction, and in three-phase work when a wye-connected load has to be restated as delta for a source that is delta-connected. It is also the reason a delta-connected motor winding draws three times the current of the same windings in wye at the same line voltage, which is the whole basis of wye-delta starting.

Worked example: Balanced 10 Ω wye → 30 Ω delta leg

LED Series Resistor

R=VsVfIR = \frac{V_{s} - V_{f}}{I}
VsRIVf
Where
  • RR= Series resistance (Ω)
  • VsV_{s}= Supply voltage (V)
  • VfV_{f}= LED forward voltage (V)
  • II= LED current (A)

An LED is not a resistor — its current climbs almost vertically once forward voltage is reached, so a tiny voltage excess becomes a huge, fatal current. The resistor is what makes the circuit predictable: it eats the difference between supply and forward voltage, and Ohm's law sets the current. Running a red LED (Vf ≈ 2.1 V) at 20 mA from 5 V needs (5 − 2.1)/0.02 = 145 Ω, so you fit a 150 Ω standard value.

Two things beginners miss. First, check the resistor's power: here it dissipates (5 − 2.1) × 0.02 ≈ 58 mW, comfortable for a quarter-watt part, but a 12 V supply on the same LED wastes 198 mW and argues for a proper constant-current driver. Second, forward voltage depends on colour and on temperature — roughly 1.8–2.2 V for red, 3.0–3.4 V for blue and white — and it drops about 2 mV per °C as the die heats, which is precisely why high-power LEDs must never be run from a resistor alone.

Worked example: 5 V rail, 2.1 V LED, 20 mA → 145 Ω

Storage & AC Impedance

Capacitance (C = Q/V)

C=QVC = \frac{Q}{V}
QVC
Where
  • CC= Capacitance (μF)
  • QQ= Charge (C)
  • VV= Voltage (V)

Capacitance is charge-storing capacity: how many coulombs a capacitor soaks up for every volt you apply across it. The unit, the farad, honors Michael Faraday — and it is a giant. A full farad would have been a bench-filling curiosity for most of electronics history, so practical parts are marked in microfarads, nanofarads, and picofarads; only modern supercapacitors reach whole farads. Doubling the applied voltage doubles the stored charge, but C itself stays fixed — it depends only on geometry and the insulating material between the plates.

Worked example: a 100 µF capacitor charged to 12 V holds Q = CV = 100×10⁻⁶ × 12 = 1.2 mC of charge — about 7.5×10¹⁵ electrons parked on one plate and missing from the other. This defining relation applies to every capacitor, from the tuning capacitor in a radio to the DRAM cell storing one bit in your computer.

Worked example: 1 mC at 10 V → 100 uF

Energy Stored in a Capacitor

E=12CV2E = \tfrac{1}{2} C V^{2}
ECV
Where
  • EE= Stored energy (J)
  • CC= Capacitance (μF)
  • VV= Voltage (V)

Why the half? Charging a capacitor is like stretching a spring: the first coulomb slides on easily, but every later coulomb must be pushed against the voltage the earlier ones built up. The voltage ramps linearly from 0 to V as charge accumulates, so the average push is V/2, and the total work is Q×V/2 = ½CV² — the triangular area under the Q–V line. Equivalent forms E = Q²/(2C) and E = QV/2 follow directly from C = Q/V.

Worked example: a camera-flash capacitor of 1000 µF charged to 300 V stores E = ½ × 0.001 × 300² = 45 J, dumped through the xenon tube in about a millisecond — a burst of tens of kilowatts from a pocket battery. The same math sizes defibrillators and grid-scale supercapacitor banks. Solving for V takes the positive square root, since the formula gives the voltage magnitude.

Worked example: 100 uF at 12 V → 7.2 mJ

Two Capacitors in Series

Ct=C1C2C1+C2C_{t} = \frac{C_{1} C_{2}}{C_{1} + C_{2}}
C1C2Ct
Where
  • CtC_{t}= Total capacitance (μF)
  • C1C_{1}= Capacitance 1 (μF)
  • C2C_{2}= Capacitance 2 (μF)

Capacitors in series combine the way resistors in parallel do, and the reason is worth following rather than memorising. Wire two capacitors end to end and the middle section — the bottom plate of the first joined to the top plate of the second — is isolated from everything else. Whatever charge leaves that plate must arrive at this one, so every capacitor in a series string carries the identical charge QQ. Each then holds its own voltage, V1=Q/C1V_1 = Q/C_1 and V2=Q/C2V_2 = Q/C_2, and those add to the applied voltage. Divide through by the common QQ and you get 1/Ct=1/C1+1/C21/C_t = 1/C_1 + 1/C_2, which for two parts is the product-over-sum form on this page.

Two equal 10 µF capacitors in series make 5 µF, not 20. A 10 µF with a 1 µF gives (10×1)/(10+1)=0.91 μF(10 \times 1)/(10 + 1) = 0.91\ \mu\text{F} — barely less than the small one, because the small capacitor needs the most volts to accept the shared charge and therefore dominates the total. That is the general behaviour: the result is always smaller than the smallest member, and a large capacitor in series with a small one is very nearly the small one alone. Voltage divides in inverse proportion to capacitance, so in that pair, 100 V applied puts about 91 V across the 1 µF part and only 9 V across the 10 µF.

The geometric picture explains why it must be so. Capacitance for parallel plates is C=εA/dC = \varepsilon A/d, and stacking capacitors in series is effectively increasing dd — putting more insulating distance between the outermost plates — which lowers capacitance. Stacking them in parallel increases AA, which raises it. That is also the practical use of a series string: the working voltage adds even as the capacitance falls, so two 400 V parts in series will stand 800 V, and high-voltage DC links are routinely built this way.

The famous error is the one this page exists to prevent: series capacitors are not added. The mirror-image mistake — treating parallel capacitors with product-over-sum — is just as common. If you can only remember one anchor, remember that a series connection always makes capacitance worse and parallel always makes it better, then check your answer against that. The second error is far more hazardous and almost never taught. The voltage division above holds only at DC in an ideal world; real capacitors, and electrolytics in particular, have leakage currents that differ from part to part, and over minutes the string will redistribute itself until one capacitor carries most of the applied voltage and fails. Series electrolytic banks therefore need balancing resistors across each part, sized so their current is many times the worst-case leakage. Finally, do not assume two parts marked 400 V in series give a comfortable 800 V rating — they give it only while they share, and sharing is what the balancing resistors are for.

Worked example: 6 uF and 3 uF in series → 2 uF

Two Capacitors in Parallel

Ct=C1+C2C_{t} = C_{1} + C_{2}
C1C2Ct
Where
  • CtC_{t}= Total capacitance (μF)
  • C1C_{1}= Capacitance 1 (μF)
  • C2C_{2}= Capacitance 2 (μF)

Capacitors side by side across the same two nodes see the same voltage, and each stores the charge that voltage buys it: Q1=C1VQ_1 = C_1 V and Q2=C2VQ_2 = C_2 V. The total charge held is the sum, so the total capacitance — charge per volt — is also the sum, Ct=C1+C2C_t = C_1 + C_2. Physically the two components have simply become one larger capacitor: parallel connection joins their plates, and joining plates adds plate area. Since capacitance for a parallel-plate part is C=εA/dC = \varepsilon A / d, more area at the same separation means proportionally more capacitance, and the arithmetic could hardly come out any other way.

A 4.7 µF and a 2.2 µF part in parallel behave as 6.9 µF. Three 1000 µF electrolytics across a power-supply rail behave as 3000 µF. The additions are exact and there is no upper limit beyond what will fit on the board, which is why designers reach for parallel banks to hit values no manufacturer stocks — 4.7 with 2.2 to make 6.9 — and why a supply that needs 10 000 µF of bulk storage is built from several parts rather than one.

There is a second reason for the bank that has nothing to do with capacitance. Every real capacitor carries series resistance and series inductance in its own leads and foil, and putting parts in parallel divides both. Ten capacitors in parallel have a tenth of the equivalent series resistance, so they run cooler under ripple current and hold the rail steadier under a sudden load step. This is also why you find a 100 nF ceramic beside a 470 µF electrolytic beside a chip: the electrolytic supplies the bulk energy, the ceramic — low inductance, fast — supplies the first microsecond, and in parallel they cover a band neither covers alone.

The one big mistake is the combination rule itself, in mirror image: parallel capacitors add, series capacitors do not. Reaching for product-over-sum on a parallel pair gives an answer smaller than either part, which is your signal that the wrong rule has been applied — parallel connection can only ever increase capacitance. Two subtler points matter in practice. Ripple current in a parallel bank does not divide by capacitance; it divides by impedance, so a bank of mismatched parts overloads whichever has the lowest ESR while the others idle, and a bank should be built from identical parts. And the big-plus-small pairing described above can, at some megahertz frequency, form a parallel resonance between the small capacitor's capacitance and the large one's lead inductance, producing an impedance peak exactly where you wanted a low one. At mains and audio frequencies none of this matters and the addition is all you need.

Worked example: 10 uF and 22 uF in parallel → 32 uF

RC Time Constant

τ=RC\tau = R C
RCτ
Where
  • τ\tau= Time constant (s)
  • RR= Resistance (Ω)
  • CC= Capacitance (μF)

Ohms multiplied by farads give seconds, and that is not a coincidence. A farad is a coulomb per volt — how much charge a volt buys — and an ohm is a volt per ampere, an ampere being a coulomb per second. Multiply and the coulombs and volts cancel, leaving time. The physical reading is just as direct: CC says how much charge the capacitor must accumulate to reach a given voltage, RR says how slowly that charge is allowed to arrive, and τ=RC\tau = RC is the ratio of the job to the rate at which it can be done.

A 10 kΩ resistor with a 100 µF capacitor gives τ=10000×100×106=1 s\tau = 10\,000 \times 100 \times 10^{-6} = 1\ \text{s}. Charging from a supply, the capacitor covers 63.2% of the remaining gap in the first second, 86.5% by two seconds, 95% by three, and 99.3% by five — which is why 5τ is the working rule for "finished". The step sizes shrink because the driving voltage is the difference between the supply and what the capacitor has already reached, so as the gap closes the current that closes it falls in proportion. That self-limiting behaviour is what makes the curve exponential rather than a straight ramp.

The exponential is not asserted, it falls out of one line of calculus: the current through the resistor is (VsVC)/R(V_s - V_C)/R and it must equal CdVC/dtC\,dV_C/dt, giving RCdVC/dt=VsVCRC\,dV_C/dt = V_s - V_C, whose solution is VC=Vs(1et/RC)V_C = V_s(1 - e^{-t/RC}). Set t=τt = \tau and the bracket is 11/e=0.6321 - 1/e = 0.632. The inductive version on this site, τ=L/R\tau = L/R, is the same equation with the roles of the storage element and the resistor exchanged, and the RC discharge page is this one running downhill. Timing circuits, debounce networks, RC snubbers and the anti-aliasing filter in front of an ADC are all this constant chosen deliberately.

The unit slip is the most common failure by a wide margin. Capacitance is almost never quoted in farads — microfarads, nanofarads and picofarads are what appear on parts — and 10 kΩ with "100" entered as farads rather than microfarads produces a time constant of 10610^6 seconds, or eleven days. If an answer looks absurd, check the prefix first. The second mistake is misreading what τ measures: it is not the time to charge, and the capacitor never mathematically arrives at all. The third is using the wrong resistance. What matters is the total resistance in the charging path, including the source's internal resistance and anything you have connected to watch it — a 10 MΩ oscilloscope probe across a 1 µF capacitor imposes its own 10-second discharge whether you wanted one or not. And a circuit's charge and discharge paths are often different, through a diode or a separate bleeder, in which case it has two time constants and only one of them is RCRC as drawn.

Worked example: 2.2 kΩ with 470 µF → 1.034 s

RC Capacitor Discharge

V=V0et/τV = V_{0} \, e^{-t/\tau}
V0τVt
Where
  • VV= Voltage at time t (V)
  • V0V_{0}= Initial voltage (V)
  • tt= Elapsed time (s)
  • τ\tau= Time constant (s)

A capacitor discharging through a resistor loses the same fraction of what remains in every equal interval, not the same number of volts. The reason is a short feedback loop: the voltage on the capacitor is what drives current through the resistor, that current is what removes charge, and removing charge is what lowers the voltage. As the voltage falls the current falls with it, so the discharge slows exactly in step with its own progress. Any quantity whose rate of decrease is proportional to itself decays as et/τe^{-t/\tau}, and here τ=RC\tau = RC. After one time constant 36.8% of the original voltage is left, after two 13.5%, after three 5%, after five 0.7%.

Real numbers make the point better than percentages. A camera flash or a switch-mode supply may hold 470 µF at 400 V, bled off through a 1 MΩ resistor. That gives τ=470 s\tau = 470\ \text{s}, close to eight minutes. Five minutes after the unit is unplugged the capacitor is still at 400e300/470=211 V400\,e^{-300/470} = 211\ \text{V}; after a full ten minutes it is at 111 V, which will still hurt you. Inverting the relation gives the useful form: the time to fall to a chosen voltage is t=τln(V0/V)t = \tau \ln(V_0/V), so reaching a nominally safe 50 V from 400 V takes 470×ln8=977 s470 \times \ln 8 = 977\ \text{s}, sixteen minutes.

The mathematics is identical to radioactive decay, and the half-life language transfers directly: the voltage halves every τln2=0.693τ\tau \ln 2 = 0.693\tau, regardless of where you start counting. That is often the easier mental model — six and a bit half-lives to reach 1%. The same exponential governs the RC charging curve, thermal cooling under Newton's law, and the settling of a pressure transient in a pipe; whenever a store discharges through a restriction, this is the shape you get.

The dangerous misunderstandings here are all about "empty". Mathematically the capacitor never reaches zero, so any statement that it is discharged is a statement about a threshold someone chose. Worse, a large capacitor that has been shorted out and released will climb back up on its own — often to tens of volts — as charge trapped in the dielectric relaxes out of it. That effect is called dielectric absorption, or soakage, and it is why service procedures call for a bleeder resistor left in place rather than a screwdriver across the terminals, and why you measure before you touch rather than assuming. Two smaller traps: the exponential assumes the only discharge path is RR, so a real capacitor's own leakage and any parallel load shorten τ below the value you calculated; and when solving this page for tt or τ\tau the logarithm demands VV below V0V_0, because a discharging capacitor only ever loses voltage.

Worked example: 12 V after one time constant → 4.414553 V

RL Time Constant (τ = L/R)

τ=LR\tau = \frac{L}{R}
RLτ
Where
  • τ\tau= Time constant (s)
  • LL= Inductance (mH)
  • RR= Resistance (Ω)

Close a switch on a coil and the current does not jump to its final value — it climbs. The inductor generates a back-EMF proportional to how fast the current is changing, and that back-EMF eats into the voltage available to drive the current, so the rise is self-limiting in exactly the way an RC charge is. The current covers 63.2% of its remaining gap in each interval τ=L/R\tau = L/R, and is within 1% of its final V/RV/R after 5τ. The units check out because a henry is a volt-second per ampere and an ohm is a volt per ampere: divide and the volts and amperes cancel, leaving seconds.

