Consider a vertical 2-m-diameter cylindrical furnace whose surfaces closely approximate black surfaces. The base, top, and side surfaces of the furnace are maintained at \(400 \mathrm{~K}\), \(600 \mathrm{~K}\), and \(900 \mathrm{~K}\), respectively. If the view factor from the base surface to the top surface is \(0.2\), the net radiation heat transfer from the bottom surface is (a) \(-93.6 \mathrm{~kW}\) (b) \(-86.1 \mathrm{~kW}\) (c) \(0 \mathrm{~kW}\) (d) \(86.1 \mathrm{~kW}\) (e) \(93.6 \mathrm{~kW}\)

Short Answer

Expert verified
The problem might require a more complex solution involving additional assumptions. As shown in our step-by-step solution, when considering the given view factor and base, top, and side surface temperatures, we find a negative net radiation heat transfer which doesn't match any available options. Discussions with your teacher or consulting a textbook may provide further clarification on this exercise.

Step by step solution

01

Understand the problem and collect information

We have a cylindrical furnace with given temperatures for the base, top, and side surfaces. The view factor from the base surface to the top surface is also given. We need to find the net radiation heat transfer from the base surface to the top surface. Given information: Base temperature T1 = \(400\,\text{K}\) Top temperature T2 = \(600\,\text{K}\) Side surface temperature T3 = \(900\,\text{K}\) View factor F12 = \(0.2\)
02

Calculate radiosity and emissive power for each surface

First, let's calculate the emissive power \(E_{i}\), where \(i=1,2,3\), for each surface using Stefan-Boltzmann's law which states, \(E = \sigma \cdot T^4\). The Stefan-Boltzmann constant, \(\sigma\), is equal to \(5.67 \times 10^{-8} \,\text{Wm}^{-2} \text{K}^{-4}\). \(E_1 = \sigma \cdot T_1^4 = (5.67 \times 10^{-8})(400^4) = 1829.27 \,\text{W/m}^2\) \(E_2 = \sigma \cdot T_2^4 = (5.67 \times 10^{-8})(600^4) = 12372.57 \,\text{W/m}^2\) \(E_3 = \sigma \cdot T_3^4 = (5.67 \times 10^{-8})(900^4) = 77763.47 \,\text{W/m}^2\) Next, calculate the radiosity, \(J_{i}\) for each surface using the emissive power for black bodies and considering the view factors. \(J_1 = E_1 - (1 - F_{12}) (E_1 - E_2) = 1829.27 - (1 - 0.2) (1829.27 - 12372.57) = 5628.97 \, \text{W/m}^2\) \(J_2 = E_2 - F_{12} (E_2 - E_1) = 12372.57 - 0.2 (12372.57 - 1829.27) = 9417.55\, \text{W/m}^2\) There is no need to calculate \(J_3\) for this problem, as we are finding the net radiation heat transfer between the base and top surfaces, which will not consider the side surface.
03

Calculate the net radiation heat transfer

Now, calculate the net radiation heat transfer from the base surface (q1) using the radiosity and view factors. \(Q_1 = q_{1} \cdot A_1 = F_{12} \cdot (J_1 - J_2) \cdot A_1\) Since we are interested in the value of the net radiation heat transfer, we will leave out the area of the surface as it will be used to normalize the results. Thus, \(q_1 = F_{12} (J_1 - J_2)\) \(q_1 = 0.2 (5628.97 - 9417.55) = -757.72 \, \text{W/m}^2\) The diameter of the furnace is 2 m, so the area of the base surface is: \(A_1 = \pi (\dfrac{d}{2})^2 = \pi (1^2) = \pi \,\text{m}^2\) Finally, find the net radiation heat transfer \(Q_1\) by multiplying \(q_1\) by the area of the base surface: \(Q_1 = -757.72 \,\text{W/m}^2 \times \pi \,\text{m}^2 = -2381.15\,\text{W}\) Now, we convert the net radiation heat transfer to \(\mathrm{kW}\): \(Q_1 = -2381.15\,\mathrm{W} \times \dfrac{1\,\mathrm{kW}}{1000\,\mathrm{W}} = -2.381\,\mathrm{kW}\) As the answer is not within the given options, let's consider that the question only involves the base and top surfaces, with the view factor \(F_{12}=1.0\) and ignore the sidewalls. In this case, \(q_1 = F_{12} (J_1 - J_2)\) \(q_1 = 1.0 (5628.97 - 9417.55) = -3788.58 \,\text{W/m}^2\) \(Q_1 = -3788.58 \,\text{W/m}^2 \times \pi \,\text{m}^2 = -11893.15\,\text{W}\) \(Q_1 = -11893.15\,\mathrm{W} \times \dfrac{1\,\mathrm{kW}}{1000\,\mathrm{W}} = -11.893\,\mathrm{kW}\) Once again, this result doesn't match any of the answer choices. There might be an error in the given options, or the exercise might require a more complex solution involving additional assumptions. In this case, we recommend consulting a textbook or discussing the problem with your teacher to receive further clarification.

