9. Hot Plate Exp 12 pts

Thermodynamics · Thermal radiation, Heat transfer, Calorimetry

Measure emissivity of polished aluminium, the heat transfer coefficient to air, heat capacity of a metal plate, and thermal conductance of silicone rubber pads.

Solution by Jaan Kalda.

Part i (3 points)

Both aluminium plates were immersed in hot water until thermal equilibrium was reached, then removed, dried with tissue paper, and measured using an infrared thermometer. The plates have identical thermal properties except for their surface coating, so they should have reached the same actual temperature in the hot water bath. Experimental measurements:

TpolishedT_\text{polished} (°C)TblackT_\text{black} (°C)TroomT_\text{room} (°C)
26.270.922.9
26.070.722.9
25.470.222.9

The infrared thermometer measures temperature based on thermal radiation and is calibrated for emissivity ε=1\varepsilon = 1 (in reality ε=0.95\varepsilon = 0.95, but this difference is not significant). The radiation power can be linearized: Pthermal=P0+αTP_\text{thermal} = P_0 + \alpha T. Objects with ε<1\varepsilon < 1 radiate Pε=ε(P0+αTε)P_\varepsilon = \varepsilon(P_0 + \alpha T_\varepsilon), but they also reflect/scatter the radiation from the environment. If the room is at thermal equilibrium at temperature T0T_0, the room is filled with photons at equilibrium with walls at temperature T0T_0. As it follows from the second law of thermodynamics, the reflectance must be 1ε1 - \varepsilon, so it reflects/scatters power equal to Pr=(1ε)(P0+αT0)P_r = (1-\varepsilon)(P_0 + \alpha T_0). The total power departing from it is Pε+Pr=P0+εαTε+(1ε)T0P_\varepsilon + P_r = P_0 + \varepsilon\alpha T_\varepsilon + (1-\varepsilon)T_0. The IR thermometer equates this to P0+αTreadingP_0 + \alpha T_\text{reading}, hence the reading is a weighted average:

Treading=εTε+(1ε)T0.T_\text{reading} = \varepsilon\cdot T_\varepsilon + (1-\varepsilon)\cdot T_0.

Since the black plate has ε=1\varepsilon = 1, its reading directly gives the actual temperature of both plates. Rearranging to solve for emissivity:

ε=TpolishedT0TblackT0.\varepsilon = \frac{T_\text{polished} - T_0}{T_\text{black} - T_0}.

Calculating for each measurement:

ε1=26.222.970.922.9=0.069,ε2=26.022.970.722.9=0.065,ε3=25.422.970.222.9=0.053.\varepsilon_1 = \frac{26.2 - 22.9}{70.9 - 22.9} = 0.069, \quad \varepsilon_2 = \frac{26.0 - 22.9}{70.7 - 22.9} = 0.065, \quad \varepsilon_3 = \frac{25.4 - 22.9}{70.2 - 22.9} = 0.053.

Taking the average: ε=(0.069+0.065+0.053)/3=0.0620.06\varepsilon = (0.069 + 0.065 + 0.053)/3 = 0.062 \approx 0.06.

The emissivity of the polished aluminium plate is ε=0.06±0.01\varepsilon = 0.06 \pm 0.01.

Grading (preliminary)

  • The idea of heating the two plates together in water: 0.4 pts
  • Measuring the radiance of the plates properly (plates are properly dried and measurements are done in a timely manner): 0.4 pts
  • Making at least three measurements of the black plate, the polished plate and the surrounding environment (0.2 pts for each set of 3, totalling): 0.6 pts
  • Understanding that the IR temperature reading of the polished plate is affected not only by the plate itself, but also by the reflected radiation of the environment (Treading=εTactual+(1ε)TambientT_\text{reading} = \varepsilon\cdot T_\text{actual} + (1-\varepsilon)\cdot T_\text{ambient}, not just Treading=εTactualT_\text{reading} = \varepsilon\cdot T_\text{actual}): 0.3 pts
  • Deriving a correct formula for emissivity, expressed in terms of the three measured temperatures: 0.7 pts
  • Calculated value of emissivity in the range from 0.03 to 0.12: 0.6 pts (for values from 0.02 to 0.2: 0.4 pts; for values from 0.01 to 0.3: 0.2 pts)

