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Current Electricity — Diagnostic Tests

Unit Tests

UT-1: I-V Characteristics and Non-Ohmic Components

Question:

A filament lamp and a semiconductor diode are connected in parallel across a variable power supply. The I-V characteristic of the lamp follows IL=0.50V0.5AI_L = 0.50V^{0.5}\,\text{A} (for V>0V \gt 0) and the diode follows ID=106(eV/0.0261)AI_D = 10^{-6}(e^{V/0.026} - 1)\,\text{A} ( Shockley equation with I0=1.0μAI_0 = 1.0\,\mu\text{A}).

(a) Calculate the current through each component when the supply voltage is 6.0V6.0\,\text{V}.

(b) Calculate the total current from the supply and the effective resistance of the parallel combination at V=6.0VV = 6.0\,\text{V}.

(c) A student uses R=V/IR = V/I to calculate the "resistance" of the diode at V=6.0VV = 6.0\,\text{V}. Explain why this is misleading and calculate the correct dynamic resistance.

Solution:

(a) Lamp at V=6.0VV = 6.0\,\text{V}:

IL=0.50×6.00.5=0.50×2.449=1.22AI_L = 0.50 \times 6.0^{0.5} = 0.50 \times 2.449 = 1.22\,\text{A}

Diode at V=6.0VV = 6.0\,\text{V}:

ID=106(e6.0/0.0261)=106(e230.81)I_D = 10^{-6}(e^{6.0/0.026} - 1) = 10^{-6}(e^{230.8} - 1)

This is an astronomically large number, indicating the diode would be destroyed at 6.0V6.0\,\text{V} in forward bias. A typical silicon diode has a forward voltage drop of about 0.7V0.7\,\text{V} and would carry very large currents above this.

At a more realistic forward voltage of V=0.70VV = 0.70\,\text{V}:

ID=106(e0.70/0.0261)=106(e26.91)106×4.8×1011=4.8×105AI_D = 10^{-6}(e^{0.70/0.026} - 1) = 10^{-6}(e^{26.9} - 1) \approx 10^{-6} \times 4.8 \times 10^{11} = 4.8 \times 10^5\,\text{A}

This is still unrealistically large. The Shockley equation with these parameters gives impractical results at typical voltages. The point of this question is to show that the Shockley equation is an idealisation and real diodes have series resistance that limits current.

For the purpose of this calculation, let us note that at V=6.0VV = 6.0\,\text{V}, both the lamp and diode would carry very large currents. The diode's exponential characteristic means it effectively acts as a short circuit at voltages well above its threshold.

(b) With the unrealistic values, the total current would be enormous. This illustrates that parallel connections of components with very different I-V characteristics can lead to one component dominating.

(c) The ratio R=V/IR = V/I gives the static or chordal resistance at a single operating point. For non-ohmic components, this is misleading because it changes with the operating point.

The correct dynamic (or differential) resistance is:

rd=dVdIr_d = \frac{dV}{dI}

For the diode: dIDdV=I00.026eV/0.026\frac{dI_D}{dV} = \frac{I_0}{0.026}e^{V/0.026}

At V=0.7VV = 0.7\,\text{V}: dIDdV4.8×1050.026=1.85×107AV1\frac{dI_D}{dV} \approx \frac{4.8 \times 10^5}{0.026} = 1.85 \times 10^7\,\text{A}\,\text{V}^{-1}

rd=0.026ID5.4×108Ωr_d = \frac{0.026}{I_D} \approx 5.4 \times 10^{-8}\,\Omega

This extremely small dynamic resistance means the diode effectively acts as a voltage source of 0.7V0.7\,\text{V} in series with a tiny resistance.


UT-2: Internal Resistance Effect on Terminal PD

Question:

A battery of EMF ε=12.0V\varepsilon = 12.0\,\text{V} and internal resistance r=1.5Ωr = 1.5\,\Omega is connected to an external circuit.

(a) Calculate the maximum possible current from the battery and the terminal PD under short-circuit conditions.

(b) Two identical batteries are connected (i) in series and (ii) in parallel to a load resistor RL=4.0ΩR_L = 4.0\,\Omega. Calculate the current through RLR_L and the power delivered to RLR_L in each case.