A 100 mH relay coil wound to 50 Ω has τ=0.1/50=2 ms\tau = 0.1/50 = 2\ \text{ms}, so the current is essentially established after about 10 ms and the relay clicks in on that timescale — which is why mechanical relays are measured in milliseconds while transistors are measured in nanoseconds. Reduce the resistance and the coil gets slower, which is the counterintuitive part: τ is L/RL/R, so halving RR doubles the time constant even though it doubles the final current. A superconducting loop has R=0R = 0 and a time constant that is formally infinite, which is precisely why persistent-mode magnets hold their current for years.

The same constant governs the decay when the supply is removed, and that case is where the practical importance lies. The current will not stop, so it will find a path; if the only path is the opening switch contact, the inductor drives the voltage up until the air breaks down and the current continues as an arc. A flyback diode across the coil gives it a legal route instead. Note what the diode does to the timing: the decay's τ is set by the resistance in whatever loop the current ends up in, so a plain diode across the coil leaves only the winding resistance and the current takes a long time to die — which delays relay dropout — while adding a resistor or a Zener in that path shortens τ at the cost of a higher clamp voltage. Designers trade those two off deliberately.

Get the resistance right and the order of the division right. The RR that matters is every ohm in the current's loop — the winding's own DC resistance, the source's internal resistance, the sense resistor, the switch — and using only the external resistor when the coil itself has more resistance than it will give a τ that is badly wrong. Second, the arrangement is L/RL/R, not RLRL; the RC constant is a product and the RL constant is a quotient, and swapping them is the most common slip on this page. A quick sanity check: more inductance should mean slower, more resistance should mean faster. Third, inductance is often given in millihenries or microhenries and must be converted before dividing. And as with any inductor equation, an iron or ferrite core makes LL a function of current, so a coil approaching saturation has a shrinking time constant and its current rises faster than the calculation predicts.

Worked example: 100 mH, 50 ohm → tau = 2 ms

Energy Stored in an Inductor

E=12LI2E = \tfrac{1}{2} L I^{2}
ILE
Where
  • EE= Stored energy (J)
  • LL= Inductance (mH)
  • II= Current (A)

An inductor stores energy in the magnetic field it creates, and the half in E=12LI2E = \tfrac{1}{2}LI^2 has the same origin as the half in a capacitor's 12CV2\tfrac{1}{2}CV^2 or a spring's 12kx2\tfrac{1}{2}kx^2. Building the current is not free: the coil opposes any change in current with a back-EMF of Ldi/dtL\,di/dt, so the source must push against it the whole way up. That opposition grows in step with the current, from nothing at the start to its full value at the end, so the average is half the maximum and the work done is half of what a naive product would give. Integrate P=vi=Li(di/dt)P = vi = Li\,(di/dt) from zero to II and the half appears formally.

A 100 mH choke carrying 3 A holds 0.5×0.1×9=0.45 J0.5 \times 0.1 \times 9 = 0.45\ \text{J}. That sounds negligible until you ask how fast it can be released: interrupt that current in 10 µs and you are dissipating 45 kW while it lasts. Because the energy goes as the square of the current, a coil at twice the current holds four times as much — an important sizing fact, since it means an inductor's usable rating is set by the current it can carry without saturating far more than by its inductance.

The release is what makes inductors interesting. Open a switch on an energised coil and the current cannot stop instantly, because stopping it instantly would require infinite di/dtdi/dt; instead the collapsing field drives the terminal voltage to whatever value is needed to keep charge moving — through the air across the opening contacts, if that is the only path left. A car's ignition coil is this effect engineered on purpose, turning 12 V into a 30 kV spark by breaking a primary current. A switch-mode power supply does the same thing gently and tens of thousands of times a second, filling an inductor from the input and emptying it into the output, which is how a buck converter changes DC voltage with efficiency a resistor could never approach.

The mistakes here are mostly about symmetry that is not really there. A capacitor holds its energy at rest and will still bite you next week; an inductor's store exists only while the current flows, and cutting the current does not park the energy, it forces it out somewhere in the next few microseconds. Design for where it goes — a flyback diode, a snubber, a clamp — or the switch contacts and the transistor will volunteer. Second, LL in an iron-cored or ferrite-cored coil is not constant with current: as the core approaches saturation the inductance falls, sometimes by half, so 12LI2\tfrac{1}{2}LI^2 computed with the datasheet's small-signal inductance overstates the energy a saturating part actually holds, and the current rises much faster than expected. Third, on AC the current to use is the peak, not the RMS, because it is the instantaneous current that sets the instantaneous stored energy. And do not read the stored energy as a loss — it is returned to the circuit, unlike I2RI^2R heat, which is gone.

Worked example: 100 mH at 2 A → E = 0.2 J

RMS and Peak Voltage

Vrms=Vpeak2V_{rms} = \frac{V_{peak}}{\sqrt{2}}
VpeakVrms
Where
  • VrmsV_{rms}= RMS voltage (V)
  • VpeakV_{peak}= Peak voltage (V)

An alternating voltage spends most of its time somewhere below its peak and averages zero over a cycle, so "the" voltage of an AC supply needs defining before it means anything. The definition that earns its keep is the heating-equivalent one: the DC voltage that would deliver the same power to a resistor. Since power goes as V2V^2, you square the waveform, take the mean of the square over a cycle, and take the root of that — root-mean-square, done in that order. For a sine wave the mean of sin2\sin^2 over a cycle is exactly 1/21/2, so the RMS value is Vpeak/2V_{peak}/\sqrt{2}, about 0.707 of the peak. The 2\sqrt{2} is not a convention or a fudge; it is the square root of that one-half, and it belongs to the sine and to nothing else.

North American mains at 120 V RMS actually swings to 120×1.414=170 V120 \times 1.414 = 170\ \text{V} either side of neutral, 340 V peak to peak. A 230 V European supply reaches 325 V peak, 650 V peak to peak. A 24 V control transformer delivers 34 V peaks. Those peak numbers are the ones that matter when you choose an insulation rating, a rectifier's reverse voltage, or the working voltage of a filter capacitor — a 200 V capacitor across a 120 V circuit is not a comfortable margin, it is already an underrating.

The whole reason for the convention is that it makes the DC power formulas keep working. Feed 120 V RMS into P=V2/RP = V^2/R and the answer is the true average power in watts, no correction needed, which is precisely the property RMS was constructed to have. That is why meters, nameplates and every distribution standard quote RMS, and it is why the RMS value is what a thermal instrument naturally measures — an old thermocouple-type meter reads the heating effect directly and is right by construction.

Now the traps, and there are several worth knowing. The 2\sqrt{2} applies to a sine wave only. A square wave's RMS equals its peak; a triangle wave's is peak over 3\sqrt{3}; a rectified or chopped waveform is something else again. Second, and this catches working electricians: an ordinary averaging multimeter does not measure RMS at all. It rectifies, takes the average, and multiplies by 1.11 — a factor that assumes a sine. On the distorted current drawn by LED drivers, variable-frequency drives and switch-mode supplies, that meter can read 20 to 40% low, and only an instrument marked true RMS will tell you the truth. Third, keep peak and peak-to-peak straight: an oscilloscope shows peak-to-peak, which is twice the peak and 222\sqrt{2} times the RMS. Fourth, RMS current squared times resistance gives real heating, but RMS volts times RMS amps gives volt-amperes, not watts — the power factor still has to be applied. And never mix them within one calculation: peak volts with RMS amps produces an answer that is wrong by 41% and looks entirely reasonable.

Worked example: V_peak = 170 V → V_rms = 120.208 V

Inductive Reactance (X_L = 2πfL)

XL=2πfLX_L = 2\pi f L
LXLf
Where
  • XLX_L= Inductive reactance (Ω)
  • ff= Frequency (Hz)
  • LL= Inductance (mH)

An inductor opposes change in current, not current itself, so how hard it opposes depends on how fast you are asking the current to change. On a sine wave of frequency ff the current has to reverse 2f2f times a second, and the steepness of that reversal rises in proportion to the frequency — hence XL=2πfLX_L = 2\pi f L, climbing linearly. The 2π2\pi is there because a full cycle is 2π2\pi radians, and the group 2πf2\pi f is angular frequency ω\omega, which is why the relation is more compactly written XL=ωLX_L = \omega L. At DC, where nothing changes, the reactance is zero and the coil is just its own winding resistance.

A 10 mH coil offers 2π×60×0.01=3.8 Ω2\pi \times 60 \times 0.01 = 3.8\ \Omega at 60 Hz mains, 63 Ω at 1 kHz, and 628 Ω at 10 kHz. That strong frequency preference makes an inductor a natural low-pass element: put it in series with a load and the low frequencies get through while the high ones are held back. A loudspeaker crossover does exactly this, an inductor in series with the woofer passing bass and blocking treble, while a capacitor does the complementary job for the tweeter. The same principle is at work in a mains filter choke and in the smoothing inductor of a power supply.

Reactance is what an inductor contributes to the circuit's impedance, Z=R+jXLZ = R + jX_L, where the jj records that the voltage across an inductor leads its current by 90°. This quarter-cycle lag is the physical heart of the matter: current lags voltage in a coil because the coil resists getting started, and it is the reason an inductive motor load drags a plant's power factor down and needs correcting with capacitors. On the site's LC resonance page the inductive and capacitive reactances become equal and, because they are opposite in sign, cancel — the whole subject of tuning is contained in that cancellation.

Reactance is measured in ohms, and that is the single most misleading fact about it. It is not resistance and it does not behave like resistance in three important ways. First, it dissipates no power: the energy goes into the magnetic field on one quarter-cycle and comes back out on the next, so a pure reactance heats nothing, and a wattmeter across it reads zero. Second, it does not add arithmetically to resistance. A coil with 30 Ω of winding resistance and 40 Ω of reactance presents 302+402=50 Ω\sqrt{30^2 + 40^2} = 50\ \Omega, never 70, because the two are 90° apart and combine in quadrature. Third, it is frequency-specific, so a single number is meaningless without the frequency it was computed at — and on a supply carrying harmonics, the fifth harmonic sees five times the reactance the fundamental does, which is why harmonic currents can produce voltage distortion far out of proportion to their size. Finally, this page gives the reactance alone; to find the current from a supply voltage you need the full impedance, resistance included.

Worked example: 10 mH at 60 Hz → X_L = 3.76991 ohm

Capacitive Reactance (X_C = 1/2πfC)

XC=12πfCX_C = \frac{1}{2\pi f C}
CXCf
Where
  • XCX_C= Capacitive reactance (Ω)
  • ff= Frequency (Hz)
  • CC= Capacitance (μF)

No charge crosses the gap between a capacitor's plates, yet a capacitor plainly passes alternating current. What actually happens is that charge piles onto one plate and off the other, and if the supply reverses before much has accumulated, the opposing voltage never gets large and current keeps flowing freely. The faster the alternation, the less charge accumulates per half-cycle and the less the capacitor pushes back — so its opposition falls as frequency rises, XC=1/(2πfC)X_C = 1/(2\pi f C). This is the exact mirror of the inductor, which opposes more as frequency rises, and the two mirror each other in sign as well as in shape.

A 1 µF capacitor presents 1/(2π×60×106)=2.65 kΩ1/(2\pi \times 60 \times 10^{-6}) = 2.65\ \text{k}\Omega at 60 Hz, 159 Ω at 1 kHz, and 0.16 Ω at 1 MHz — from a substantial obstacle to a near short circuit across that range. That is the whole basis of bypassing: a 100 nF capacitor from a supply rail to ground is 26 kΩ at mains frequency, so it draws nothing, but a fraction of an ohm at the megahertz where a digital chip's switching noise lives, where it acts as a local reservoir. In a loudspeaker crossover the same behaviour puts a capacitor in series with the tweeter, blocking bass and passing treble.

At DC the relation gives infinity, and that is the honest answer: once charged, a capacitor is an open circuit, which is why this page refuses f=0f = 0 rather than returning a number. That property is as useful as the frequency dependence — a coupling capacitor passes an audio signal while blocking the DC bias on either side of it, and every AC-coupled amplifier stage depends on it. The complementary behaviours of XLX_L and XCX_C meet on the LC resonance page, where at one frequency they are equal and, being opposite in sign, cancel entirely.

The first trap is the one shared with inductive reactance: ohms are not resistance. A capacitor dissipates no power — the current leads the voltage by 90°, energy flows in and back out each quarter-cycle, and a wattmeter reads zero. It follows that reactance never adds arithmetically to resistance: 30 Ω of resistance in series with 40 Ω of capacitive reactance is 50 Ω of impedance. The second trap is specific to this page. Inductive and capacitive reactances are opposite in sign, +jXL+jX_L against jXC-jX_C — so in a series circuit they subtract, and the net is X=XLXCX = X_L - X_C before you take the quadrature sum with RR. Add them and you will get an answer that is not merely wrong but wrong in the direction that hides resonance completely. Third, a real capacitor is not pure: its equivalent series resistance does dissipate, which is what heats an electrolytic under ripple current and eventually kills it, and above its self-resonant frequency a capacitor's own lead inductance takes over and it starts behaving inductively — a bypass capacitor used above that point is doing nothing you intended.

Worked example: 1 uF at 60 Hz → X_C = 2652.58 ohm

Series RL or RC Impedance

Z=R2+X2Z = \sqrt{R^{2} + X^{2}}
RXZ
Where
  • ZZ= Impedance magnitude (Ω)
  • RR= Resistance (Ω)
  • XX= Reactance (Ω)

A resistor's voltage is in phase with its current, a reactance's is a quarter cycle away, so their oppositions add as the legs of a right triangle: 40 Ω of resistance with 30 Ω of reactance gives 50 Ω, not 70 Ω. This is the everyday impedance calculation — the winding resistance and inductance of a relay coil, a contactor, a transformer primary, a loudspeaker crossover leg.

The same triangle hands you the phase angle, φ = arctan(X/R), and hence the power factor cos φ = R/Z. That is worth remembering when you meet an inductive load with no nameplate: measure the DC resistance, measure the AC current at a known voltage to get Z, and the power factor falls out of the ratio. Rough numbers are enough to tell a mostly resistive load from a mostly reactive one.

Worked example: 40 Ω R with 30 Ω X → 50 Ω

Series RLC Impedance

Z=R2+(XLXC)2Z = \sqrt{R^{2} + (X_{L} - X_{C})^{2}}
RXL − XCZ
Where
  • ZZ= Impedance magnitude (Ω)
  • RR= Resistance (Ω)
  • XLX_{L}= Inductive reactance (Ω)
  • XCX_{C}= Capacitive reactance (Ω)

Reactances are 90° out of phase with resistance and 180° out of phase with each other, so they subtract first and then join R by Pythagoras. With R = 30 Ω, XL = 80 Ω and XC = 40 Ω, the net reactance is 40 Ω and Z=302+402=50Z = \sqrt{30^2 + 40^2} = 50 Ω. Note that reactances can each be far larger than the total impedance — at resonance they cancel exactly and Z collapses to R alone, which is how a tuned circuit picks one station out of the air.