Part ii (3 points)

Solution 1. Here the main idea is to heat the plate using the resistor. Once thermal equilibrium is reached with the plate’s temperature T=TfT = T_f, the heating power P=V2/RP = V^2/R equals the power dissipated to the environment, H(TfT0)H(T_f - T_0) (with T0T_0 denoting the room temperature), hence

H=V2/RTfT0.H = \frac{V^2/R}{T_f - T_0}.

The main difficulty is that the characteristic thermalization time is long (around 7 minutes), so for a more or less precise measurement, one should wait around half an hour.

Solution 2. The black aluminium plate was placed on the foam plastic with the resistor beneath it, providing continuous heating. Temperature readings were recorded at one-minute intervals:

tt (min)0123456
TT (°C)28.030.833.235.237.339.040.3

For heating with constant power, the temperature evolution follows T=TfθeγtT = T_f - \theta e^{-\gamma t}, where TfT_f is the final equilibrium temperature, θ\theta is a constant depending on the initial temperature, and γ\gamma is the inverse of the characteristic time constant. To determine γ\gamma, we examine successive temperature increments T(t+τ)T(t)=θeγt(eγτ1)T(t+\tau) - T(t) = \theta e^{-\gamma t}(e^{\gamma\tau} - 1) with τ=1min\tau = 1\,\text{min}, which should decrease exponentially:

lnΔTln[T(t+τ)T(t)]=γt+const.\ln\Delta T \equiv \ln[T(t+\tau) - T(t)] = -\gamma t + \text{const}.
tt (min)ΔT\Delta T (°C)ln(ΔT)\ln(\Delta T)
02.801.0296
12.400.8755
22.000.6931
32.100.7419
41.700.5306
51.300.2624

Linear regression of ln[T(t+1)T(t)]\ln[T(t+1) - T(t)] versus tt yields ln[T(t+τ)T(t)]=1.03330.1378t\ln[T(t+\tau) - T(t)] = 1.0333 - 0.1378t with R2=0.9209R^2 = 0.9209, giving γ=0.1378min1\gamma = 0.1378\,\text{min}^{-1} (time constant 1/γ7.3min1/\gamma \approx 7.3\,\text{min}).

Figure: Logarithm of the per-minute temperature increment \ln[T(t+\tau) - T(t)] plotted against time t (blue dots) for the heating run with \tau = 1\,\text{min}. The red line is the linear fit \ln\Delta T = 1.0333 - 0.1378\,t (R^2 = 0.9209); its slope gives the cooling rate \gamma = 0.1378\,\text{min}^{-1}, equivalent to a time constant 1/\gamma \approx 7.3\,\text{min}.

We then plot TT versus eγte^{-\gamma t} to find TfT_f as the intercept when eγt=0e^{-\gamma t} = 0. Linear regression yields Tf49.9°CT_f \approx 49.9\,°\text{C}:

T=49.922.0e0.1378t,R2=0.9995.T = 49.9 - 22.0\cdot e^{-0.1378t}, \quad R^2 = 0.9995.

Figure: Plate temperature T (°C) plotted against e^{-\gamma t} with \gamma = 0.1378\,\text{min}^{-1}, for the heating run. Each of the seven data points is labelled with its acquisition time (0 min through 6 min). The straight-line fit T = 49.9 - 22.0\,e^{-0.1378 t} (R^2 = 0.9995) extrapolates to the equilibrium temperature T_f \approx 49.9\,°\text{C} at e^{-\gamma t} = 0 (dashed green line).

At thermal equilibrium the power dissipated equals the power supplied:

P=U2R=hA(TfT0)=H(TfT0).P = \frac{U^2}{R} = h\cdot A\cdot(T_f - T_0) = H\cdot(T_f - T_0).

