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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.

Short Answer

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Question: Calculate the net heat transfer per unit surface area between two large parallel plates with temperatures of 750K and 400K, and emissivities of 0.8 and 0.7, respectively, separated by an aluminum radiation shield with emissivity 0.12 on both sides. Answer: First, find the view factors for each surface in contact using the given emissivities. Next, calculate the temperature of the radiation shield using the equality of heat transfers between the shield and both plates. Finally, find the net heat transfer per unit surface area between the two plates using the heat transfer equation.

Step by step solution

01

Finding the view factors

To determine the view factors of the two plates, we first look at the emissivity of the radiation shield, which is given as 0.12 for both sides. Since the aluminum sheet is a radiation shield, both plates and the radiation shield will have view factors close to 1. Therefore, we can assume \(F_{1-shield} = 0.12\) and \(F_{2-shield} = 0.12\). To find the view factors between the plates \(F_{12}\), we can use the relationship \(F_{12} = 1 - F_{1-shield} - F_{2-shield}\).
02

Calculating the temperature of the radiation shield

In steady operation, the heat transfer between plate 1 and the shield and between plate 2 and the shield should be equal. So, we can represent these two heat transfers using the following equations: *q_{1-shield} = σ * ε_1 * ε_{shield} * (T_1^4 - T_{shield}^4) * F_{1-shield} = σ * ε_2 * ε_{shield} * (T_{shield}^4 - T_2^4) * F_{2-shield}$ We can plug in the given values for the emissivities (\(ε_1 = 0.8\), \(ε_2 = 0.7\), and \(ε_{shield} = 0.12\)) and temperatures (\(T_1 = 750K\) and \(T_2 = 400K\)) into this equation, and solve for the temperature of the radiation shield, \(T_{shield}\).
03

Calculating the net heat transfer per unit surface area

Now that we have the temperature of the radiation shield, we can find the net heat transfer per unit surface area between the two plates using the total heat transfer equation: *q_{total} = σ * ε_1 * ε_2 * (T_1^4 - T_2^4) * F_{12}$ We know all the variables in the equation, so we can plug them in and solve for the net heat transfer.
04

Finalizing the solution

In conclusion, first, we found the view factors for each surface in contact. Then, we calculated the temperature of the radiation shield using the equality of heat transfers between the shield and both plates. Finally, we found the net heat transfer per unit surface area between the two plates.

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Most popular questions from this chapter

A hot liquid is being transported inside a long tube with a diameter of $25 \mathrm{~mm}$. The hot liquid causes the tube surface temperature to be \(150^{\circ} \mathrm{C}\). To prevent thermal burn hazards, the tube is enclosed by a concentric outer cylindrical cover of \(5 \mathrm{~cm}\) in diameter, creating a vacuumed gap between the two surfaces. The concentric outer cover has an emissivity of \(0.6\), and the outer surface is exposed to natural convection with a heat transfer coefficient of $8 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ and radiation heat transfer with the surroundings at a temperature of \(20^{\circ} \mathrm{C}\). Determine the necessary emissivity of the inside tube so that the outer cover temperature remains below \(45^{\circ} \mathrm{C}\) to prevent thermal burns.

Consider an infinitely long three-sided triangular enclosure with side lengths \(5 \mathrm{~cm}, 3 \mathrm{~cm}\), and \(4 \mathrm{~cm}\). The view factor from the \(5-\mathrm{cm}\) side to the \(4-\mathrm{cm}\) side is (a) \(0.3\) (b) \(0.4\) (c) \(0.5\) (d) \(0.6\) (e) \(0.7\)

Consider a long semicylindrical duct of diameter \(1.0 \mathrm{~m}\). Heat is supplied from the base surface, which is black, at a rate of $1200 \mathrm{~W} / \mathrm{m}^{2}\(, while the side surface with an emissivity of \)0.4$ is maintained at \(650 \mathrm{~K}\). Neglecting the end effects, determine the temperature of the base surface.

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) \(14 \mathrm{~kW}\)

A large ASTM A992 carbon steel plate is $(k=10 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\(. The ceramic plate has a thickness of \)10 \mathrm{~cm}$, with its lower surface at \(T_{0}=800^{\circ} \mathrm{C}\) and upper surface at \(T_{1}=700^{\circ} \mathrm{C}\). The upper surface of the ceramic plate faces the carbon steel plate. Convection occurs on the upper surface of the ceramic plate with air at \(20^{\circ} \mathrm{C}\) and a convection heat transfer coefficient of \(12 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\). The ceramic and steel plates have emissivity values of \(0.93\) and \(0.75\), respectively. The ASME Code for Process Piping specifies the maximum use temperature suitable for ASTM A992 carbon steel to be \(427^{\circ} \mathrm{C}\) (ASME B31.3-2014, Table A-1M). A radiation shield is to be placed in parallel between the two plates to keep the temperature of the steel plate from exceeding its maximum use temperature. Determine the emissivity that the radiation shield needs to keep the steel plate surface from exceeding \(427^{\circ} \mathrm{C}\).

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