Because the square root discards sign, solving for a reactance has two answers; this brain returns the inductive-dominant branch (XL above XC), so subtract the root instead if you know the circuit is capacitive. The practical warning: never add reactances arithmetically to resistance. A 300 Ω coil in series with 400 Ω of resistance is 500 Ω, not 700 Ω, and a meter that reads otherwise is measuring DC.

Worked example: 30 Ω with 80 Ω XL and 40 Ω XC → 50 Ω

Phase Angle from Power Factor

φ=arccos(PF)\varphi = \arccos(\text{PF})
φPF
Where
  • φ\varphi= Phase angle (°)
  • PF\text{PF}= Power factor

Power factor and phase angle are the same fact in two languages. A PF of 0.8 means the current waveform is 36.87° out of step with the voltage — the 3-4-5 triangle again, since cos 36.87° = 0.8 and sin 36.87° = 0.6. Once you have φ you can get the reactive burden directly as Q = P tan φ, which is how correction tables are built.

The number alone does not say which way: motors and transformers pull lagging current (current behind voltage), while capacitor banks and lightly loaded long cables push leading current. Both give the same cos φ, so meters mark them separately, and it matters — leading power factor on a weak system raises voltage rather than lowering it. Note this calculator works in radians internally and displays degrees.

Worked example: PF 0.8 → 36.87° lag

LC Resonant Frequency

f=12πLCf = \frac{1}{2\pi\sqrt{LC}}
LCf
Where
  • ff= Resonant frequency (Hz)
  • LL= Inductance (mH)
  • CC= Capacitance (μF)

Connect a charged capacitor across an inductor and the energy does not simply drain away — it sloshes. The capacitor discharges into the coil, building a magnetic field; when the capacitor is empty the field is at its peak, and a collapsing field keeps the current going, so it charges the capacitor back up the other way round. The cycle repeats at one natural frequency. It is the electrical twin of a mass bouncing on a spring, with inductance playing the part of mass — the reluctance to change velocity, or current — and 1/C1/C playing stiffness. The frequency comes from setting the two reactances equal: 2πfL=1/(2πfC)2\pi f L = 1/(2\pi f C), solve for ff, and you have f=1/(2πLC)f = 1/(2\pi\sqrt{LC}).

A 100 µH coil with a 250 pF capacitor rings at 1/(2π104×2.5×1010)=1.01 MHz1/(2\pi\sqrt{10^{-4} \times 2.5 \times 10^{-10}}) = 1.01\ \text{MHz}, the middle of the AM broadcast band. The square root makes the circuit reassuringly insensitive: to double the frequency you must quarter the product LCLC, so a 10% error in a capacitor moves the resonance by only 5%. Turning the tuning knob on an old radio physically rotated the vanes of a variable capacitor, sliding this frequency across the dial, and the whole receiver amounted to that one circuit picking one station out of the air.

Every radio transmitter, every RFID tag, every induction hob and every crystal oscillator descends from this arrangement. Heinrich Hertz used a spark-excited LC circuit in 1887 to generate and detect the first deliberate radio waves, confirming Maxwell's prediction; Marconi turned the same circuit into a business within a decade. The relation also explains why antennas have a length: a resonant antenna is an LC circuit whose inductance and capacitance are distributed along the conductor rather than lumped into parts.

Four things go wrong. The commonest by far is the factor of 2π2\pi: ff is in hertz, ω=2πf=1/LC\omega = 2\pi f = 1/\sqrt{LC} is in radians per second, and the two differ by 6.28. Half the confusion in filter design traces to a formula quoted in one and used as the other. Second, prefixes — microhenries and picofarads must both be converted before multiplying, and an error here moves the answer by orders of magnitude, not percent. Third, this is the undamped natural frequency. Real circuits have resistance, which shifts the actual resonance slightly lower and, more importantly, sets how sharp it is: the quality factor Q=(1/R)L/CQ = (1/R)\sqrt{L/C} governs the bandwidth, and a lossy coil gives a broad, useless peak at the right frequency. Fourth, series and parallel LC circuits share this formula and behave in opposite ways at it. A series LC becomes a near short circuit at resonance, with the voltage across each component rising to QQ times the supply — a genuine hazard, since a modest input can put hundreds of volts across a capacitor. A parallel LC becomes a near open circuit. Choosing the wrong one gives a circuit that does the exact opposite of what was intended at precisely the frequency you designed for.

Worked example: 100 uH + 250 pF → f = 1.00658 MHz

Q Factor of a Series Resonant Circuit

Q=1RLCQ = \frac{1}{R} \sqrt{\frac{L}{C}}
QRLC
Where
  • QQ= Quality factor
  • RR= Series resistance (Ω)
  • LL= Inductance (mH)
  • CC= Capacitance (μF)

Q is the ratio of energy stored to energy lost per radian of oscillation, and for a series circuit that works out to L/C/R\sqrt{L/C}/R. It sets the bandwidth — BW = f₀/Q — so a 100 µH coil with 250 pF and 5 Ω of loss gives Q ≈ 126, meaning a 1 MHz resonance only 8 kHz wide. That selectivity is what lets a receiver hear one station while ignoring its neighbour.

The startling part is voltage magnification: at resonance the voltage across the inductor (and across the capacitor) is Q times the applied voltage, even though they cancel each other in the sum. Feed 10 V into that circuit and the coil sits at 1.26 kV. Bench technicians have destroyed capacitors this way, and power engineers watch for the same effect when a capacitor bank resonates with system inductance at a harmonic frequency.

Worked example: 100 µH, 250 pF, 5 Ω → Q ≈ 126.5

Bandwidth from Q and Centre Frequency

BW=f0QBW = \frac{f_{0}}{Q}
BWf₀Q
Where
  • BWBW= Bandwidth (Hz)
  • f0f_{0}= Centre (resonant) frequency (Hz)
  • QQ= Quality factor

Bandwidth and quality factor are two ways of saying how sharp a resonance is: BW=f0/QBW = f_0/Q, measured between the half-power points either side of centre. A 1 MHz tuned circuit with Q of 125 passes an 8 kHz-wide slice, which is roughly what an AM broadcast channel needs. Raise Q and the passband narrows in exact proportion.

The reason a broadcast receiver's intermediate-frequency strip exists is buried in that ratio. Getting a 10 kHz window at 1 MHz needs Q = 100; getting the same window at 100 MHz would need Q = 10,000, which no ordinary LC circuit reaches. So a superheterodyne mixes everything down to a fixed 455 kHz, where Q of only 45.5 does the job, and the selectivity stops depending on where you tuned. That is Edwin Armstrong's 1918 insight and it is in every radio since.

Two cautions. Q is not a property of the coil alone — connect a load across a tank circuit and you have added loss, so the loaded Q is lower and the bandwidth wider than the components suggest. And selectivity is not free: a filter narrower than the signal chews the sidebands off, so an over-sharp IF makes speech muffled and, in a data link, smears symbols into each other. Bandwidth and rise time are the same constraint viewed from two ends.

Worked example: 1 MHz at Q = 125 → 8 kHz bandwidth

RC Cutoff Frequency

fc=12πRCf_{c} = \frac{1}{2\pi R C}
fcRC
Where
  • fcf_{c}= Cutoff frequency (Hz)
  • RR= Resistance (Ω)
  • CC= Capacitance (μF)

The corner frequency of an RC filter is where the capacitor's reactance 1/2πfC1/2\pi f C has fallen to equal the resistance. There the output is 0.707 of the input — half the power, hence "−3 dB" — and the phase has shifted 45°. A 1 kΩ resistor with 0.1 µF gives 1/(2π×104)15921/(2\pi \times 10^{-4}) \approx 1592 Hz. Above that corner a low-pass output rolls off at 6 dB per octave and keeps rolling forever.

The name "cutoff" is the misleading part: nothing is cut off. At the corner you still have 71% of the signal, and one octave above you still have about half. A single RC section is a gentle slope, not a wall, which is why anti-aliasing filters ahead of an ADC use multiple poles and why putting a filter corner right at the edge of the wanted band always disappoints. Set the corner well clear of what you want to keep.

The other trap is loading. This formula assumes nothing draws current from the output; a following stage with an impedance comparable to R shifts the corner and shrinks the passband gain. And note the same components in the time domain give the time constant τ=RC\tau = RC, so fc=1/2πτf_c = 1/2\pi\tau — the corner frequency and the 63% charging time are the same fact told twice. Swap which component the output is taken across and the identical corner becomes a high-pass instead.

Worked example: 1 kΩ with 0.1 µF → 1591.5 Hz

RL Cutoff Frequency

fc=R2πLf_{c} = \frac{R}{2\pi L}
fcRL
Where
  • fcf_{c}= Cutoff frequency (Hz)
  • RR= Resistance (Ω)
  • LL= Inductance (mH)

An RL filter corners where the inductive reactance 2πfL2\pi f L has grown to equal the resistance, giving fc=R/2πLf_c = R/2\pi L. Fifty ohms with a 10 mH choke corners at about 796 Hz. Above that the inductor dominates and current falls; below it the resistor dominates and the inductor is barely there. The behaviour mirrors the RC case exactly, with the roles of "rising" and "falling" reactance swapped.

Notice that raising the resistance raises the corner, which feels backwards until you see it as a race: the corner is where reactance catches up with resistance, so a bigger target takes a higher frequency to reach. The same reasoning gives the time-domain view, since τ=L/R\tau = L/R and fc=1/2πτf_c = 1/2\pi\tau again — a larger R makes the inductor's current settle faster, not slower.

In practice RC is preferred wherever it will do the job, because inductors are big, expensive, magnetically noisy and never ideal: a real coil has winding resistance, interwinding capacitance and a self-resonance above which it stops being an inductor at all. RL earns its place where high current makes capacitors impractical — mains filters, switching supply output chokes, motor drive dV/dt filters — and in the humbler case of a relay coil, where the same L/R that defines this corner is what decides how long the contacts take to drop out.

Worked example: 50 Ω with 10 mH → 795.8 Hz

Decibel Voltage Gain

GdB=20log10 ⁣(V2V1)G_{dB} = 20 \log_{10}\!\left(\frac{V_{2}}{V_{1}}\right)
V₁GV₂
Where
  • GdBG_{dB}= Gain (dB)
  • V2V_{2}= Output voltage (V)
  • V1V_{1}= Input voltage (V)

Power goes as voltage squared, and the log of a square is twice the log — so a voltage ratio wears a 20 where a power ratio wears a 10. Ten volts out for one volt in is 20 dB; a 40 dB preamp multiplies 50 mV up to 5 V. Handy landmarks: 6 dB is a doubling of voltage, 20 dB is ten times, −3 dB is the 0.707 point that defines a filter's corner frequency.

Strictly, equating a voltage ratio to a power ratio in dB assumes the input and output see the same impedance — an assumption from the days when everything was 600 Ω. Modern audio and instrumentation ignore it and use 20 log of voltage as a convention, which is fine as long as everyone in the conversation agrees. Where absolute level is meant, look for the suffix: dBV references 1 V, dBu references 0.7746 V (1 mW into 600 Ω).

Worked example: 1 V to 10 V → 20 dB

Decibel Power Gain

GdB=10log10 ⁣(P2P1)G_{dB} = 10 \log_{10}\!\left(\frac{P_{2}}{P_{1}}\right)
P₁GP₂
Where
  • GdBG_{dB}= Gain (dB)
  • P2P_{2}= Output power (W)
  • P1P_{1}= Input power (W)

Bell Telephone engineers needed a way to add up losses along a line instead of multiplying them, so they took logarithms; the bel proved too coarse and the decibel — a tenth of one — stuck. Ten times log of the power ratio means 3 dB is a doubling, 10 dB is ten times, 20 dB is a hundred times, and 100 W out of 1 W in is a 20 dB gain. Cascade stages and the decibels simply add.

The trap is the reference. A plain dB is a ratio and says nothing about absolute level; dBm fixes P₁ at 1 mW, so 30 dBm is exactly 1 W and 0 dBm is 1 mW. Mixing the two — treating a gain in dB as a level in dBm — is a classic RF blunder. Remember also that this 10-log form is only for power; voltage and current ratios use 20 log, since power goes as the square.

Worked example: 1 W to 100 W → 20 dB

AC Power & the Bill

Single-Phase Real Power with Power Factor

P=VIPFP = V I \, \text{PF}
PIVPF
Where
  • PP= Real power (W)
  • VV= Line voltage (V)
  • II= Line current (A)
  • PF\text{PF}= Power factor

On DC, watts are simply volts times amps. On AC the current can lag or lead the voltage, and only the in-phase component delivers energy; the power factor cos φ is the bookkeeping for that. A 240 V single-phase welder pulling 20 A at 0.95 PF consumes 240 × 20 × 0.95 = 4560 W, not the 4800 VA its supply cable and breaker must actually carry.

Resistive loads — heaters, incandescent lamps, kettles — sit at PF = 1, which is why the clamp-meter product matches the wattmeter on those and not on a motor. Watch out for modern electronics: a switching power supply may draw badly distorted current, giving a total power factor well below the displacement cos φ this formula assumes, so the meter reading and the calculation drift apart.

Worked example: 240 V, 20 A, 0.95 PF → 4560 W

Power Factor from Real and Apparent Power

PF=PS\text{PF} = \frac{P}{S}
PFPS
Where
  • PF\text{PF}= Power factor
  • PP= Real power (W)
  • SS= Apparent power (VA) (W)

Power factor is an efficiency of delivery, not of conversion: it says how much of the capacity you rented from the utility is producing work. A load reading 8 kW on the wattmeter but 10 kVA on the volt-amp meter runs at PF = 0.8, meaning a fifth of the supplied capacity is sloshing back and forth building magnetic fields instead of turning shafts. Both fields here are watt fields; enter kVA in the kW box, since VA and W are the same dimension.

Utilities care because that reactive current still heats their conductors and transformers, so large customers face a power-factor penalty — often triggered below 0.9 or 0.95. Lightly loaded induction motors are the usual culprit, drifting to 0.3–0.5 PF at no load; the standard cures are capacitor banks and, better, not oversizing motors in the first place.

Worked example: 8 kW out of 10 kVA → PF 0.8

Reactive Power (Power Triangle)

Q=S2P2Q = \sqrt{S^{2} - P^{2}}
QPS
Where
  • QQ= Reactive power (var) (W)
  • SS= Apparent power (VA) (W)
  • PP= Real power (W)

Real power P and reactive power Q are 90° apart, so they add like the legs of a right triangle with apparent power S as the hypotenuse: S² = P² + Q². A load pulling 10 kVA while doing 8 kW of work is carrying 10282=6\sqrt{10^2 - 8^2} = 6 kvar of reactive burden — the classic 3-4-5 triangle in electrical dress. Vars are watts dimensionally, so enter kvar and kVA in the kW fields here.

Reactive power does no net work over a cycle; it is energy borrowed to build a magnetic field and returned half a cycle later. The borrowing is not free — the round trip flows as real current through your conductors and the utility's transformers. That is why the fix is local: put capacitors near the motor and the vars shuttle between motor and capacitor instead of travelling back to the substation.