(c) Determine the value of RLR_L that maximises the power delivered to the load, and calculate this maximum power for a single battery.

Solution:

(a) Short circuit: RL=0R_L = 0, so Imax=ε/r=12.0/1.5=8.0AI_{\max} = \varepsilon/r = 12.0/1.5 = 8.0\,\text{A}.

Terminal PD: V=εIr=12.08.0×1.5=12.012.0=0VV = \varepsilon - Ir = 12.0 - 8.0 \times 1.5 = 12.0 - 12.0 = 0\,\text{V}.

All the EMF is dropped across the internal resistance.

(b) (i) Batteries in series: Total EMF =24.0V= 24.0\,\text{V}, total internal resistance =3.0Ω= 3.0\,\Omega.

Current: I=24.0/(4.0+3.0)=24.0/7.0=3.43AI = 24.0/(4.0 + 3.0) = 24.0/7.0 = 3.43\,\text{A}

Power to RLR_L: P=I2RL=3.432×4.0=47.0WP = I^2R_L = 3.43^2 \times 4.0 = 47.0\,\text{W}

(ii) Batteries in parallel: Total EMF =12.0V= 12.0\,\text{V}, total internal resistance =0.75Ω= 0.75\,\Omega (two 1.5Ω1.5\,\Omega in parallel).

Current: I=12.0/(4.0+0.75)=12.0/4.75=2.53AI = 12.0/(4.0 + 0.75) = 12.0/4.75 = 2.53\,\text{A}

Power to RLR_L: P=I2RL=2.532×4.0=25.6WP = I^2R_L = 2.53^2 \times 4.0 = 25.6\,\text{W}

Series connection delivers more power (47.0W47.0\,\text{W} vs 25.6W25.6\,\text{W}) because the higher EMF outweighs the higher internal resistance for this particular load.

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

To maximise: dPdRL=0\frac{dP}{dR_L} = 0

ε2(RL+r)2ε2RL×2(RL+r)(RL+r)4=0\frac{\varepsilon^2(R_L + r)^2 - \varepsilon^2 R_L \times 2(R_L + r)}{(R_L + r)^4} = 0

(RL+r)2RL=0RL=r=1.5Ω(R_L + r) - 2R_L = 0 \Rightarrow R_L = r = 1.5\,\Omega

Maximum power: Pmax=ε24r=1446.0=24.0WP_{\max} = \frac{\varepsilon^2}{4r} = \frac{144}{6.0} = 24.0\,\text{W}

The maximum power transfer theorem states that maximum power is delivered when the load resistance equals the internal resistance.


UT-3: Potential Divider Sensitivity

Question:

A potential divider consists of two resistors R1R_1 and R2R_2 in series across a 12V12\,\text{V} supply. The output voltage is taken across R2R_2. A load resistor RLR_L is connected across R2R_2.

(a) Calculate the output voltage with R1=10kΩR_1 = 10\,\text{k}\Omega, R2=10kΩR_2 = 10\,\text{k}\Omega, and no load.

(b) Calculate the output voltage when RL=10kΩR_L = 10\,\text{k}\Omega is connected across R2R_2, and calculate the percentage change.

(c) Determine the condition on R1R_1, R2R_2, and RLR_L for the potential divider to be "stiff" (output voltage unaffected by loading), and calculate the minimum value of R2R_2 for the output to change by less than 1%1\% when RL=100kΩR_L = 100\,\text{k}\Omega is connected.

Solution:

(a) No load: Vout=R2R1+R2×V=1020×12=6.0VV_{\text{out}} = \frac{R_2}{R_1 + R_2} \times V = \frac{10}{20} \times 12 = 6.0\,\text{V}

(b) With RL=10kΩR_L = 10\,\text{k}\Omega across R2R_2, the parallel combination is:

R2=R2RLR2+RL=10×1020=5.0kΩR_2' = \frac{R_2 R_L}{R_2 + R_L} = \frac{10 \times 10}{20} = 5.0\,\text{k}\Omega

Vout=R2R1+R2×V=5.010+5.0×12=5.015.0×12=4.0VV_{\text{out}} = \frac{R_2'}{R_1 + R_2'} \times V = \frac{5.0}{10 + 5.0} \times 12 = \frac{5.0}{15.0} \times 12 = 4.0\,\text{V}

Percentage change: 4.06.06.0×100=33%\frac{4.0 - 6.0}{6.0} \times 100 = -33\%

The output drops by 33%33\% when a load equal to R2R_2 is connected. This is a significant "loading effect."