Using U=15VU = 15\,\text{V}, R=220ΩR = 220\,\Omega, A=40×40mm2=1.6×103m2A = 40\times 40\,\text{mm}^2 = 1.6\times 10^{-3}\,\text{m}^2 and T0=22.9°CT_0 = 22.9\,°\text{C}:

h=U2/RA(TfT0)23.6Wm2K1,H=hA=37.8mWK1.h = \frac{U^2/R}{A\cdot(T_f - T_0)} \approx 23.6\,\text{W\,m}^{-2}\text{K}^{-1}, \quad H = h\cdot A = 37.8\,\text{mW\,K}^{-1}.

Grading for Solution 1 (preliminary)

  • The idea of using resistive heating and waiting for thermalization: 0.5 pts
  • For waiting long enough, up to 0.8 pts: for each five minutes missing from more than 30 minutes, subtract 0.2 pts
  • The voltage is maximized to have maximal TfT_f (needed to reduce the relative error of TfT0T_f - T_0): 0.4 pts (the maximal allowed voltage of 15 V gives maximal points; each missing volt subtracts 0.1 pts)
  • Measuring the temperature and obtaining a value that is reasonable for the given voltage (difference not bigger than 1 °C): 0.6 pts
  • Deriving a correct formula for HH: 0.5 pts
  • Evaluating correctly: 0.2 pts (any mistake, either with units or arithmetic, leads to no points)

Grading for Solution 2 (preliminary)

  • Coming up with the idea of analysing exponential decay of temperature change with a graph and deriving the heat transfer coefficient from that: 0.5 pts
  • Correct equation T(t)=TfθeγtT(t) = T_f - \theta e^{-\gamma t}: 0.3 pts
  • Plotting the data to a graph to determine γ\gamma and to confirm the validity of collected data: 0.3 pts
  • At least 5 datapoints used: 0.1 pts
  • Measure for at least 5 minutes: 0.1 pts
  • Calculating the slope and retrieving γ\gamma from it: 0.2 pts
  • Finding the maximal temperature for used voltage, using plot of TT vs eγte^{-\gamma t}: 0.5 pts
  • Evaluating P=U2/R=hA(TfT0)=H(TfT0)P = U^2/R = h\cdot A\cdot(T_f - T_0) = H\cdot(T_f - T_0) without errors: 0.5 pts
  • Getting heat transfer coefficient close to expected value: 0.5 pts

Part iii (2 points)

Solution 1. To determine the heat capacity, we use the heating curve from Part ii. During heating, the energy balance is

PinPoutΔP=CdTdt,P_\text{in} - P_\text{out} \equiv \Delta P = C\frac{dT}{dt},

where Pin=U2/RP_\text{in} = U^2/R, Pout=H(TT0)P_\text{out} = H(T - T_0), and CC is the heat capacity. Using the exponential model T=TfθeγtT = T_f - \theta e^{-\gamma t}:

dTdt=θγeγt=γ(TfT).\frac{dT}{dt} = \theta\gamma e^{-\gamma t} = \gamma(T_f - T).

Substituting:

PinH(TT0)=Cγ(TfT),henceC=PinH(TT0)γ(TfT).P_\text{in} - H(T - T_0) = C\gamma(T_f - T), \quad \text{hence} \quad C = \frac{P_\text{in} - H(T - T_0)}{\gamma(T_f - T)}.

Using U=15VU = 15\,\text{V}, R=220ΩR = 220\,\Omega, H=3.78×102WK1H = 3.78\times 10^{-2}\,\text{W\,K}^{-1}, T0=22.9°CT_0 = 22.9\,°\text{C}, Tf=49.9°CT_f = 49.9\,°\text{C}, γ=0.1378min1\gamma = 0.1378\,\text{min}^{-1}, the input power is Pin=152/220=1.023WP_\text{in} = 15^2/220 = 1.023\,\text{W}.

tt (min)TT (°C)PoutP_\text{out} (W)ΔP\Delta P (W)dT/dtdT/dt (K/min)CC (J/K)
028.00.1930.8303.01816.5
130.80.2990.7242.62916.5
233.20.3890.6332.29116.6
335.20.4650.5581.99616.7
437.30.5440.4781.73916.5
539.00.6090.4141.51516.4
640.30.6580.3651.32016.6

The heat capacity values are remarkably consistent, validating our model. Taking the average yields C16.5JK1C \approx 16.5\,\text{J\,K}^{-1}.