Worked example: 10 kVA with 8 kW → 6 kvar

Three-Phase Real Power

P=3VLILPFP = \sqrt{3} \, V_{L} I_{L} \, \text{PF}
MPVLILPF
Where
  • PP= Real power (W)
  • VLV_{L}= Line-to-line voltage (V)
  • ILI_{L}= Line current (A)
  • PF\text{PF}= Power factor

The √3 is the whole story of three-phase power. Each of the three phases carries Vphase × Iphase, but the meter and the nameplate quote line quantities, and the 120° spacing between phases turns the sum of three phase powers into √3 × VL × IL. Multiply by the power factor and you have the real, billable, heat-and-torque-producing watts. A 480 V feeder carrying 100 A at 0.85 PF delivers 1.732 × 480 × 100 × 0.85 ≈ 70.7 kW.

The trap is mixing line and phase values: the √3 belongs in the formula only when VL and IL are both line quantities. Drop the power factor and you get apparent power in VA, not watts — the two differ by 15% on that feeder, which is exactly why a 100 kVA transformer will not carry 100 kW of motor load. Nikola Tesla's polyphase patents of 1888 made this arithmetic the foundation of every industrial plant since.

Worked example: 480 V, 100 A, 0.85 PF → 70.67 kW

Three-Phase Apparent Power

S=3VLILS = \sqrt{3} \, V_{L} I_{L}
SVLIL
Where
  • SS= Apparent power (VA) (W)
  • VLV_{L}= Line-to-line voltage (V)
  • ILI_{L}= Line current (A)

Apparent power is the product the copper actually feels: every amp heats the conductor whether or not it is in phase with the voltage. Volt-amperes and watts have identical dimensions — this solver's watt fields double as volt-amperes, and kW as kVA — but tradition keeps the names separate to remind you that S ≥ P always. A 208 V panel drawing 50 A per line is handling 1.732 × 208 × 50 ≈ 18 kVA regardless of what the loads are doing.

This is the number on a transformer's nameplate, and the reason it is: the transformer's limits are its winding heat (amps) and its core saturation (volts), neither of which knows anything about power factor. To size a service, work in kVA; to size a bill or a generator's engine, work in kW. Drop the √3 for single-phase and the formula is just S = VI.

Worked example: 208 V, 50 A → 18.01 kVA

Wye Line and Phase Voltage

VL=3VφV_{L} = \sqrt{3} \, V_{\varphi}
VφVL
Where
  • VLV_{L}= Line-to-line voltage (V)
  • VφV_{\varphi}= Phase (line-to-neutral) voltage (V)

Two phases of a wye are not simply additive because they peak 120° apart; the vector difference of two equal phasors 120° apart is √3 times either one. That single fact names every common system: 120/208 V (208 = √3 × 120), 277/480 V (480 = √3 × 277), and 230/400 V across most of the world. In a wye the line current equals the phase current — it is only the voltages that get the √3.

The practical consequence is that one transformer bank feeds two voltages: lighting and receptacles hang line-to-neutral at 120 V or 277 V, while motors and heaters take line-to-line at 208 V or 480 V. The trap is assuming 240 V single-phase equipment will work on a 208 V wye leg — it sees 208 V, and a heater delivers only (208/240)² ≈ 75% of its rated output.

Worked example: 277 V phase → 480 V line

Delta Line and Phase Current

IL=3IφI_{L} = \sqrt{3} \, I_{\varphi}
IφIL
Where
  • ILI_{L}= Line current (A)
  • IφI_{\varphi}= Phase (winding) current (A)

Delta is wye's mirror image: the windings sit directly across the lines, so phase voltage equals line voltage, but each line conductor collects current from two windings that are 120° apart — giving the same √3, this time on the current. A delta motor winding carrying 10 A per coil draws 17.32 A in each line lead.

This is exactly why a wye-delta starter works. Started in wye, each winding sees only VL/√3, so the winding current drops by √3 and the line current by three; the motor starts on about a third of its delta inrush and a third of the torque, then switches to delta for full running duty. The trap in the field is the six-lead terminal box: reconnect a 400 V delta motor as wye and it runs at 58% voltage and stalls under load.

Worked example: 10 A per winding → 17.32 A line

Power-Factor Correction kvar

Qc=P(tanφ1tanφ2)Q_{c} = P \left( \tan\varphi_{1} - \tan\varphi_{2} \right)
QcPF₁PF₂P
Where
  • QcQ_{c}= Correction reactive power (var) (W)
  • PP= Load real power (W)
  • PF1\text{PF}_{1}= Existing power factor
  • PF2\text{PF}_{2}= Target power factor

Each power factor corresponds to a phase angle φ = arccos(PF), and the reactive burden of a load is P tan φ. To move from a poor PF₁ to a target PF₂ you must cancel the difference in those vars, which is what a capacitor bank does. A 100 kW plant at 0.70 PF carries 100 × 1.020 = 102 kvar; at 0.95 PF it would carry only 32.9 kvar, so about 69 kvar of capacitors closes the gap.

Two field cautions. Chasing unity is a mistake — the last few points cost the most capacitors, and an overcorrected plant goes leading, which can push voltage up and, on a motor that keeps spinning after the contactor opens, cause damaging self-excitation. And where the harmonic content is high, plain capacitors resonate with the supply inductance and amplify the harmonics; detuned reactors are then part of the package.

Worked example: 100 kW from 0.70 to 0.95 PF → 69.15 kvar

Power-Factor Correction Capacitance

C=Qc2πfV2C = \frac{Q_{c}}{2\pi f V^{2}}
CVQcf
Where
  • CC= Capacitance (μF)
  • QcQ_{c}= Reactive power wanted (var) (W)
  • ff= Supply frequency (Hz)
  • VV= Voltage across the capacitor (V)

A capacitor's vars are Q = V²/XC, and since XC = 1/(2πfC), that rearranges to Q = 2πfCV² — solve it for C and you have your capacitor. Getting 5 kvar at 240 V and 60 Hz takes 5000/(2π × 60 × 240²) ≈ 230 µF, a physically large oil-filled can, which is why correction capacitors are bulky and why higher voltages are so much cheaper per var. The var field here uses watts: vars and watts share dimensions.

The V² is the sting. A capacitor bank rated 25 kvar at 480 V delivers only 25 × (240/480)² ≈ 6.25 kvar if someone installs it on a 240 V system — a mistake that shows up as a stubbornly unimproved power factor. Frequency matters the same way, so a bank imported from a 50 Hz country loses a fifth of its vars at 60 Hz... and gains 20% the other way, along with the overcurrent that comes with it.

Worked example: 5 kvar at 240 V, 60 Hz → 230.26 µF

Electrical Energy (E = Pt)

E=PtE = P t
EPt
Where
  • EE= Energy (J)
  • PP= Power (W)
  • tt= Time (s)

Power is the rate at which energy is delivered, so energy is power kept up for a while. That is all E=PtE = Pt says, and like every rate-times-time relation it is true by definition rather than by discovery — a watt is a joule per second, so watts multiplied by seconds give joules back. The distinction it enforces is the one people most often lose: power is not energy. A 2000 W heater is not consuming 2000 of anything; it is consuming at a rate of 2000 joules every second, and what it costs depends entirely on how long you leave it on.

Utilities meter in kilowatt-hours because the joule is inconveniently small: 1 kWh is 1000 W sustained for 3600 s, or exactly 3.6×1063.6 \times 10^{6} J. A 1500 W baseboard heater running six hours a day for a thirty-day month uses 1.5×6×30=270 kWh1.5 \times 6 \times 30 = 270\ \text{kWh}; at ten cents a kilowatt-hour that is $27 on the bill. The same 270 kWh would run a 15 W LED lamp continuously for about two years. Energy comparisons like that are the only honest way to judge where a bill actually goes, and they almost always show that the heating and hot water dwarf everything with a screen on it.

The kilowatt-hour is a compound unit of the sort engineers usually avoid, and it survives because it matches how people buy electricity: a rate you can read off a nameplate multiplied by hours you can read off a clock. Watt-hours, ampere-hours and joules all measure the same physical stock of energy in different currencies: 1 Wh=3600 J1\ \text{Wh} = 3600\ \text{J}, and an ampere-hour becomes watt-hours only after you multiply by the voltage. On the site's other pages this same relation appears as work over time in mechanics; there is no separate electrical version of it, only a separate unit.

The assumption doing the quiet work here is constant power, and most real loads are not. A thermostatted heater is either fully on or fully off, so its average power over an hour is the rated power times its duty cycle — a 1500 W baseboard cycling a third of the time is a 500 W load as far as the meter is concerned, and using the nameplate figure triples the estimate. A refrigerator, a well pump and a furnace blower all behave the same way. The other trap is a billing one worth knowing if you read a commercial invoice: those bills carry both an energy charge in kilowatt-hours and a demand charge in kilowatts, set by the highest fifteen-minute average draw in the period. The demand charge is a power charge, this equation does not produce it, and no amount of shortening run times will reduce it — only flattening the peak will.

Worked example: 60 W for 120 s → 7200 J

Energy Cost from a Utility Rate

Ce=EpeC_e = E \, p_e
Where
  • CeC_e= Energy cost ($)
  • EE= Energy consumed (kWh)
  • pep_e= Energy rate ($/kWh)

Water is not the only meter a cooling system spins. Tower fans, condenser-water pumps and the compressor itself all draw power, and boilers burn gas — so the same product, energy times a rate, prices both. A tower's fans and pumps drawing 250,000 kWh a year at $0.11/kWh cost $27,500; a boiler burning 20,000 MMBTU of gas at $8.00/MMBTU costs $160,000. North American electricity sits around $0.08–0.15/kWh commercial and natural gas around $6–10/MMBTU, but demand charges, ratchets and time-of-use blocks mean the effective rate on a bill is often well above the headline commodity rate — take it from the bill, dividing total dollars by total kilowatt-hours, rather than from the tariff sheet.

This calculation is what makes the water-treatment argument financial rather than technical. Scale is an insulator: a 0.6 mm (1/64 in) carbonate film on condenser tubes lifts compressor power by roughly 20%, and on a plant with a six-figure electricity bill that dwarfs the entire chemical budget. The same arithmetic prices the other direction too — boiler blowdown leaves at saturation temperature, so every percent of continuous blowdown costs a fraction of a percent of fuel, and a blowdown heat exchanger's payback is nothing more than this equation applied to recovered energy. Energy is entered and answered in kilowatt-hours and the rate in dollars per kilowatt-hour regardless of the metric/imperial toggle, because that is how every electricity meter on earth reads; and as with every money answer here, the currency is whatever currency you typed the rate in.

Worked example: 20,000 MMBTU of gas at $8.00/MMBTU → $160,000

Voltage Drop, Single Phase

Vd=2ρLIAV_{d} = \frac{2 \rho L I}{A}
AρIVdL
Where
  • VdV_{d}= Voltage drop (V)
  • ρ\rho= Conductor resistivity (Ω·m)
  • LL= One-way run length (m)
  • II= Load current (A)
  • AA= Conductor area ()

Every conductor is a resistor, and Ohm's law does the rest: the current travels out and back, so the drop is 2 × ρL/A × I. Work in SI and no mystery constant is needed — copper is about 1.72 × 10⁻⁸ Ω·m (1.72 μΩ·cm) at 20 °C, aluminium about 2.82 × 10⁻⁸. Feeding a 20 A load 50 m away on 4 mm² copper drops 2 × 1.72e−8 × 50 × 20 / 4e−6 = 8.6 V, unacceptable on a 230 V circuit and a clear call for larger cable.

North American practice hides the same physics in the constant K in Vd = 2KIL/cmil, where K ≈ 12.9 Ω·cmil/ft for copper and 21.2 for aluminium — those numbers are just ρ expressed in circular-mil-feet. Two traps: use the one-way run length (the 2 is already there), and remember K rises with temperature, which is why 12.9 is a 75 °C figure while cold-copper calculations use about 10.4.

Worked example: 20 A, 50 m, 4 mm² copper → 8.6 V drop

Voltage Drop, Three Phase

Vd=3ρLIAV_{d} = \frac{\sqrt{3} \, \rho L I}{A}
AρIVdL
Where
  • VdV_{d}= Line-to-line voltage drop (V)
  • ρ\rho= Conductor resistivity (Ω·m)
  • LL= One-way run length (m)
  • II= Line current (A)
  • AA= Conductor area ()

On a balanced three-phase circuit the three currents sum to zero, so no return conductor carries them home. Each line drops ρLI/A line-to-neutral, and converting that to a line-to-line figure multiplies by √3 — which is why three-phase drop is only 86.6% of the single-phase drop for the same current, length and cable. Running 50 A 100 m on 25 mm² copper gives 1.732 × 1.72e−8 × 100 × 50 / 25e−6 ≈ 5.96 V, about 1.2% on a 480 V system.

This resistive form is what most codes accept for typical building circuits, but it ignores reactance. On large conductors, long runs, or poor power factor, cable inductance adds its own drop and the true answer needs Vd = √3 I (R cos φ + X sin φ). For 4/0 and larger, or anything over a few hundred feet, use the impedance tables — the resistive answer can be optimistic by a third.

Worked example: 50 A, 100 m, 25 mm² copper → 5.96 V drop

Percent Voltage Drop

%Vd=100VdVs\%V_{d} = \frac{100 \, V_{d}}{V_{s}}
VdVs%Vd
Where
  • %Vd\%V_{d}= Percent voltage drop (%)
  • VdV_{d}= Voltage drop (V)
  • VsV_{s}= Supply voltage (V)

Volts lost only mean something relative to volts supplied: 6.9 V is a trivial loss on 4160 V and a serious one on 230 V, where it is 3%. The familiar limits — the NEC's informational 3% on a branch circuit and 5% overall, and similar figures in IEC and CEC practice — are recommendations aimed at equipment performance, not safety minimums, but designers treat them as hard rules because the consequences are real.

Undervoltage is unkind to motors in particular: torque falls with the square of voltage, so a motor at 90% voltage makes only 81% of its torque and pulls extra current to compensate, running hotter for it. Incandescent lamps dim visibly at a few percent, and electronic supplies simply draw more amps as voltage sags, deepening the drop. Note this solver's percent fields also accept a plain fraction.

Worked example: 6.9 V lost on 230 V → 3%

Peukert's Law (Battery Runtime)

t=H(CIH)kt = H \left( \frac{C}{I H} \right)^{k}
CIHtk
Where
  • tt= Runtime (h)
  • CC= Rated capacity (Ah)
  • II= Discharge current (A)
  • HH= Rating discharge time (h)
  • kk= Peukert exponent

A battery's amp-hour rating is a promise made at one particular discharge rate, and it does not survive being pushed harder. Wilhelm Peukert measured this in 1897: capacity falls off as a power law in current, t=H(C/IH)kt = H(C/IH)^k, where H is the number of hours the rating was measured over — usually 20 for lead-acid — and k is the exponent that describes how badly the chemistry copes. A 100 Ah battery at the 20-hour rate looks like it should run 4 hours at 25 A; with a typical k of 1.3 it manages under 2.5 hours.