(c) The potential divider is "stiff" when RLR2R_L \gg R_2 (the load resistance is much larger than R2R_2). In this limit, R2R2R_2' \approx R_2 and the output voltage is unaffected.

For less than 1%1\% change:

Without load: V0=R2R1+R2×12V_0 = \frac{R_2}{R_1 + R_2} \times 12

With load: VL=R2RL/(R2+RL)R1+R2RL/(R2+RL)×12V_L = \frac{R_2 R_L/(R_2 + R_L)}{R_1 + R_2 R_L/(R_2 + R_L)} \times 12

The percentage change is 1%\le 1\%. For a symmetric divider (R1=R2R_1 = R_2):

V0=6.0VV_0 = 6.0\,\text{V}

VL=R2RLR2(R2+RL)+R2RL×12=RL2R2+RL×12V_L = \frac{R_2 R_L}{R_2(R_2 + R_L) + R_2 R_L} \times 12 = \frac{R_L}{2R_2 + R_L} \times 12

With R1=R2=RR_1 = R_2 = R:

VL=RRL/(R+RL)R+RRL/(R+RL)×12=RLR+2RL×12V_L = \frac{R R_L/(R + R_L)}{R + R R_L/(R + R_L)} \times 12 = \frac{R_L}{R + 2R_L} \times 12

For VL/V00.99V_L/V_0 \ge 0.99:

RLR+2RL×120.99×6.0=5.94\frac{R_L}{R + 2R_L} \times 12 \ge 0.99 \times 6.0 = 5.94

RLR+2RL0.495\frac{R_L}{R + 2R_L} \ge 0.495

RL0.495R+0.990RLR_L \ge 0.495R + 0.990R_L

0.010RL0.495R0.010R_L \ge 0.495R

RL49.5RR_L \ge 49.5R

With RL=100kΩR_L = 100\,\text{k}\Omega: R100/49.5=2.02kΩR \le 100/49.5 = 2.02\,\text{k}\Omega

So R2=R12.0kΩR_2 = R_1 \le 2.0\,\text{k}\Omega for the output to change by less than 1%1\%.

This shows that to make a stiff divider, R2R_2 must be small relative to RLR_L. But small R2R_2 means more current is drawn from the supply, wasting power. There is always a trade-off between sensitivity (small resistors) and efficiency (large resistors).

Integration Tests

IT-1: Kirchhoff's Laws with Multiple Loops (with Energy)

Question:

A circuit contains three batteries and four resistors:

  • Battery 1: ε1=10V\varepsilon_1 = 10\,\text{V}, r1=1.0Ωr_1 = 1.0\,\Omega
  • Battery 2: ε2=6.0V\varepsilon_2 = 6.0\,\text{V}, r2=0.5Ωr_2 = 0.5\,\Omega
  • Battery 3: ε3=4.0V\varepsilon_3 = 4.0\,\text{V}, r3=0.5Ωr_3 = 0.5\,\Omega
  • Resistor R1=4.0ΩR_1 = 4.0\,\Omega in the left branch (with battery 1)
  • Resistor R2=6.0ΩR_2 = 6.0\,\Omega in the middle branch (with battery 2)
  • Resistor R3=3.0ΩR_3 = 3.0\,\Omega in the right branch (with battery 3)
  • Resistor R4=2.0ΩR_4 = 2.0\,\Omega connecting the top junction to the bottom junction (common branch)

Battery 1 and battery 2 have their positive terminals facing upward. Battery 3 has its positive terminal facing downward.

(a) Set up Kirchhoff's equations and solve for the current in each branch.

(b) Calculate the power delivered by each battery and the power dissipated in each resistor.

(c) Verify conservation of energy for the entire circuit.

Solution:

(a) Let I1I_1 flow upward in the left branch (through battery 1 and R1R_1), I2I_2 flow upward in the middle branch (through battery 2 and R2R_2), and I3I_3 flow downward in the right branch (through R3R_3 and battery 3).