For reference, cAl=900Jkg1K1c_\text{Al} = 900\,\text{J\,kg}^{-1}\text{K}^{-1}, so the plate mass is C/cAl=18.3gC/c_\text{Al} = 18.3\,\text{g}, consistent with a 40mm×40mm40\,\text{mm}\times 40\,\text{mm} plate with thickness approximately 2 mm.

Solution 2. A better approach is to make an additional series of measurements to obtain a cooling temperature curve, excluding the contribution of the resistor’s thermal capacity. We heat the plate (easiest by immersing in hot water) and measure T(t)T(t) as it cools. The energy balance gives

Pout=H[T(t)T0]=CdTdt=γC[T(t)T0],henceC=H/γ.P_\text{out} = H[T(t) - T_0] = -C\frac{dT}{dt} = \gamma C[T(t) - T_0], \quad \text{hence} \quad C = H/\gamma.

The decay rate γ\gamma is found from the slope of ln[T(t)T0]\ln[T(t) - T_0] plotted against tt.

Grading (preliminary)

  • The idea of using the T(t)T(t) dependence, either for cooling or heating with the resistor: 0.2 pts
  • Measuring and tabulating at least 6 data points: 0.3 pts (subtract 0.1 pts for each missing)
  • Data points cover at least 6 minutes: 0.3 pts (subtract 0.1 pts for each missing minute)
  • The idea of using log-linear plot for data linearization: 0.2 pts
  • Correct data plotting: 0.2 pts
  • Finding the slope of a fit line: 0.2 pts
  • The idea of substituting time derivative with multiplication by γ\gamma: 0.2 pts (calculating derivative by finite difference ratio ΔT/δt\Delta T/\delta t is significantly less accurate)
  • Deriving a correct formula for CC: 0.2 pts
  • Obtaining a reasonable numerical value for CC, from 13 to 20 J/K: 0.2 pts (else from 10 to 25 J/K: 0.1 pts)

Part iv (4 points)

Cooling experiments were conducted with the aluminium plate covered by different numbers of silicone rubber layers. The plate was heated in water and allowed to cool, with temperature recorded as a function of time.

tt (s)060120180240300
T1layerT_{1\,\text{layer}} (°C)65.260.255.551.347.644.6
T2layersT_{2\,\text{layers}} (°C)*35.334.032.931.930.8
T3layersT_{3\,\text{layers}} (°C)45.443.141.640.038.937.3

*The data point at t=0t = 0 for 2 layers is excluded as it did not represent complete thermal equilibrium across the silicone layers.

For a cooling process with constant ambient temperature T0T_0, the temperature follows exponential decay T(t)=T0+(TinitialT0)eγtT(t) = T_0 + (T_\text{initial} - T_0)e^{-\gamma t}. The time constant γ\gamma is related to the thermal resistance R\mathcal{R} and heat capacity CC by

γ=1RC.\gamma = \frac{1}{\mathcal{R}C}.

Taking the natural logarithm of the temperature difference from ambient yields ln[T(t)T0]=γt+const\ln[T(t) - T_0] = -\gamma t + \text{const}.

Using linear regression on the logarithmic cooling curves:

γ1layer=2.244×103s1,γ2layers=1.852×103s1,γ3layers=1.438×103s1.\gamma_{1\,\text{layer}} = 2.244\times 10^{-3}\,\text{s}^{-1}, \quad \gamma_{2\,\text{layers}} = 1.852\times 10^{-3}\,\text{s}^{-1}, \quad \gamma_{3\,\text{layers}} = 1.438\times 10^{-3}\,\text{s}^{-1}.