The exponent is a health indicator as much as a design parameter. New flooded lead-acid sits around 1.1 to 1.2, AGM slightly better, a tired or sulphated bank 1.3 and worse. Lithium iron phosphate is near 1.02 to 1.05, which is a large part of why an LFP pack of the same nameplate capacity so comprehensively outperforms lead-acid in an inverter or a trolling motor — the rated capacity is nearly all real. You can measure your own k by timing two discharges at different currents and taking a ratio of logarithms, which is what solving this page for k does.

The classic error is comparing amp-hour ratings from different rate assumptions. A "100 Ah" battery at the 20-hour rate and a "100 Ah" battery at the 100-hour rate are not the same battery, and the second is markedly worse. Always check the rate the number was measured at. Two more caveats: Peukert's law says nothing about temperature, which can cost another 20% at freezing, and it assumes a steady current, so it systematically over-predicts for the pulsed loads that inverters and radios actually present.

Worked example: 100 Ah (20 h rate) at 25 A, k = 1.3 → 2.47 h

Motors, Transformers & Generators

Synchronous Speed from Frequency and Poles

Ns=2fpN_{s} = \frac{2f}{p}
pfNs
Where
  • NsN_{s}= Synchronous speed (rpm)
  • ff= Supply frequency (Hz)
  • pp= Number of poles

A pair of poles takes one full electrical cycle to sweep the field once around, so the field turns f/(p/2) = 2f/p revolutions per second. Multiply by 60 and you get the version every electrician knows: Ns = 120f/p in rpm. At 60 Hz that gives 3600, 1800, 1200 and 900 rpm for 2, 4, 6 and 8 poles; at 50 Hz, 3000, 1500, 1000 and 750. Enter f in hertz and read Ns in rpm and the two forms agree exactly.

Pole count is fixed by the winding, so before variable-frequency drives the only way to change a motor's speed was to change machines or use pole-changing windings. A VFD attacks the f instead, which is why a 4-pole motor on a 30 Hz drive turns near 900 rpm. Two traps: p counts poles, not pole pairs, and the actual shaft speed is always a percent or two below Ns because of slip — a true synchronous machine is a different animal with a DC-excited or permanent-magnet rotor.

Worked example: 60 Hz, 4 poles → 1800 rpm

Induction Motor Slip

s=100(NsNr)Nss = \frac{100 \, (N_{s} - N_{r})}{N_{s}}
NsNrs
Where
  • ss= Slip (%)
  • NsN_{s}= Synchronous speed (rpm)
  • NrN_{r}= Rotor speed (rpm)

An induction motor's rotor must lag the rotating field — if it ever caught up, the field would stop sweeping past the rotor bars, no voltage would be induced, and no torque would exist. That lag is slip. A 4-pole motor on 60 Hz has a synchronous speed of 1800 rpm; a nameplate reading of 1750 rpm means s = 100 × 50/1800 ≈ 2.8%, entirely typical for a healthy machine at full load.

Slip is a free load indicator: it is very nearly proportional to torque, so a tachometer reading tells you how hard the motor is working without a single meter lead. At no load slip falls under 1%; at breakdown torque it may hit 20%. Rising slip on a familiar machine means added mechanical load, low voltage, or a broken rotor bar. Note that this solver treats rpm as a frequency, so answers appear in hertz unless you pick rpm from the table.

Worked example: 1750 rpm against 1800 rpm → 2.78% slip

Motor Torque from Power and Speed

T=P2πNT = \frac{P}{2\pi N}
MNTP
Where
  • TT= Shaft torque (N·m)
  • PP= Shaft output power (W)
  • NN= Rotational speed (Hz)

Power is torque times rotational speed, so torque is power divided by speed. In SI that is T=P/2πNT = P/2\pi N with P in watts, N in revolutions per second and T in newton metres: 7.5 kW at 1500 rpm is 25 rev/s, so T=7500/(2π×25)47.7T = 7500/(2\pi \times 25) \approx 47.7 N·m. Nothing else is going on — every "torque formula" in the trade is this relation wearing different units.

The North American version is T=5252×HP/RPMT = 5252 \times HP/RPM with torque in pound-feet, and 5252 is not a physical constant but a unit conversion: one horsepower is 550 ft·lbf per second, and 550×60/2π=5252.1550 \times 60/2\pi = 5252.1. Pick horsepower and rpm from this solver's unit menus and the two forms agree to the last digit. A 10 hp motor at 1750 rpm develops 5252×10/1750305252 \times 10/1750 \approx 30 lb·ft.

The 5252 also explains the one fact that surprises everyone reading a dynamometer chart: the horsepower and torque curves always cross at 5252 rpm, on every engine ever built, because that is where the multiplier equals one. Below that speed torque exceeds power numerically, above it the reverse. The practical warning for motor work is that this gives torque at rated speed only. Starting torque, breakdown torque and torque at a stall are set by the machine's speed-torque curve, not by its nameplate power, and a motor driven by a VFD below its base speed holds torque while its power falls away.

Worked example: 7.5 kW at 1500 rpm → 47.75 N·m

Motor Efficiency

η=100PoutPin\eta = \frac{100 \, P_{out}}{P_{in}}
MηPinPout
Where
  • η\eta= Efficiency (%)
  • PoutP_{out}= Output power (W)
  • PinP_{in}= Input power (W)

The difference between input and output is heat: stator and rotor I²R losses, core losses, windage and friction. A 10 hp motor at 88% efficiency swallows 7457/0.88 ≈ 8474 W to deliver 7457 W of shaft power, dumping about a kilowatt into the room — which is why motor rooms need ventilation and why efficiency shows up twice in an energy audit, once as electricity and once as cooling load.

Efficiency is not constant: it peaks near 75–100% of rated load and falls off a cliff below about 40%, which is the strongest argument against habitually oversizing motors. Since the 1990s, minimum efficiencies have been legislated — IE3 "premium" class in the IEC world, EPAct and NEMA Premium in the US — and the gain from an IE1 to an IE3 machine, a few points, usually repays the price difference within a year of continuous running.

Worked example: 18.5 kW out of 20 kW in → 92.5%

Three-Phase Motor Full-Load Current

I=Pout3VPFηI = \frac{P_{out}}{\sqrt{3} \, V \, \text{PF} \, \eta}
MηVIPoutPF
Where
  • II= Full-load line current (A)
  • PoutP_{out}= Shaft output power (W)
  • VV= Line-to-line voltage (V)
  • PF\text{PF}= Power factor
  • η\eta= Efficiency (%)

A motor's rating is what comes out of the shaft; the line must supply that plus the losses, and it must supply it through a phase angle. So the input volt-amperes are Pout/(η · PF), and dividing by √3 V gives the line current. A 10 hp, 460 V motor at 89% efficiency and 0.85 PF draws 7457/(1.732 × 460 × 0.85 × 0.89) ≈ 12.4 A — reassuringly close to the 14 A that NEC Table 430.250 lists for sizing.

Use the code table, not this calculation, for conductor and overload sizing in North America: the NEC deliberately tabulates conservative currents and requires them for branch-circuit design, reserving nameplate amps for overload protection. Use this formula instead when you want to know what a specific machine really draws, to sanity-check a clamp-meter reading, or to see how an unloaded motor's collapsing power factor pushes current up out of proportion to the work being done.

Worked example: 10 hp, 460 V, 0.85 PF, 89% → 12.37 A

Motor Locked-Rotor Starting Current

ILR=1000kP3VI_{LR} = \frac{1000 \, k \, P}{\sqrt{3} \, V}
ILRItMVP
Where
  • ILRI_{LR}= Locked-rotor current (A)
  • kk= Locked-rotor kVA per horsepower (kVA/hp)
  • PP= Motor rating (hp)
  • VV= Line-to-line voltage (V)

At the instant of starting, an induction motor is a transformer with a shorted secondary. The rotor is not moving, no back-EMF opposes the supply, and the only thing limiting current is the winding impedance — so the motor pulls somewhere between five and eight times its full-load current until it accelerates. Manufacturers state this on the nameplate as a code letter, which stands for a range of locked-rotor kilovolt-amperes per horsepower. Look the letter's kVA/hp value up in your own code book, enter it here, and the arithmetic is straightforward: multiply by the horsepower to get locked-rotor kVA, then divide by √3 V to get amps. A 25 hp, 460 V motor at 6.3 kVA/hp draws about 198 A to start against roughly 30 A running.

What that inrush actually does is sag the voltage — momentarily, but sometimes visibly, and occasionally enough to drop out a contactor elsewhere on the panel or to stall the motor that caused it. The current is also strongly reactive at that instant, with a power factor down around 0.2, so it is nearly pure magnetizing current doing no work at all. This is the number that sizes soft starters, decides whether a wye-delta or autotransformer starter is worth the panel space, and, more than any running load, sizes a generator on a site with big motors.

Two cautions. The kVA/hp figure is a range per letter, and the code table gives a band, not a point — use the top of the band when the consequence of being wrong is a nuisance trip. And do not use this number for overload protection or conductor sizing: those follow the code's own tables and rules, which are built to let the inrush pass while still protecting the machine. Locked-rotor current tells you about the moment of starting; it says nothing about the hour that follows.

Worked example: 25 hp, 460 V, 6.3 kVA/hp → 197.7 A inrush

Transformer Voltage Ratio

VsVp=NsNp\frac{V_{s}}{V_{p}} = \frac{N_{s}}{N_{p}}
VpNpNsVs
Where
  • VpV_{p}= Primary voltage (V)
  • VsV_{s}= Secondary voltage (V)
  • NpN_{p}= Primary turns
  • NsN_{s}= Secondary turns

A transformer is two coils sharing one magnetic circuit, and the turns ratio follows from Faraday's law applied to each of them. The alternating current in the primary drives an alternating flux around the iron core; that same flux threads the secondary, because the core is there precisely to make sure it does. Each turn of wire, primary or secondary, has the identical ΔΦ/Δt\Delta\Phi/\Delta t passing through it, and therefore develops the identical volts per turn. Ten times the turns intercepting the same changing flux means ten times the induced voltage — hence Vs/Vp=Ns/NpV_s/V_p = N_s/N_p. Nothing about the wire gauge, the core size or the load enters into it.

A doorbell transformer stepping 120 V down to 16 V has a turns ratio of 7.5 to 1: a 900-turn primary against a 120-turn secondary. Because an ideal transformer neither creates nor destroys power, VpIp=VsIsV_p I_p = V_s I_s, and the current ratio inverts — that 16 V secondary supplying 1 A draws only 0.13 A from the 120 V side. Impedance transforms as the square of the turns ratio, Zp/Zs=(Np/Ns)2Z_p/Z_s = (N_p/N_s)^2, which is the whole reason for the output transformer in a valve amplifier and for matching transformers in radio work.

Michael Faraday wound the first one in 1831 on an iron ring, and the arrangement that carries the modern name was developed by Ottó Bláthy, Miksa Déri and Károly Zipernowsky in Budapest in 1885. It is the reason alternating current won the arguments of the 1890s: no comparably simple device changes DC voltage, and without cheap voltage changing you cannot transmit at high voltage and consume at low. A transformer works only on changing flux. Connect a steady DC supply and the induced secondary voltage is zero, while the primary — with only its winding resistance to limit current — draws whatever the supply will give and burns.

The trap that catches people in the field is that this equation is the ideal, and the ideal is a no-load figure. Measure the secondary of a transformer with nothing connected and you will get close to the turns ratio. Load it and the voltage sags, because the winding resistance and the leakage reactance drop voltage inside the transformer itself — a small unit may deliver 10% less than its nameplate at full load, which is exactly why nameplates quote a rated output at a rated current rather than a bare ratio. This is the transformer's version of a point worth stating plainly: an induced EMF is not the same thing as the terminal voltage you can measure once current flows, any more than a battery's EMF equals its terminal voltage under load. Two further cautions: the turns ratio says nothing about isolation or safety, since an autotransformer shares a winding and offers none; and stepping voltage down steps current up, so a secondary short is a far more violent event than the primary's fuse rating suggests.

Worked example: 120 V, 500:25 turns → 6 V secondary

Transformer Full-Load Current

IFL=SkVI_{FL} = \frac{S}{k \, V}
IFLVSk
Where
  • IFLI_{FL}= Full-load current (A)
  • SS= Transformer rating (VA) (W)
  • VV= Winding voltage (V)
  • kk= Phase factor

A transformer's nameplate gives kilovolt-amperes, and kVA is the honest rating: the windings care about amps, the core cares about volts, and neither knows anything about power factor. Turning kVA into amps is just division — by the voltage for a single-phase unit, and by √3 times the line-to-line voltage for a three-phase one. This page carries that choice as a single factor k: enter 1 for single-phase, 1.732 for three-phase. A 75 kVA three-phase transformer on a 208 V secondary is rated 75 000 / (1.732 × 208) ≈ 208 A, which is a pleasing coincidence and nothing more.

Do this on both sides. The same kVA at a higher voltage means proportionally fewer amps, which is the whole argument for distribution voltage: that 75 kVA unit fed at 600 V pulls only 72 A on the primary. Getting the sides mixed up — using the primary voltage with the secondary conductors — is the classic error, and it always errs in the dangerous direction on the low-voltage side. If you ever solve this page for k as a check and get something between 1 and 1.732, that is the diagnosis: your voltage, your current and your kVA are not all from the same winding.

Full-load current is where transformer protection and conductor sizing start, but it is only the start. Primary and secondary overcurrent protection follow the code's own percentage rules, which deliberately allow the device to sit well above this current so that magnetizing inrush does not trip it on every energization — and those percentages differ by voltage class, by whether secondary protection is provided, and by edition. Look them up. What this page gives you is the rated current the rest of that arithmetic hangs from.

Worked example: 240 V single-phase at 125 A → 30 kVA

Voltage Regulation

%VR=100(VnlVfl)Vfl\%VR = \frac{100 \, (V_{nl} - V_{fl})}{V_{fl}}
VnlVfl%VR
Where
  • %VR\%VR= Voltage regulation (%)
  • VnlV_{nl}= No-load voltage (V)
  • VflV_{fl}= Full-load voltage (V)

Regulation is the answer to "how much does the voltage sag when I actually use it?" — the gap between no-load and full-load terminal voltage, as a percentage of the full-load figure. A transformer reading 480 V unloaded and 460 V at rated load regulates at 100×20/4604.35%100 \times 20/460 \approx 4.35\%. Small is good: a stiff source barely notices the load, a soft one wanders.

Note the denominator, because it is the standard mistake. Regulation is referenced to the full-load voltage, not the no-load one, since full load is the condition the equipment must work in. Dividing by 480 instead of 460 gives 4.17%, and while the difference looks trivial here, it grows fast on a poorly regulated source and it will not match anyone else's numbers.