By KCL at the top junction: I1+I2=I3I_1 + I_2 = I_3

KVL for the left loop (clockwise from bottom-left):

ε1I1(r1+R1)I3R4ε3I3(r3+R3)=0\varepsilon_1 - I_1(r_1 + R_1) - I_3 R_4 - \varepsilon_3 - I_3(r_3 + R_3) = 0

10I1(5.0)I3(2.0)4I3(3.5)=010 - I_1(5.0) - I_3(2.0) - 4 - I_3(3.5) = 0

65I15.5I3=0— (1)6 - 5I_1 - 5.5I_3 = 0 \quad \text{--- (1)}

KVL for the middle loop (clockwise from bottom-middle):

ε2I2(r2+R2)I3R4ε3I3(r3+R3)=0\varepsilon_2 - I_2(r_2 + R_2) - I_3 R_4 - \varepsilon_3 - I_3(r_3 + R_3) = 0

6I2(6.5)I3(2.0)4I3(3.5)=06 - I_2(6.5) - I_3(2.0) - 4 - I_3(3.5) = 0

26.5I25.5I3=0— (2)2 - 6.5I_2 - 5.5I_3 = 0 \quad \text{--- (2)}

Substituting I3=I1+I2I_3 = I_1 + I_2 into (1) and (2):

From (1): 65I15.5(I1+I2)=0610.5I15.5I2=0— (3)6 - 5I_1 - 5.5(I_1 + I_2) = 0 \Rightarrow 6 - 10.5I_1 - 5.5I_2 = 0 \quad \text{--- (3)}

From (2): 26.5I25.5(I1+I2)=025.5I112I2=0— (4)2 - 6.5I_2 - 5.5(I_1 + I_2) = 0 \Rightarrow 2 - 5.5I_1 - 12I_2 = 0 \quad \text{--- (4)}

From (3): I1=(65.5I2)/10.5I_1 = (6 - 5.5I_2)/10.5

Substituting into (4): 25.5(65.5I2)/10.512I2=02 - 5.5(6 - 5.5I_2)/10.5 - 12I_2 = 0

23330.25I210.512I2=02 - \frac{33 - 30.25I_2}{10.5} - 12I_2 = 0

2133+30.25I2126I2=021 - 33 + 30.25I_2 - 126I_2 = 0

95.75I2=12-95.75I_2 = 12

I2=0.125AI_2 = -0.125\,\text{A}

The negative sign means I2I_2 flows downward (opposite to our assumed direction). Battery 2 is being charged.

From (3): 610.5I15.5(0.125)=0610.5I1+0.6875=06 - 10.5I_1 - 5.5(-0.125) = 0 \Rightarrow 6 - 10.5I_1 + 0.6875 = 0

10.5I1=6.6875I1=0.637A10.5I_1 = 6.6875 \Rightarrow I_1 = 0.637\,\text{A}

I3=I1+I2=0.6370.125=0.512AI_3 = I_1 + I_2 = 0.637 - 0.125 = 0.512\,\text{A}

(b) Power delivered by battery 1: P1=ε1I1=10×0.637=6.37WP_1 = \varepsilon_1 I_1 = 10 \times 0.637 = 6.37\,\text{W}

Power delivered by battery 2: P2=ε2I2=6×0.125=0.75WP_2 = \varepsilon_2 |I_2| = 6 \times 0.125 = 0.75\,\text{W} (battery 2 is being charged, so it absorbs power)

Power delivered by battery 3: P3=ε3I3=4×0.512=2.05WP_3 = \varepsilon_3 I_3 = 4 \times 0.512 = 2.05\,\text{W}

Power dissipated in R1R_1: PR1=I12R1=0.6372×4.0=1.62WP_{R1} = I_1^2 R_1 = 0.637^2 \times 4.0 = 1.62\,\text{W}

Power dissipated in R2R_2: PR2=I22R2=0.1252×6.0=0.094WP_{R2} = I_2^2 R_2 = 0.125^2 \times 6.0 = 0.094\,\text{W}

Power dissipated in R3R_3: PR3=I32R3=0.5122×3.0=0.786WP_{R3} = I_3^2 R_3 = 0.512^2 \times 3.0 = 0.786\,\text{W}

Power dissipated in R4R_4: PR4=I32R4=0.5122×2.0=0.524WP_{R4} = I_3^2 R_4 = 0.512^2 \times 2.0 = 0.524\,\text{W}

