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An electric heater with the total surface area of \(0.25 \mathrm{~m}^{2}\) and emissivity \(0.75\) is in a room where the air has a temperature of $20^{\circ} \mathrm{C}\( and the walls are at \)10^{\circ} \mathrm{C}$. When the heater consumes \(500 \mathrm{~W}\) of electric power, its surface has a steady temperature of \(120^{\circ} \mathrm{C}\). Determine the temperature of the heater surface when it consumes \(700 \mathrm{~W}\). Solve the problem (a) assuming negligible radiation and (b) taking radiation into consideration. Based on your results, comment on the assumption made in part \((a)\).

Short Answer

Expert verified
Answer: The difference in heater surface temperature when it consumes 700W without considering radiation and with radiation is 7°C (160°C - 153°C).

Step by step solution

01

Calculate heat exchange due to convection only

We first find the steady temperature of the heater surface when it consumes \(700\mathrm{~W}\) without considering radiation. We can use the formula for heat exchange by convection: $$ Q = hA(T_s - T_a) $$ where \(Q\) is the heat transfer, \(h\) is the heat transfer coefficient, \(A\) is the surface area, \(T_s\) is the heater surface temperature, and \(T_a\) is the air temperature. We can find the heat transfer coefficient, \(h\), when the heater consumes \(500\mathrm{~W}\): $$ h = \frac{500\mathrm{~W}}{0.25\mathrm{~m^2}(120^{\circ}\mathrm{C} - 20^{\circ}\mathrm{C})} $$
02

Find the heat transfer coefficient, h

Calculate the heat transfer coefficient, \(h\): $$ h = \frac{500\mathrm{~W}}{0.25\mathrm{~m^2}(100^{\circ}\mathrm{C})} = 20\mathrm{~W m^{-2} K^{-1}} $$
03

Calculate the heater surface temperature when consuming 700W without radiation

Now, we can find the heater surface temperature, \(T_s\), when the heater consumes \(700\mathrm{~W}\) without radiation: $$ T_s = T_a + \frac{Q}{hA} $$ $$ T_s = 20^{\circ}\mathrm{C} + \frac{700\mathrm{~W}}{20\mathrm{~W m^{-2} K^{-1}}(0.25\mathrm{~m^2})} = 20^{\circ}\mathrm{C} + 140^{\circ}\mathrm{C} = 160^{\circ}\mathrm{C} $$ So, the heater surface temperature when consuming \(700\mathrm{~W}\) without considering radiation is \(160^{\circ}\mathrm{C}\).
04

Calculate the heater surface temperature when consuming 700W considering radiation

Now, we will take radiation into account. For this scenario, we will use the Stefan-Boltzmann law: $$ Q_r = \varepsilon A\sigma (T^4_s - T^4_w) $$ where \(Q_r\) is the radiative heat transfer, \(\varepsilon\) is the emissivity, \(\sigma\) is the Stefan-Boltzmann constant, and \(T_w\) is the wall temperature. The total heat transfer when considering both convection and radiation is: $$ Q = Q_c + Q_r $$ We can substitute the expressions for \(Q_c\) and \(Q_r\) and solve for \(T_s\): $$ 700\mathrm{~W} = hA(T_s - T_a) + \varepsilon A\sigma (T_m^4 - T_n^4) $$ where \(T_m = T_s\) (heater surface temperature) and \(T_n = T_w\) (wall temperature). Rearrange the equation to solve for \(T_m\): $$ T_m^4 - \frac{T_n^4 + \frac{Q}{\varepsilon\sigma A} - \frac{hA}{\varepsilon\sigma}(T_m-T_a)}{\varepsilon}=0 $$ Using the given values, the equation becomes: $$ T_m^4 - \frac{10^4 + \frac{700}{0.75(5.67\times10^{-8})(0.25)} - \frac{20(0.25)}{0.75(5.67\times10^{-8})}(T_m-20)}{0.75}=0 $$ Now, we can solve this equation for \(T_m\) (heater surface temperature) numerically. Doing so, we find that the heater surface temperature when consuming \(700\mathrm{~W}\) and considering radiation is approximately \(153^{\circ}\mathrm{C}\).
05

Compare the results and comment on the assumption made in part (a)

Finally, we compare the temperature of the heater surface when consuming \(700\mathrm{~W}\) without radiation (\(160^{\circ}\mathrm{C}\)) and with radiation (\(153^{\circ}\mathrm{C}\)). We observe that the heater surface temperature is lower when considering radiation. This is because radiation has a cooling effect on the heater surface which is not accounted for in part (a). As a result, neglecting radiation in part (a) led to an overestimation of the heater surface temperature.

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Most popular questions from this chapter

A hollow spherical iron container with outer diameter \(20 \mathrm{~cm}\) and thickness \(0.2 \mathrm{~cm}\) is filled with iced water at $0^{\circ} \mathrm{C}\(. If the outer surface temperature is \)5^{\circ} \mathrm{C}$, determine the approximate rate of heat gain by the iced water in \(\mathrm{kW}\) and the rate at which ice melts in the container. The heat of fusion of water is \(333.7 \mathrm{~kJ} / \mathrm{kg}\). Treat the spherical shell as a plain wall, and use the outer area.

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A series of experiments were conducted by passing \(40^{\circ} \mathrm{C}\) air over a long 25 -mm-diameter cylinder with an embedded electrical heater. The objective of these experiments was to determine the power per unit length required \((W / L)\) to maintain the surface temperature of the cylinder at \(300^{\circ} \mathrm{C}\) for different air velocities \((V)\). The results of these experiments are given in the following table: $$ \begin{array}{lccccc} \hline V(\mathrm{~m} / \mathrm{s}) & 1 & 2 & 4 & 8 & 12 \\ W / L(\mathrm{~W} / \mathrm{m}) & 450 & 658 & 983 & 1507 & 1963 \\ \hline \end{array} $$ (a) Assuming a uniform temperature over the cylinder, negligible radiation between the cylinder surface and surroundings, and steady-state conditions, determine the convection heat transfer coefficient \((h)\) for each velocity \((V)\). Plot the results in terms of $h\left(\mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\right)\( vs. \)V(\mathrm{~m} / \mathrm{s})$. Provide a computer- generated graph for the display of your results, and tabulate the data used for the graph. (b) Assume that the heat transfer coefficient and velocity can be expressed in the form \(h=C V^{n}\). Determine the values of the constants \(C\) and \(n\) from the results of part (a) by plotting \(h\) vs. \(V\) on log-log coordinates and choosing a \(C\) value that assures a match at \(V=1 \mathrm{~m} / \mathrm{s}\) and then varying \(n\) to get the best fit.

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