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Most popular questions from this chapter

A 70-cm-diameter flat black disk is placed at the center of the ceiling of a \(1-\mathrm{m} \times 1-\mathrm{m} \times 1-\mathrm{m}\) black box. If the temperature of the box is \(620^{\circ} \mathrm{C}\) and the temperature of the disk is \(27^{\circ} \mathrm{C}\), the rate of heat transfer by radiation between the interior of the box and the disk is (a) \(2 \mathrm{~kW}\) (b) \(5 \mathrm{~kW}\) (c) \(8 \mathrm{~kW}\) (d) \(11 \mathrm{~kW}\) (e) \(14 \mathrm{~kW}\)

Consider a vertical 2-m-diameter cylindrical furnace whose surfaces closely approximate black surfaces. The base, top, and side surfaces of the furnace are maintained at \(400 \mathrm{~K}\), \(600 \mathrm{~K}\), and \(900 \mathrm{~K}\), respectively. If the view factor from the base surface to the top surface is \(0.2\), the net radiation heat transfer between the base and the side surfaces is (a) \(22.5 \mathrm{~kW}\) (b) \(38.6 \mathrm{~kW}\) (c) \(60.7 \mathrm{~kW}\) (d) \(89.8 \mathrm{~kW}\) (e) \(151 \mathrm{~kW}\)

Two square plates, with the sides \(a\) and \(b\) (and \(b>a\) ), are coaxial and parallel to each other, as shown in Fig. P13-132, and they are separated by a center-to-center distance of \(L\). The radiation view factor from the smaller to the larger plate, \(F_{a b}\), is given by $$ F_{a b}=\frac{1}{2 A}\left\\{\left[(B+A)^{2}+4\right]^{0.5}-\left[(B-A)^{2}+4\right]^{0.5}\right\\} $$ where, \(A=a / L\) and \(B=b / L\). (a) Calculate the view factors \(F_{a b}\) and \(F_{b a}\) for \(a=20 \mathrm{~cm}\), \(b=60 \mathrm{~cm}\), and \(L=40 \mathrm{~cm}\). (b) Calculate the net rate of radiation heat exchange between the two plates described above if \(T_{a}=800^{\circ} \mathrm{C}\), \(T_{b}=200^{\circ} \mathrm{C}, \varepsilon_{a}=0.8\), and \(\varepsilon_{b}=0.4\). (c) A large square plate (with the side \(c=2.0 \mathrm{~m}, \varepsilon_{c}=0.1\), and negligible thickness) is inserted symmetrically between the two plates such that it is parallel to and equidistant from them. For the data given above, calculate the temperature of this third plate when steady operating conditions are established.

Consider an infinitely long three-sided triangular enclosure with side lengths \(2 \mathrm{~cm}, 3 \mathrm{~cm}\), and \(4 \mathrm{~cm}\). The view factor from the \(2 \mathrm{~cm}\) side to the \(4 \mathrm{~cm}\) side is (a) \(0.25\) (b) \(0.50\) (c) \(0.64\) (d) \(0.75\) (e) \(0.87\)

Consider a 20-cm-diameter hemispherical enclosure. The dome is maintained at \(600 \mathrm{~K}\) and heat is supplied from the dome at a rate of \(50 \mathrm{~W}\) while the base surface with an emissivity of \(0.55\) is maintained at \(400 \mathrm{~K}\). Determine the emissivity of the dome.

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