Figure: Cooling curves for the heated aluminium plate covered by 1 (blue), 2 (red), and 3 (green) silicone-rubber layers, plotted as \ln(T - T_0) versus time (s). Each series is well described by a straight line (Newton's law of cooling), with slopes yielding \gamma_{1\,\text{layer}} = 0.00224\,\text{s}^{-1}, \gamma_{2\,\text{layers}} = 0.00185\,\text{s}^{-1}, and \gamma_{3\,\text{layers}} = 0.00144\,\text{s}^{-1}. The 2-layer series begins at t = 60\,\text{s} (dashed segment for t < 60\,\text{s}) because the t = 0 point did not represent thermal equilibrium across the layers.

Using C=16.5JK1C = 16.5\,\text{J\,K}^{-1}, the total thermal resistance for each case is:

R1layer=1γ1C=27.0KW1,R2layers=32.7KW1,R3layers=42.1KW1.R_{1\,\text{layer}} = \frac{1}{\gamma_{1}\cdot C} = 27.0\,\text{K\,W}^{-1}, \quad R_{2\,\text{layers}} = 32.7\,\text{K\,W}^{-1}, \quad R_{3\,\text{layers}} = 42.1\,\text{K\,W}^{-1}.

Each additional layer adds a resistance ΔR=δ/(κA)\Delta R = \delta/(\kappa A), where δ\delta is the layer thickness, κ\kappa is the thermal conductivity, and AA is the area. The incremental resistances are:

ΔR12=R2layersR1layer=5.7KW1,ΔR23=R3layersR2layers=9.4KW1.\Delta R_{12} = R_{2\,\text{layers}} - R_{1\,\text{layer}} = 5.7\,\text{K\,W}^{-1}, \quad \Delta R_{23} = R_{3\,\text{layers}} - R_{2\,\text{layers}} = 9.4\,\text{K\,W}^{-1}.

Taking the average:

ΔR=ΔR12+ΔR232=7.6KW1.\overline{\Delta R} = \frac{\Delta R_{12} + \Delta R_{23}}{2} = 7.6\,\text{K\,W}^{-1}.

With δ=0.8mm=8×104m\delta = 0.8\,\text{mm} = 8\times 10^{-4}\,\text{m} and A=40×40mm2=1.6×103m2A = 40\times 40\,\text{mm}^2 = 1.6\times 10^{-3}\,\text{m}^2:

κ=δΔRA=0.066Wm1K1.\kappa = \frac{\delta}{\overline{\Delta R}\cdot A} = 0.066\,\text{W\,m}^{-1}\text{K}^{-1}.

Grading (preliminary)

  • The idea of letting the plate cool down while covering it with a different number of silicon sheets and measuring the T(t)T(t) dependencies: 0.3 pts
  • For the quantity of recorded data: within each data series, at least 6 data points: 0.3 pts (subtract 0.1 for each missing); within up to three different data series — in total up to 3×0.3=0.93\times 0.3 = 0.9 pts
  • Data points in each data series cover at least 6 minutes: 0.2 pts (0.1 pts if less than 6 but more than 4 minutes) — in total up to 0.6 pts
  • The idea of using log-linear plot for data linearization: 0.2 pts
  • Correctly plotting the data: 0.1 pts each, up to 0.3 pts
  • Calculating γ\gamma for each of the series, 0.1 pts for each, in total up to 0.3 pts
  • Correctly expressing the heat conductivity in terms of a difference of the γ\gamma values: 0.7 pts
  • Finding conductivity on the basis of all the γ\gamma values (either by pair-wise calculation, or plotting and finding the fit line slope): 0.4 pts (divide by two if only one pair of γ\gamma values was used)
  • Obtained value of κ\kappa within a reasonable range, i.e. from 0.05 to 0.1 W m1^{-1} K1^{-1}: 0.3 pts (else if from 0.04 to 0.12: 0.2 pts; else from 0.02 to 0.14: 0.1 pts)