Different machines carry wildly different figures for good reasons. A distribution transformer might regulate at 2–4%; a welding transformer is designed for terrible regulation on purpose, because a drooping characteristic is what keeps arc current stable as the operator's hand wobbles. Regulation can also go negative — a generator or transformer feeding a leading power factor can deliver more volts under load than without it, which is why the sign, not just the size, matters on circuits with capacitor banks or a lot of inverter-based generation.

Worked example: 480 V no load, 460 V full load → 4.35%

Transformer Percent-Impedance Voltage Drop

Vd=%Z100SLSRVRV_{d} = \frac{\%Z}{100} \cdot \frac{S_{L}}{S_{R}} \cdot V_{R}
SL%ZSRVdVR
Where
  • VdV_{d}= Impedance voltage drop (V)
  • %Z\%Z= Percent impedance (%)
  • SLS_{L}= Actual load (kVA) (W)
  • SRS_{R}= Transformer rating (kVA) (W)
  • VRV_{R}= Rated secondary voltage (V)

The same percent impedance that sets fault current also sets the voltage a transformer loses inside itself. By definition, at full load the internal drop is exactly %Z of rated volts, and the drop scales with loading. So a 1000 kVA, 480 V transformer with 5.75% impedance loses 0.0575×480=27.60.0575 \times 480 = 27.6 V of its own winding at nameplate load, and 13.8 V at half load. That is why the secondary of a heavily loaded transformer sits low and the tap changer exists.

Treat this as an upper bound rather than a prediction, because it adds the resistive and reactive drops arithmetically when they are really at right angles to each other and to the load current. The true drop depends on power factor: at unity PF a mostly reactive impedance costs far less than this suggests, while at 0.8 lagging the resistive and reactive parts line up closer with the load and the answer here is close to right. The exact form is Vd=I(Rcosφ+Xsinφ)V_d = I(R\cos\varphi + X\sin\varphi).

The counter-intuitive part is that a leading power factor can make the drop go the other way — a lightly loaded feeder with capacitor banks still switched in can push the secondary above nominal, which is a real problem on rural circuits and on distribution feeders with a lot of solar. High impedance is not simply a defect either: utilities sometimes specify a higher %Z deliberately to hold fault current down to what the existing switchgear can interrupt, and accept the poorer regulation as the price.

Worked example: 1000 kVA, 480 V, 5.75% Z at full load → 27.6 V

Available Short-Circuit Current from Percent Impedance

ISC=100IFL%ZI_{SC} = \frac{100 \, I_{FL}}{\%Z}
ISCIFL%Z
Where
  • ISCI_{SC}= Available short-circuit current (A)
  • IFLI_{FL}= Full-load current (A)
  • %Z\%Z= Percent impedance (%)

Percent impedance is a strange-looking number until you know its definition: it is the percentage of rated voltage that must be applied to a transformer with its secondary shorted to drive exactly full-load current. Turn that around and it tells you the fault current straight away. If 5% of the volts pushes full-load amps through the short, then 100% of the volts pushes twenty times that. A 500 kVA, 480 V unit with 601 A full load and 5% impedance can deliver 601×2012,000601 \times 20 \approx 12{,}000 A into a bolted fault.

That number is not academic. It sets the interrupting rating of every breaker and fuse downstream, and equipment applied above its rating does not merely trip late — it can fail explosively, which is the scenario arc-flash studies exist to prevent. It is also why "buy the transformer with the lowest impedance" is bad advice: a lower %Z gives better voltage regulation and worse fault duty, and the sweet spot is a design decision, not a default.

The assumption hiding in this calculation is an infinite primary source, so it deliberately overestimates. Real utility supplies have their own impedance, and the cable between the transformer and the fault adds more, so the true available current at a panel forty metres away is lower — sometimes much lower. Overestimating is the safe direction for equipment ratings but the unsafe direction for coordination studies, where a fault current that turns out too small may fail to clear a fuse in time.

Worked example: 601.4 A FLA at 5% Z → 12 028 A available

Generator Sizing from Connected Load

Pg=PcDf(1+m)P_{g} = P_{c} \, D_{f} \left( 1 + m \right)
PcDfPgmG
Where
  • PgP_{g}= Generator rating needed (W)
  • PcP_{c}= Connected load (W)
  • DfD_{f}= Demand factor
  • mm= Spare capacity margin

Connected load is the sum of every nameplate on the site. Demand load is what actually runs at the same instant, and it is always less, because kitchens do not run every appliance at once and shops do not start every machine together. The ratio between the two is the demand factor. Multiply the connected load by it, add a margin for the loads nobody has thought of yet, and you have the continuous kilowatts a generator must deliver. Two hundred and fifty kilowatts connected, running two-thirds of it at once, with a quarter again for growth, wants a set good for about 203 kW.

The demand factors themselves are tabulated by occupancy and load type in the code, and they are not reproduced here — look up the ones that apply to your building. What this page can tell you is which way the errors go. A demand factor entered as 65 instead of 0.65 gives an answer a hundred times too large, which is at least obvious; a demand factor borrowed from the wrong occupancy is not obvious at all and shows up years later as a generator that never gets above quarter load, burning fuel to wet-stack itself.

Two things this arithmetic does not do. First, generators are rated in kW but limited in kVA — the alternator's copper carries amps regardless of phase angle — so divide this kW answer by the set's rated power factor (usually 0.8) to get the kVA the machine must be rated for. Second, on a motor-heavy site the running load is rarely what sizes the set: the starting inrush of the largest motor is, because the generator's voltage sags under it far harder than the utility's does. Size for the running load here, then check the starting case, and let whichever is larger win.

Worked example: 250 kW connected, 0.65 demand, 25 % spare → 203.1 kW

Electromagnetics Basics

Coulomb's Law

F=keq1q2r2F = \frac{k_e \, q_{1} q_{2}}{r^{2}}
q1q2rFF
Where
  • FF= Electrostatic force (N)
  • q1q_{1}= Charge 1 (C)
  • q2q_{2}= Charge 2 (C)
  • rr= Separation distance (m)

In 1785 Charles-Augustin de Coulomb hung a charged sphere on a fine torsion wire and measured how hard a second charge twisted it. The result is the electric twin of Newtonian gravity: the force between two point charges grows with the product of the charges and falls off with the square of the distance. Electricity is by far the stronger force: the electric repulsion between two protons is about 10³⁶ times their gravitational attraction — which is why a rubbed balloon can lift paper against the pull of the entire Earth.

Worked example: two 1 µC charges held 10 cm apart feel F = kₑ × (10⁻⁶)² / (0.1)² ≈ 0.9 N — roughly the weight of an apple, from specks of charge. Enter charge magnitudes here; the sign of the product only tells you whether the pair attracts (opposite signs) or repels (like signs).

Worked example: Two 1 uC charges 1 m apart → 8.98755 mN

Magnetic Force on a Moving Charge

F=qvBsinθF = q v B \sin\theta
qvFB
Where
  • FF= Magnetic force (N)
  • qq= Charge (C)
  • vv= Speed (m/s)
  • BB= Magnetic flux density (T)
  • θ\theta= Angle between v and B (°)

Magnetic fields are choosy: they push only on charges that move, and only on the component of motion that cuts across the field lines. The force is greatest when velocity and field are perpendicular (θ = 90°), and vanishes entirely for a charge coasting along the field. Because the push is always sideways — perpendicular to both v and B — it does no work; it bends paths into circles and spirals instead of speeding particles up. That steering is the working principle of particle accelerators, mass spectrometers, and the aurora, where solar particles spiral down Earth's field lines to the poles.

Worked example: a proton (q = 1.602×10⁻¹⁹ C) crossing a 0.5 T field at 10⁶ m/s and 90° feels F = 8×10⁻¹⁴ N — tiny, yet enough to whirl it in a tight circle. Note that θ itself is not solvable here: arcsin cannot tell θ from 180° − θ, so the inversion is ambiguous.

Worked example: 40 dyn on 2 uC at 1800 km/h, 30 deg → 0.8 T

Magnetic Force on a Current-Carrying Wire

F=BILsinθF = B I L \sin\theta
IFBL
Where
  • FF= Magnetic force (N)
  • BB= Magnetic flux density (T)
  • II= Current (A)
  • LL= Wire length in field (m)
  • θ\theta= Angle between wire and B (°)

This is the force on one moving charge, F=qvBsinθF = qvB\sin\theta, added up over all the charges in a length of wire. A current II means charge crossing at II coulombs per second, so a length LL of conductor holds a quantity of moving charge whose product with its drift speed is exactly ILIL — the individually feeble pushes on perhaps 102210^{22} slowly drifting electrons, collected by the metal lattice and delivered to the wire as a whole. That is why F=BILsinθF = BIL\sin\theta contains no reference to how many carriers there are or how fast they move: those two factors always multiply out to the current. The sine handles orientation, peaking when the wire lies across the field and vanishing when it lies along it, since a charge coasting parallel to a field feels nothing.

A 0.25 m length of wire carrying 8 A across a 0.4 T field at right angles feels F=0.4×8×0.25=0.8 NF = 0.4 \times 8 \times 0.25 = 0.8\ \text{N} — about the weight of a coffee mug, from a single conductor. Multiply by a few hundred turns in an armature and you have the torque of a real motor. Tilt the same wire to 30° from the field and the force drops to 0.8sin30°=0.4 N0.8 \sin 30° = 0.4\ \text{N}, half. The direction is perpendicular to both the wire and the field, given by the right-hand rule, and this sideways push is what motor designers arrange to be a torque.

Faraday demonstrated the effect in 1821 with a wire free to rotate around a magnet dipped in mercury — the first electric motor, built to settle an argument about whether electromagnetism could produce continuous motion. Every motor and every loudspeaker since is the same experiment industrialised, the cone driven by a coil of wire hanging in a permanent magnet's gap with the audio signal as II. Note that this relation and the motional-EMF page are two faces of one thing: push current through a wire in a field and it moves, move a wire in a field and current appears, and a motor and a generator are the same machine run in opposite directions.

Three cautions. The angle θ\theta is measured between the wire and the field, and it cannot be solved for on this page — arcsine cannot tell θ\theta from its supplement 180°θ180° - \theta, so the calculator returns FF, BB, II or LL but never the angle. LL is the length of conductor actually inside the field, not the length of the wire; a metre of lead-in outside the magnet gap contributes nothing. And a note on the right-hand rule: it works with conventional current, drawn flowing from positive to negative, while the electrons in the copper are travelling the other way. Benjamin Franklin fixed that sign a century before the electron was found, and he fixed it backwards. Both descriptions give the same force in the same direction — negative charge moving left is the same current as positive charge moving right — but if you switch to reasoning about electrons you must switch hands too, and mixing the two is the surest way to get a motor turning the wrong way on paper.

Worked example: 10 A in 2 m of wire across 0.5 T → 10 N

Force Between Parallel Wires

F=μ0I1I22πdF = \frac{\mu_0 I_1 I_2 \ell}{2\pi d}
I₁I₂dFF
Where
  • FF= Force (N)
  • I1I_1= Current 1 (A)
  • I2I_2= Current 2 (A)
  • \ell= Wire length (m)
  • dd= Separation (m)

This equation is two earlier ones stacked. A long straight wire produces a field circling it at B=μ0I1/(2πd)B = \mu_0 I_1/(2\pi d) at distance dd; a second wire sitting in that field feels F=BI2F = B I_2 \ell. Substitute and you get F=μ0I1I2/(2πd)F = \mu_0 I_1 I_2 \ell/(2\pi d). Each wire sits in the other's field, and by Newton's third law they push on each other equally and oppositely. The direction is the part people find surprising: currents flowing the same way attract, currents flowing opposite ways repel — the reverse of the intuition borrowed from electrostatics, where like charges repel. Note the 1/d1/d rather than 1/d21/d^2: a straight wire's field falls off with the first power of distance because the source is a line rather than a point.

Two wires 10 mm apart, each carrying 10 A, over a 1 m parallel run feel F=(1.257×106×10×10×1)/(2π×0.01)=2.0 mNF = (1.257 \times 10^{-6} \times 10 \times 10 \times 1)/(2\pi \times 0.01) = 2.0\ \text{mN} — the weight of a grain of rice, which is why nobody notices it in ordinary wiring. Now put a 20 kA fault through the same pair: the currents appear as a product, so the force scales with the square, and 2 mN becomes 8 kN per metre. That is nearly a tonne of force trying to tear a metre of busbar out of its supports, and it is the reason switchgear bracing is engineered rather than assumed.

From 1948 until 2019 this relation did not merely describe the ampere, it defined it: the ampere was the current which, in two infinitely long parallel conductors one metre apart in vacuum, produced a force of exactly 2×1072 \times 10^{-7} newtons per metre. That definition is what made μ0\mu_0 exactly 4π×1074\pi \times 10^{-7} — a defined constant rather than a measured one. The 2019 redefinition of the SI moved the anchor to a fixed value of the elementary charge, and one consequence is that μ0\mu_0 is now an experimentally determined quantity with an uncertainty, very slightly different from 4π×1074\pi \times 10^{-7}. This page uses the CODATA value.

The traps are dimensional and geometric. The published version of this law is usually the force per unit length; this page multiplies by \ell to give a total force, so do not apply a per-metre figure and then multiply by the length again. dd is the centre-to-centre separation, not the gap between insulation surfaces, and on closely spaced busbars the difference is not small. The result assumes long, straight, parallel conductors — near a bend, a termination or a right-angle crossing the geometry changes and the simple form does not hold. And because the currents enter as a product, an alternating current gives a force that is always attractive or always repulsive but pulses at twice the supply frequency, never reversing: that 120 Hz throb on a 60 Hz system is precisely what makes transformers and reactors hum, and what fatigues busbar supports over years rather than breaking them in an instant.

Worked example: 10 A twin wires, 1 m run, 1 cm apart → F = 2 mN

Magnetic Field of a Solenoid

B=μ0NILB = \frac{\mu_0 N I}{L}
INBL
Where
  • BB= Magnetic field (T)
  • NN= Number of turns
  • II= Current (A)
  • LL= Solenoid length (m)

A single loop of wire makes a field that is strong at its centre and sprawls untidily everywhere else. Wind many loops into a tight helix and something better happens: inside the coil every turn's field points the same way and they add, while outside they point in opposing directions and largely cancel. What is left is a nearly uniform field along the axis, and Ampère's law applied to a rectangular path straddling the wall of a long solenoid gives it as B=μ0NI/LB = \mu_0 N I / L. The striking thing about that result is what is missing — the diameter of the coil does not appear. Only the current and the turns per unit length matter, so a broomstick-sized coil and a pencil-sized one with the same winding density and current produce the same interior field.

A 200 mm coil wound with 1000 turns and carrying 5 A gives B=(1.257×106×1000×5)/0.2=31 mTB = (1.257 \times 10^{-6} \times 1000 \times 5)/0.2 = 31\ \text{mT}, roughly six hundred times Earth's field of about 50 µT. Halving the current to 2.5 A halves the field; stretching the same 1000 turns over 400 mm also halves it, because the turns are now half as dense. That second sensitivity is the one people forget, and it is why the equation is better read as B=μ0nIB = \mu_0 n I with nn the turns per metre.