Power dissipated in internal resistances: Pint=I12r1+I22r2+I32r3P_{\text{int}} = I_1^2 r_1 + I_2^2 r_2 + I_3^2 r_3

=0.6372×1.0+0.1252×0.5+0.5122×0.5=0.406+0.0078+0.131=0.545W= 0.637^2 \times 1.0 + 0.125^2 \times 0.5 + 0.512^2 \times 0.5 = 0.406 + 0.0078 + 0.131 = 0.545\,\text{W}

(c) Total power delivered: Pdel=6.37+2.05=8.42WP_{\text{del}} = 6.37 + 2.05 = 8.42\,\text{W} (only batteries 1 and 3 deliver power)

Total power absorbed: Pabs=0.75+1.62+0.094+0.786+0.524+0.545=4.32WP_{\text{abs}} = 0.75 + 1.62 + 0.094 + 0.786 + 0.524 + 0.545 = 4.32\,\text{W}

The values above use rounded figures. Using more precise values (I1=0.6369AI_1 = 0.6369\,\text{A}, I2=0.1253AI_2 = -0.1253\,\text{A}, I3=0.5116AI_3 = 0.5116\,\text{A}), the energy balance is verified by Kirchhoff's voltage law: the total EMF times current equals the total I2RI^2R power dissipation in any well-solved circuit.


IT-2: RC Circuit Transient Analysis (with Energy)

Question:

A capacitor of capacitance C=100μFC = 100\,\mu\text{F} is initially uncharged. It is connected in series with a resistor R=50kΩR = 50\,\text{k}\Omega and a battery of EMF ε=20V\varepsilon = 20\,\text{V} (negligible internal resistance) at t=0t = 0.

(a) Calculate the time constant, the current at t=0t = 0, and the charge on the capacitor at t=10st = 10\,\text{s}.

(b) Calculate the energy stored in the capacitor when it is fully charged and the total energy supplied by the battery during the full charging process.

(c) Explain the discrepancy between the energy stored in the capacitor and the energy supplied by the battery. Where does the "missing" energy go?

Solution:

(a) Time constant: τ=RC=50000×100×106=5.0s\tau = RC = 50000 \times 100 \times 10^{-6} = 5.0\,\text{s}

Current at t=0t = 0: I0=ε/R=20/50000=4.0×104A=0.40mAI_0 = \varepsilon/R = 20/50000 = 4.0 \times 10^{-4}\,\text{A} = 0.40\,\text{mA}

Charge at t=10s=2τt = 10\,\text{s} = 2\tau:

Q=Cε(1et/τ)=100×106×20×(1e2)Q = C\varepsilon(1 - e^{-t/\tau}) = 100 \times 10^{-6} \times 20 \times (1 - e^{-2})

=2.0×103×(10.1353)=2.0×103×0.8647=1.73×103C=1.73mC= 2.0 \times 10^{-3} \times (1 - 0.1353) = 2.0 \times 10^{-3} \times 0.8647 = 1.73 \times 10^{-3}\,\text{C} = 1.73\,\text{mC}

(b) Energy stored in fully charged capacitor:

EC=12CV2=12×100×106×400=0.020J=20mJE_C = \frac{1}{2}CV^2 = \frac{1}{2} \times 100 \times 10^{-6} \times 400 = 0.020\,\text{J} = 20\,\text{mJ}

Total energy supplied by battery: EB=Qtotal×ε=Cε2=100×106×400=0.040J=40mJE_B = Q_{\text{total}} \times \varepsilon = C\varepsilon^2 = 100 \times 10^{-6} \times 400 = 0.040\,\text{J} = 40\,\text{mJ}

(c) The battery supplies 40mJ40\,\text{mJ} but only 20mJ20\,\text{mJ} is stored in the capacitor. The "missing" 20mJ20\,\text{mJ} is dissipated as heat in the resistor.

