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=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 \(1200 \mathrm{~K}\), 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) \(73 \mathrm{~kW}\) (b) \(126 \mathrm{~kW}\) (c) \(215 \mathrm{~kW}\) (d) \(292 \mathrm{~kW}\) (e) \(344 \mathrm{~kW}\)

Short Answer

Expert verified
Answer: (b) 126 kW

Step by step solution

01

Recall the formula for net radiation heat transfer between two surfaces

The formula to calculate the net radiation heat transfer between two black surfaces i and j is: \(Q_{i \rightarrow j} = A_i F_{i \rightarrow j} \epsilon_{ij} \sigma [T_i^4 - T_j^4]\) Where \(A_i\) is the area of surface i, \(F_{i \rightarrow j}\) is the view factor from surface i to surface j, \(\epsilon_{ij}\) is the effective emissivity between surfaces i and j, \(\sigma\) is the Stefan-Boltzmann constant(\(5.67 \times 10^{-8} \mathrm{W/m^2 K^4}\)), and \(T_i\) and \(T_j\) are the absolute temperatures of surfaces i and j, respectively. Since the surfaces are black, \(\epsilon_{ij} = 1\).
02

Calculate the area of the base surface

The base and top surfaces are circles with diameter 2 m. The area of a circle is given by the formula: \(A = \pi r^2\) The radius (r) can be calculated by dividing the diameter by 2: \(r = \frac{2}{2} = 1 \mathrm{m}\) Now, we can calculate the area (A): \(A = \pi (1 \mathrm{m})^2 = \pi \mathrm{m^2}\)
03

Find the view factor from the base surface to the side surface

Given that the view factor from the base surface to the top surface (\(F_{b \rightarrow t}\)) is 0.2, we can find the view factor from the base surface to the side surface (\(F_{b \rightarrow s}\)) using the knowledge that the sum of the view factors from one surface to all other surfaces in an enclosure must be equal to 1: \(F_{b \rightarrow s} = 1 - F_{b \rightarrow t} = 1 - 0.2 = 0.8\)
04

Calculate the net radiation heat transfer between the base and side surfaces

Now that we have all the necessary information, we can apply the formula and calculate the net radiation heat transfer: \(Q_{b \rightarrow s} = A_b F_{b \rightarrow s} \sigma [T_b^4 - T_s^4]\) Substitute the values into the equation: \(Q_{b \rightarrow s} = \pi \mathrm{m^2} (0.8) (5.67 \times 10^{-8} \mathrm{W/m^2 K^4}) [(400 \mathrm{K})^4 - (1200 \mathrm{K})^4]\) Evaluate the expression: \(Q_{b \rightarrow s} = \pi \mathrm{m^2} (0.8) (5.67 \times 10^{-8} \mathrm{W/m^2 K^4}) [(2.56 \times 10^7 \mathrm{K^4}) - (2.0736 \times 10^9 \mathrm{K^4})]\) \(Q_{b \rightarrow s} = -126.3 \mathrm{kW}\) Since the heat transfer is negative, this means that the heat is actually transferred from the side surface to the base surface. The magnitude of the heat transfer is 126.3 kW. The correct option is: (b) \(126 \mathrm{~kW}\)

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Most popular questions from this chapter

A clothed or unclothed person feels comfortable when the skin temperature is about \(33^{\circ} \mathrm{C}\). Consider an average man wearing summer clothes whose thermal resistance is \(1.1\) clo. The man feels very comfortable while standing in a room maintained at \(20^{\circ} \mathrm{C}\). If this man were to stand in that room unclothed, determine the temperature at which the room must be maintained for him to feel thermally comfortable. Assume the latent heat loss from the person to remain the same. Answer: 27.8°C

A vertical 2-m-high and 5-m-wide double-pane window consists of two sheets of glass separated by a \(3-\mathrm{cm}\)-thick air gap. In order to reduce heat transfer through the window, the air space between the two glasses is partially evacuated to \(0.3 \mathrm{~atm}\) pressure. The emissivities of the glass surfaces are \(0.9\). Taking the glass surface temperatures across the air gap to be \(15^{\circ} \mathrm{C}\) and \(5^{\circ} \mathrm{C}\), determine the rate of heat transfer through the window by natural convection and radiation.

A thin aluminum sheet with an emissivity of \(0.12\) on both sides is placed between two very large parallel plates maintained at uniform temperatures of \(T_{1}=750 \mathrm{~K}\) and \(T_{2}=400 \mathrm{~K}\). The emissivities of the plates are \(\varepsilon_{1}=0.8\) and \(\varepsilon_{2}=0.7\). Determine the net rate of radiation heat transfer between the two plates per unit surface area of the plates and the temperature of the radiation shield in steady operation.

Two very large parallel plates are maintained at uniform temperatures of \(T_{1}=600 \mathrm{~K}\) and \(T_{2}=400 \mathrm{~K}\) and have emissivities \(\varepsilon_{1}=0.5\) and \(\varepsilon_{2}=0.9\), respectively. Determine the net rate of radiation heat transfer between the two surfaces per unit area of the plates.

A long cylindrical fuel rod with a diameter of 3 cm is enclosed by a concentric tube with a diameter of \(6 \mathrm{~cm}\). The tube is an ASTM A249 904L stainless steel tube with a maximum use temperature of $260^{\circ} \mathrm{C}$ specified by the ASME Code for Process Piping (ASME B31.3-2014, Table A-1M). The gap between the fuel rod and the tube is a vacuum. The fuel rod has a surface temperature of \(550^{\circ} \mathrm{C}\). The emissivities of the fuel rod and the ASTM A249 904L tube are \(0.97\) and \(0.33\), respectively. The rate of radiation heat transfer per unit length from the fuel rod to the stainless steel tube is \(120 \mathrm{~W} / \mathrm{m}\). A concentric radiation shield with a diameter of \(45 \mathrm{~mm}\) is to be placed in between the fuel rod and the stainless steel tube to keep the temperature of the stainless steel tube from exceeding its maximum use temperature. Determine (a) the emissivity that the radiation shield needs to keep the stainless steel tube from exceeding \(260^{\circ} \mathrm{C}\) and \((b)\) the temperature of the stainless steel tube if there is no radiation shield.

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