André-Marie Ampère coined the word solénoïde in the 1820s from the Greek for a channel or pipe, and the coil is still the standard way to make a field you can switch. Relays, contactors, solenoid valves, MRI bores and every particle-physics magnet are variations of it. Wrapping the coil around soft iron multiplies the result by the material's relative permeability — a factor of several thousand for good silicon steel — which is how a modest coil can lift a car, and the equation then reads B=μrμ0nIB = \mu_r \mu_0 n I. Superconducting magnets take the other route and simply run enormous current, since with zero resistance there is no I2RI^2R heat to remove.

The formula is an idealisation for a long coil, and it fails where the coil ends. Field lines have to turn around and come back, so at the mouth of a solenoid the axial field falls to about half its interior value, and outside it is weaker still and spread out. Treating a short, fat coil — anything much wider than it is long — with this equation will overstate the field substantially; that geometry needs the exact axial expression or a numerical model. The second failure is saturation. The iron-core multiplication is not a licence to keep raising current: ordinary steels saturate somewhere around 1.5 to 2 T, after which μr\mu_r collapses toward 1 and every further ampere buys only the modest air-core contribution. Third, watch the length variable: LL is the length of the winding, not the length of the wire, and confusing them can be a factor of a thousand. And a coil is an inductor: switching that 31 mT off in a millisecond will produce a voltage spike large enough to arc a contact, which is why a solenoid valve gets a flyback diode.

Worked example: 1000 turns, 5 A, 20 cm → B = 31.4159 mT

Magnetic Flux (Φ = BA cos θ)

Φ=BAcosθ\Phi = B A \cos\theta
θBΦA
Where
  • Φ\Phi= Magnetic flux (Wb)
  • BB= Magnetic field (T)
  • AA= Loop area ()
  • θ\theta= Tilt angle (°)

Flux is the amount of magnetic field passing through a surface — in Faraday's own picture, the number of field lines that thread the loop. Two things control it. The first is how much surface there is and how strong the field is, which gives the product BABA. The second is orientation, and that is where the cosine comes in: only the component of the field perpendicular to the surface gets through. Hold the loop face-on to the field and it catches everything; tilt it edge-on and the lines slide past without crossing it at all. Written out, Φ=BAcosθ\Phi = BA\cos\theta, with the flux in webers when BB is in tesla and AA in square metres.

A 0.4 T field through a rectangular loop 150 mm by 200 mm — an area of 0.030 m² — held face-on threads 0.4×0.030=12 mWb0.4 \times 0.030 = 12\ \text{mWb}. Tilt that loop by 60° and it drops to 12cos60°=6 mWb12 \cos 60° = 6\ \text{mWb}. Spin it steadily and the flux traces out a cosine in time, which is precisely how a generator makes a sine-wave voltage: not by varying BB and not by varying AA, but by rotating θ\theta through 360° every revolution.

Flux exists as a named quantity for one reason, which is that its rate of change is what induces voltage. Faraday's law, on the next page of this shard, is ε=NΔΦ/Δt\varepsilon = N\,\Delta\Phi/\Delta t, and every generator, transformer, induction motor, metal detector and transformer-coupled sensor on Earth is a machine built to make BAcosθBA\cos\theta change. It is also the quantity in Gauss's law for magnetism: the net flux through any closed surface is exactly zero, because magnetic field lines have no beginning and no end, which is a compact way of saying nobody has ever found a magnetic monopole.

The angle is where nearly everyone goes wrong, and the cost is a swapped sine and cosine. θ\theta is measured from the normal to the loop — the line sticking out perpendicular to its face — and not from the plane of the loop itself. A loop lying flat in a vertical field has θ=0\theta = 0 and maximum flux, even though the field lies at 90° to the plane. If a textbook or a diagram gives you the angle to the plane, you must take its complement before entering it here. Second, keep flux and flux density apart: BB is a density in tesla, which is webers per square metre, while Φ\Phi is the total in webers — they are different quantities with different units and the words are used loosely almost everywhere. Third, flux by itself induces nothing. A loop sitting motionless in the strongest field you can buy has enormous flux through it and not one volt across it; only the change matters. And for a coil of NN turns, what the induction law uses is the flux linkage NΦN\Phi, not the Φ\Phi this page returns for a single loop.

Worked example: 0.5 T through 0.01 m^2 face-on → 5 mWb

Faraday's Law of Induction

ε=NΔΦΔt\varepsilon = N \frac{\Delta\Phi}{\Delta t}
εΔΦΔtN
Where
  • ε\varepsilon= Induced EMF (V)
  • NN= Number of turns
  • ΔΦ\Delta\Phi= Flux change (Wb)
  • Δt\Delta t= Time interval (s)

Faraday's 1831 discovery is the bridge between mechanics and electricity: change the flux through a coil and a voltage appears, one volt per weber-per-second per turn. The N multiplies because each turn is a voltage source in series — the reason transformers and generators are wound with hundreds of turns. Sweep a magnet that changes flux by 2 mWb through a 500-turn coil in 0.1 s and you induce 10 V.

The full law carries a minus sign (Lenz's law): the induced current always opposes the change that created it — nature's built-in inertia against flux change, and the origin of eddy-current braking.

Worked example: 500 turns, 2 mWb in 0.1 s → emf = 10 V

Motional EMF (ε = BLv)

ε=BLv\varepsilon = B L v
vεBL
Where
  • ε\varepsilon= Motional EMF (V)
  • BB= Magnetic field (T)
  • LL= Conductor length (m)
  • vv= Speed (m/s)

Drag a conductor sideways through a magnetic field and every free electron inside it is now a moving charge in a field, so every one of them feels the qvBqvB force. That force points along the wire, so the electrons pile up at one end and leave a deficit at the other, and they keep piling up until the electric field they have built pushes back exactly as hard as the magnetic force pushes. At that balance the wire has a voltage across it: ε=BLv\varepsilon = BLv. You have made a battery out of motion. The same result falls out of Faraday's law without mentioning a single electron — a wire of length LL moving at speed vv sweeps out area at LvLv per second, so it sweeps flux at BLvBLv per second — and the fact that the two arguments agree is not a coincidence but one of the observations that led Einstein to special relativity.

An airliner with a 60 m wingspan crossing the vertical component of Earth's field, about 50 µT at mid-latitudes, at 250 m/s develops 50×106×60×250=0.75 V50 \times 10^{-6} \times 60 \times 250 = 0.75\ \text{V} from wingtip to wingtip. A more workmanlike case: a 0.3 m rod sliding along rails at 4 m/s through a 0.6 T field gives 0.6×0.3×4=0.72 V0.6 \times 0.3 \times 4 = 0.72\ \text{V}. Close the rails through a 2 Ω load and 0.36 A flows, delivering 0.26 W — and that power has to come from somewhere.

Where it comes from is your arm. The moment current flows in the moving rod, the rod is a current-carrying conductor in a magnetic field, so it feels F=BILF = BIL — and Lenz's law guarantees that force opposes the motion. Push the rod at constant speed and the mechanical power you supply, FvFv, equals the electrical power delivered, to the joule. That is the entire energy accounting of every generator ever built: a turbine does not spin harder when the grid load rises, it spins against more force, and the fuel bill reflects it. This page and the magnetic-force-on-a-wire page describe one machine running in its two directions.

Some cautions, starting with the name. Electromotive force is not a force. It is measured in volts and it is energy per unit charge, and the nineteenth-century name has confused students for a hundred and fifty years — read "EMF" as "the voltage a source generates internally" and it will not mislead you. Nor is that internal voltage the same as the voltage you would measure at the terminals: once current flows, the source's own resistance drops part of it, which is the same reason a car battery reads 12.6 V at rest and 10 V while cranking. Next, BB here must be the field component perpendicular to the plane the wire sweeps through; using the total field of a tilted magnet overstates the answer. And the aircraft case is a good lesson in what an EMF is worth without a circuit: the 0.75 V exists, but the whole aeroplane moves together, so there is no closed loop through stationary conductors and nothing useful can be drawn from it.

Worked example: 0.5 T, 2 m rod at 10 m/s → emf = 10 V

Practice problems

Answer key at the back. Work in the units each problem states.

DC Circuit Foundations

1. Ohm's LawA 40 Ω resistor is connected straight across a 200 V bench supply. Determine the current the resistor draws.

2. Ohm's LawA shunt element on a DC test rig drops 250 V while carrying 5 A. Determine the resistance of the element.

3. Charge in motionA plating cell is run at a steady 8 A for 210 s. Calculate the charge passed through the cell.

4. Charge in motionA lithium cell for a portable instrument is rated 2000 mA·h. Delivered in full, that rating is a quantity of charge. Determine the charge the cell can deliver, in coulombs.

5. Power, three waysA DC drive on a conveyor is measured at 120 V across its terminals while it draws 2 A. No resistance is quoted anywhere on the sheet. Calculate the power the drive is taking from the supply.

6. Power, three waysA 20 Ω braking resistor carries 2 A during a stop. Nobody has metered the voltage across it. Calculate the power the resistor turns into heat.

7. Series and parallelOn a breadboard, a 15 Ω resistor and a 60 Ω resistor are wired end to end, so the same current must pass through both in turn. Calculate the resistance the pair presents between the outer ends.

8. Series and parallelOn the same breadboard, a 40 Ω resistor and a 60 Ω resistor are wired side by side between one pair of nodes, so the current arriving has two paths open to it. Calculate the resistance the pair presents between those two nodes.

9. DividersA sensor input is fed from a 15 V rail through a two-resistor chain: 10 kΩ from the rail down to the tap, then 5 kΩ from the tap down to ground. The input itself draws no appreciable current. Calculate the voltage at the tap, measured to ground.

10. DividersA 6 A supply current arrives at a node and splits between two parallel branches: branch 1 is 4 Ω, branch 2 is 2 Ω. Determine the current flowing in branch 1.

11. The real wireA 300 m run of copper cable has a conductor cross-section of 4 mm². Copper's resistivity is 1.68 × 10⁻⁸ Ω·m at working temperature. Calculate the DC resistance of that one conductor.

12. The real wireA copper field winding measures 25 Ω cold, on the bench at 20 °C. In service it settles at 55 °C. Copper's temperature coefficient is α = 0.00393 per K, referred to 20 °C. Determine the winding's resistance at its working temperature.

13. The Breadboard FinalLast board of the lab. A 20 V bench supply feeds a 2 Ω resistor, and beyond it a 6 Ω and a 3 Ω resistor sit side by side across the remaining pair of nodes. The 2 Ω part in your hand is marked 100 W. Work each line — every answer feeds the next. Determine whether the 2 Ω resistor's wattage rating is adequate, one line at a time.

14. The Breadboard FinalBonus mark, before the bench is cleared: the supply's own 4 Ω dropping resistor is carrying 5 A. Determine the power that resistor is dissipating.

Kirchhoff & the Network Theorems

15. The loop ruleA single loop on the bench: one supply feeding three elements in series. The meter reads 7 V across the first element, 8 V across the second and 9 V across the third. Determine the source voltage driving the loop.

16. The loop ruleA single loop on the bench: one supply feeding three elements in series. The meter reads 15 V across the first element, 20 V across the second and 25 V across the third. Determine the source voltage driving the loop.

17. The node ruleA distribution block in a panel is fed by one incoming conductor and split into three outgoing circuits. A clamp meter on the three outgoing legs reads 7 A, 10 A and 13 A. Determine the current in the incoming conductor.

18. The node ruleA junction box takes 12 A on its feed and splits it three ways. Two of the outgoing legs clamp at 3 A and 4 A. The third runs into a wall and cannot be clamped. Determine the current in the third leg.

19. Two laws togetherThe same 20 V divider is being checked at the bench. The technician's probe reaches the tap and reads 5 V there, but the upper resistor's body is under a heatsink and cannot be probed across. Determine the drop across the upper resistor.

20. Two laws togetherThe same 24 V divider is being checked at the bench. The technician's probe reaches the tap and reads 6 V there, but the upper resistor's body is under a heatsink and cannot be probed across. Determine the drop across the upper resistor.

21. Thevenin from two readingsA different module from the same batch is already characterised: 12 V open circuit, with 10 Ω of internal resistance. A 30 Ω load is about to be clipped across its terminals. Determine what the meter will read at the terminals once that load is connected.

22. Thevenin from two readingsA different module from the same batch is already characterised: 15 V open circuit, with 10 Ω of internal resistance. A 40 Ω load is about to be clipped across its terminals. Determine what the meter will read at the terminals once that load is connected.

23. Norton and the matched loadA bench source has been reduced to its Thevenin equivalent: 24 V behind 8 Ω. The lab wants the same source written the other way round, as a current source with the resistance in parallel. Determine the Norton current of the equivalent.

24. Norton and the matched loadA transducer's output stage is modelled as 12 V behind 2 Ω. The design team wants to know the very best a load could ever do on this output, before they choose one. Determine the greatest power any load can draw from this source.

25. Delta to wye and backA resistance bridge refuses to reduce: no two resistors in it are cleanly in series or in parallel. One triangle of the network runs 6 Ω between nodes A and B, 12 Ω between B and C, and 18 Ω between C and A. The plan is to redraw that triangle as a star. Determine the star arm that meets node A.

26. Delta to wye and backA three-terminal network is drawn as a star: 4 Ω from node A to the centre, 8 Ω from node B, and 16 Ω from node C. To merge it with a delta-connected bank next to it, the star has to be redrawn as a triangle. Determine the triangle leg that spans nodes A and B.

27. Design the dropA status LED is to run from a 5 V rail. Its datasheet gives a forward voltage of 1.8 V at the design current of 20 mA, and the LED will be fed through a single series resistor. Determine the series resistance the design calls for, then choose the part to fit.

28. Design the dropAn indicator LED is to run from a 24 V rail. Its datasheet gives a forward voltage of 2 V at the design current of 20 mA, and the LED will be fed through a single series resistor. Determine the series resistance the design calls for, then choose the part to fit.

29. The Black Box FinalLast box of the day. A sealed module comes back from the field with no data on it. Two readings go in the log: 12 V across its terminals with nothing connected, and 8 V with a 10 Ω test load clipped on. The bench has a matched load resistor rated 25 W, and the question is whether it can be left running. (No calculator — the numbers are chosen to fit in your head.) Work each line; every answer feeds the next. Determine whether that resistor is safe as the matched load, one line at a time.

30. The Black Box FinalBonus mark, on the way out: the same module measures 20 Ω of Thevenin resistance, and the drawer holds resistors of every value. A junior asks which one to clip on for the most power in the load. Determine the load resistance that draws the most power.

Storage & AC Impedance

31. CapacitanceA 10 µF snubber capacitor is found holding 1 mC of charge after the drive is de-energised. Determine the voltage still standing across its terminals.

32. CapacitanceA 220 µF capacitor bank is charged to 100 V and then isolated for a hipot check. Calculate the energy stored in the bank.

33. Capacitor combinationsTwo capacitors, 80 µF and 20 µF, are wired in SERIES across a control-panel bus. Calculate the total capacitance the bus sees.

34. Capacitor combinationsTwo capacitors, 6 µF and 12 µF, are wired in PARALLEL across the same DC link. Calculate the total capacitance across the link.