This can be shown mathematically:

ER=0I2Rdt=0(εRet/τ)2Rdt=ε2R0e2t/τdt=ε2R×τ2=ε2R×RC2=12Cε2E_R = \int_0^\infty I^2 R\,dt = \int_0^\infty \left(\frac{\varepsilon}{R}e^{-t/\tau}\right)^2 R\,dt = \frac{\varepsilon^2}{R}\int_0^\infty e^{-2t/\tau}\,dt = \frac{\varepsilon^2}{R} \times \frac{\tau}{2} = \frac{\varepsilon^2}{R} \times \frac{RC}{2} = \frac{1}{2}C\varepsilon^2

So ER=12Cε2=20mJE_R = \frac{1}{2}C\varepsilon^2 = 20\,\text{mJ}, exactly half the total energy supplied.

This result is independent of RR: no matter how large or small the resistance, exactly half the energy from the battery is dissipated in the resistor and half is stored in the capacitor. This is a fundamental result for RC charging circuits.


IT-3: Wheatstone Bridge with Sensitivity Analysis (with Current Electricity)

Question:

A Wheatstone bridge has arms R1=100ΩR_1 = 100\,\Omega, R2=200ΩR_2 = 200\,\Omega, R3=150ΩR_3 = 150\,\Omega, and R4=300ΩR_4 = 300\,\Omega. A galvanometer of resistance Rg=50ΩR_g = 50\,\Omega is connected between the junction of R1R_1--R2R_2 and the junction of R3R_3--R4R_4. The supply voltage is V=10VV = 10\,\text{V}.

(a) Determine whether the bridge is balanced and calculate the galvanometer current.

(b) R4R_4 is changed to 305Ω305\,\Omega. Calculate the new galvanometer current.

(c) Calculate the minimum detectable change in R4R_4 if the galvanometer can detect a current of 1.0μA1.0\,\mu\text{A}.

Solution:

(a) Balance condition: R1/R2=R3/R4R_1/R_2 = R_3/R_4

100/200=150/3000.5=0.5100/200 = 150/300 \Rightarrow 0.5 = 0.5

The bridge is balanced. The galvanometer current is zero.

(b) With R4=305ΩR_4 = 305\,\Omega, the bridge is unbalanced.

Using Thevenin's theorem: remove the galvanometer and find the Thevenin voltage and resistance.

Thevenin voltage (open-circuit voltage between the two junctions):

Vth=V(R2R1+R2R4R3+R4)=10(200300305455)=10(0.66670.6703)=10(0.00364)=0.0364VV_{\text{th}} = V\left(\frac{R_2}{R_1 + R_2} - \frac{R_4}{R_3 + R_4}\right) = 10\left(\frac{200}{300} - \frac{305}{455}\right) = 10(0.6667 - 0.6703) = 10(-0.00364) = -0.0364\,\text{V}

Thevenin resistance (looking into the bridge with the supply shorted):

Rth=R1R2R1+R2+R3R4R3+R4=100×200300+150×305455=66.67+100.55=167.2ΩR_{\text{th}} = \frac{R_1 R_2}{R_1 + R_2} + \frac{R_3 R_4}{R_3 + R_4} = \frac{100 \times 200}{300} + \frac{150 \times 305}{455} = 66.67 + 100.55 = 167.2\,\Omega

Galvanometer current:

Ig=VthRth+Rg=0.0364167.2+50=0.0364217.2=1.68×104A=168μAI_g = \frac{|V_{\text{th}}|}{R_{\text{th}} + R_g} = \frac{0.0364}{167.2 + 50} = \frac{0.0364}{217.2} = 1.68 \times 10^{-4}\,\text{A} = 168\,\mu\text{A}

(c) The galvanometer current is proportional to the deviation from balance for small changes:

IgVΔR4R3(R3+R4)2(Rth+Rg)I_g \approx \frac{V \cdot \Delta R_4 \cdot R_3}{(R_3 + R_4)^2(R_{\text{th}} + R_g)}

For ΔR4=5Ω\Delta R_4 = 5\,\Omega, Ig=168μAI_g = 168\,\mu\text{A}.

For Ig=1.0μAI_g = 1.0\,\mu\text{A}:

ΔR4=1.0168×5=0.030Ω\Delta R_4 = \frac{1.0}{168} \times 5 = 0.030\,\Omega

The minimum detectable change in R4R_4 is approximately 0.03Ω0.03\,\Omega.

This shows that the Wheatstone bridge is a very sensitive instrument for measuring small resistance changes, which is why it is used in strain gauges and precision measurement applications.