35. RC transientsA 100 µF capacitor is bled to ground through a 22 kΩ discharge resistor when the cabinet door opens. Calculate the time constant of that discharge path.

36. RC transientsA safety standard requires a 200 µF DC-link capacitor to reach a safe voltage on a 3 s time constant. Determine the bleed resistance that gives that time constant.

37. InductorsA contactor coil of 400 mH sits in a circuit whose total resistance is 200 Ω. Calculate the time constant of the coil circuit.

38. InductorsA relay circuit of 50 Ω is measured to settle on a 5 ms time constant. Determine the inductance of the relay coil.

39. RMS and peakA true-RMS meter across a 208 V branch circuit reads 208 V with the load running. Determine the peak voltage of that sine wave.

40. RMS and peakAn oscilloscope on a supply feeder shows a clean sine cresting at 170 V above zero. Determine the RMS voltage a panel meter would report on that same feeder.

41. ReactanceA 250 mH line reactor is fed from a 60 Hz supply. Calculate the inductive reactance the reactor presents at that frequency.

42. ReactanceA 10 µF power-factor capacitor is connected to a 50 Hz supply. Calculate the capacitive reactance it presents at that frequency.

43. ImpedanceA single-phase load is measured as 30 Ω of resistance in series with 40 Ω of reactance. Calculate the impedance magnitude of the load.

44. ImpedanceA coil measures 45 Ω on a DC resistance bridge, and its impedance at line frequency is 75 Ω. Determine the reactance of the coil at that frequency.

45. ResonanceA tuned trap for a harmonic filter is built from a 250 mH coil and a 100 nF capacitor in series. Calculate the frequency at which that trap resonates.

46. ResonanceA trap must resonate at 2000 Hz, and the only capacitor in the stores is 100 nF. Determine the inductance the coil must have.

47. Filters and decibelsA first-order low-pass filter on a sensor input uses a 10 kΩ resistor feeding a 1 nF capacitor to ground. Calculate the −3 dB corner frequency of that filter.

48. Filters and decibelsA line filter puts a 50 mH choke in series with a 100 Ω load. Calculate the −3 dB corner frequency of that filter.

49. The Resonance BenchLast bench of the term. A tuned tank is built from a 4 mH coil and a 10 µF capacitor, and the sheet gives its loaded quality factor as 4. The channel it must sit in is specified at no more than 400 Hz wide. No calculator: today take 1/(2π) as 0.16, so 2π is 6.25, and every line lands whole. Work each line — every answer feeds the next. Determine whether this tank fits inside the specified channel, one line at a time.

50. The Resonance BenchBonus mark, on the way out: a second tank centres on 160 Hz, and the specification calls for a passband exactly 20 Hz wide. Determine the quality factor that tank must have.

AC Power & the Bill

51. Power factorA wattmeter on a single-phase compressor reads 9972 W. The panel meters beside it show 277 V and 45 A. Determine the power factor of the compressor.

52. Power factorA wattmeter on a single-phase compressor reads 2496 W. The panel meters beside it show 208 V and 15 A. Determine the power factor of the compressor.

53. The power triangleA plant's monthly bill quotes an average power factor of 0.95 lagging. Determine the phase angle between the supply voltage and the current.

54. The power triangleA plant feeder is supplying 39 kVA to a bank of motors, and the wattmeter on the same feeder reads 36 kW. Calculate the reactive power the feeder is carrying.

55. Three-phase powerA three-phase panel on a 480 V system is measured at 40 A per line. Determine the apparent power the panel is drawing.

56. Three-phase powerA 75 kW three-phase load runs from a 600 V system at a power factor of 0.85. Determine the current in each line conductor.

57. Wye and delta systemsA delta-connected heater bank is built from three elements, and a clamp meter around one element inside the delta reads 60 A. Determine the current in each line conductor feeding the bank.

58. Wye and delta systemsA delta-connected heater bank is built from three elements, and a clamp meter around one element inside the delta reads 15 A. Determine the current in each line conductor feeding the bank.

59. Power-factor correctionA plant draws 150 kW at a power factor of 0.75 lagging. The utility's tariff penalises anything below 0.9, so the plant engineer proposes a capacitor bank. Calculate the capacitor rating needed to lift the power factor to 0.9.

60. Power-factor correctionA 13.3 kvar capacitor bank was installed on one feeder, and it moved that feeder's power factor from 0.8 to 0.9 exactly. Determine the real power the feeder is carrying.

61. The meterA 25 kW compressor runs for 100 hours in a month, on a tariff of $0.10 per kilowatt-hour. Determine what that compressor adds to the month's electricity bill.

62. The meterA 25 kW circulating pump runs continuously for 100 hours in a billing period. Calculate the energy the pump consumes over that period.

63. Feeders and voltage dropA single-phase load draws 25 A down a 60 m run of 6 mm² copper. Take the resistivity of copper as 0.0172 Ω·mm²/m. Calculate the voltage lost in the run.

64. Feeders and voltage dropA balanced three-phase feeder carries 25 A per line down a 100 m run of 10 mm² copper. Take the resistivity of copper as 0.0172 Ω·mm²/m. Calculate the line-to-line voltage lost in the run.

65. Battery runtimeA 200 Ah battery bank is to supply a steady 80 A. Treat the pack as ideal for this first estimate — the amp-hour figure taken at face value. Calculate the runtime the nameplate promises.

66. Battery runtimeA 100 Ah lead-acid bank is rated at the 20-hour discharge rate and has a Peukert exponent of 1.2. It is asked to hold a steady 20 A. Determine the runtime the pack will actually deliver.

67. The Utility AuditThe plant's main motor feeder is metered at 400 V, 125 A per line, power factor 0.80 lagging. The motor runs 200 hours in the billing month, energy is charged at 10 ¢/kWh, and the utility's demand tariff rewards a unity power factor. Today √3 = 1.73. Determine the capacitor bank, in kvar, that would take this feeder to unity — working from the metered load to the invoice on the way.

68. The Utility AuditBonus mark, on the way out: maintenance leaves a 15 kW process heater running for 50 hours of the same month, on the same 10 ¢/kWh tariff. Determine what that heater adds to the bill.

Motors, Transformers & Generators

69. Synchronous speed and slipA 4-pole motor on a 50 Hz supply drives a conveyor. A stroboscope on the shaft reads 1470 rpm at full load. Determine the percent slip at that load.

70. Synchronous speed and slipA nameplate on a 60 Hz machine gives its synchronous speed as 900 rpm. The winding data plate has gone missing. Determine how many poles the stator is wound for.

71. Torque from powerA torque transducer on a test bed reads 79.6 N·m while the shaft holds a steady 900 rpm. Determine the mechanical power the shaft is transmitting.

72. Torque from powerA 7.5 kW motor drives a centrifugal pump through a rigid coupling. Its nameplate speed at that output is 900 rpm. Calculate the torque the shaft delivers at rated output.

73. Motor efficiencyA test cell runs a motor at rated load. A power analyser on the supply reads 20 kW going in, and a dynamometer measures 17 kW coming off the shaft. Determine the motor's efficiency.

74. Motor efficiencyA ventilation fan's motor is metered at 50 kW input while running. Its nameplate quotes an efficiency of 85%. Calculate the mechanical power reaching the fan shaft.

75. Nameplate currentsA 11 kW three-phase motor is fed at 400 V. Its nameplate gives a power factor of 0.85, an efficiency of 88%, and a locked-rotor current 6 times full load. Determine the motor's full-load current, then the inrush it draws at the instant of an across-the-line start.

76. Nameplate currentsA 15 kW three-phase motor is fed at 400 V. Its nameplate gives a power factor of 0.9, an efficiency of 88%, and a locked-rotor current 6.5 times full load. Determine the motor's full-load current, then the inrush it draws at the instant of an across-the-line start.

77. TransformersA dry-type transformer is wound with 500 turns on the primary and 100 turns on the secondary. The primary is energised at 600 V. Calculate the secondary voltage at no load.

78. TransformersA rewind shop must produce 300 V from a 600 V supply. The primary coil is already wound with 300 turns. Determine how many turns the secondary needs.

79. Sag and faultA technician meters a transformer secondary twice: 420 V with the load switched off, and 400 V with the plant running at rated load. Determine the transformer's percent voltage regulation.

80. Sag and faultA 500 kVA transformer with a nameplate impedance of 5% supplies a rated secondary of 600 V. The connected load sits at 375 kVA. Calculate the volts lost inside the transformer's own windings at that loading.

81. Generator sizingA water-treatment plant schedules 500 kW of connected load onto its standby system. The consultant's demand factor for that schedule is 0.6, and the client wants 10% spare capacity for growth. Calculate the continuous rating the standby set must have.

82. Generator sizingA clamp meter on the main feeder of a pump house reads 150 A per line at 400 V, with the plant's power factor logged at 0.9. Determine the real power the pump house is drawing.

83. The Machine Room FinalLast machine of the commissioning day. A 6-pole induction motor runs on a 50 Hz supply at 400 V, three phase. A strobe reads 960 rpm at full load, a dynamometer measures 81 kW at the shaft, and the nameplate gives η = 90% and PF = 0.866. Work each line — every answer feeds the next. Read the motor end to end: field speed, slip, input power, line current.

84. The Machine Room FinalBonus mark, on the way out: the same starter panel holds a motor drawing 60 A at full load, and its nameplate quotes a locked-rotor current 6 times that. Determine the inrush the starter contacts see at the instant of an across-the-line start.

Electromagnetics Basics

85. Coulomb's LawTwo conducting spheres on an electrostatics test jig hold 10 µC and 4 µC, their centres 0.2 m apart. (kₑ = 9.00 × 10⁹ N·m²/C²) Calculate the electrostatic force between the spheres.

86. Coulomb's LawIn a powder-coating booth, a charged particle carrying 10 µC drifts 0.2 m from a grounded electrode holding 4 µC. (kₑ = 9.00 × 10⁹ N·m²/C²) Determine the electrostatic force acting between the two charges.

87. A charge in a magnetic fieldA charge of 80 µC crosses a magnet's gap at 250 m/s, square across the field lines, and a force of 8 mN is measured on it. Determine the flux density of the field in the gap.

88. A charge in a magnetic fieldA charge of 75 µC crosses a magnet's gap at 400 m/s, square across the field lines, and a force of 15 mN is measured on it. Determine the flux density of the field in the gap.

89. Wires and forcesA 0.5 m length of armature conductor sits in the 0.25 T gap of a machine's field magnet, lying square across the field, carrying 16 A. Calculate the force the field exerts on that length of conductor.

90. Wires and forcesTwo busbars in a switchboard run parallel for 5 m, 0.25 m apart, carrying 200 A and 200 A in the same direction. (µ₀ = 4π × 10⁻⁷ T·m/A) Calculate the magnitude of the force each busbar exerts on the other.

91. The solenoidA relay's operating coil is wound with 2000 turns over a length of 0.5 m and carries 3 A. (µ₀ = 4π × 10⁻⁷ T·m/A) Calculate the magnetic field inside the coil.

92. The solenoidA 0.25 m solenoid on a test bench carries 500 turns of magnet wire and is driven at 6 A. (µ₀ = 4π × 10⁻⁷ T·m/A) Calculate the magnetic field inside the coil.

93. Flux and FaradayA search coil of a single turn encloses 0.025 m² and is held in a uniform 1.2 T field, tilted so that its normal makes 60° with the field lines. Calculate the magnetic flux threading the loop.

94. Flux and FaradayA 150-turn search coil sits in a magnet's gap. When the magnet is de-energised, the flux through the coil falls by 10 mWb over 0.25 s. Determine the EMF induced in the coil while the flux is falling.

95. Motional EMFA 1.5 m bar slides on rails square across a 0.4 T field, and a meter across the rails reads 12 V. Determine the speed of the bar.

96. Motional EMFA 1.5 m bar slides on rails square across a 0.4 T field, and a meter across the rails reads 12 V. Determine the speed of the bar.

97. The Induction GauntletLast bench of the term. A solenoid 0.5 m long carries 2000 turns at 10 A. A search coil of 10 turns and 100 cm² sits inside it, face-on to the field. Two ways to get a voltage out of this rig are on the table: kill the solenoid's current and let the flux through the search coil collapse to nothing in 50 ms, or slide a 1.2 m bar along rails at 20 m/s through the same field. (No calculator. Today µ₀ = 1.25 × 10⁻⁶ T·m/A.) Work each line — every answer feeds the next. Determine which of the two methods delivers the larger EMF, one line at a time.

98. The Induction GauntletBonus mark, on the way out: the bench wants exactly 2 V out of a 80-turn coil, and the flux available to collapse through it is 250 µWb. Determine how quickly that flux must collapse.

Answer key

  1. 5 A
  2. 50 Ω
  3. 1680 C
  4. 7200 C
  5. 240 W
  6. 80 W
  7. 75 Ω
  8. 24 Ω
  9. 5 V
  10. 2 A
  11. 1260 mΩ
  12. 28.44 Ω
  13. 2 Ω
  14. 100 W
  15. 24 V
  16. 60 V
  17. 30 A
  18. 5 A
  19. 15 V
  20. 18 V
  21. 9 V
  22. 12 V
  23. 3 A
  24. 18 W
  25. 3 Ω
  26. 14 Ω
  27. 160 Ω
  28. 1100 Ω
  29. 5 Ω
  30. 20 Ω
  31. 100 V
  32. 1.1 J
  33. 16 µF
  34. 18 µF
  35. 2.2 s
  36. 15 kΩ
  37. 2 ms
  38. 250 mH
  39. 294.2 V
  40. 120.2 V
  41. 94.2 Ω
  42. 318.3 Ω
  43. 50 Ω
  44. 60 Ω
  45. 1006.6 Hz
  46. 63.3 mH
  47. 15915.5 Hz
  48. 318.3 Hz
  49. 800 Hz
  50. 8 (no unit)
  51. 0.8 (no unit)
  52. 0.8 (no unit)
  53. 18.19 °
  54. 15 kvar
  55. 33.3 kVA
  56. 84.9 A
  57. 103.9 A
  58. 26 A
  59. 59.6 kvar
  60. 50 kW
  61. 2500 kWh
  62. 2500 kWh
  63. 8.6 V
  64. 7.45 V
  65. 2.5 h
  66. 3.79 h
  67. 69.2 kW
  68. 75 $
  69. 2 %
  70. 8 poles
  71. 7.5 kW
  72. 79.6 N·m
  73. 85 %
  74. 42.5 kW
  75. 21.2 A
  76. 27.3 A
  77. 120 V
  78. 150 turns
  79. 5 %
  80. 22.5 V
  81. 330 kW
  82. 93.5 kW
  83. 1000 rpm
  84. 360 A
  85. 9 N
  86. 9 N
  87. 0.4 T
  88. 0.5 T
  89. 2 N
  90. 160 mN
  91. 15.08 mT
  92. 15.08 mT
  93. 15 mWb
  94. 6 V
  95. 20 m/s
  96. 20 m/s
  97. 50 mT
  98. 10 ms