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A 9-ft-high room with a base area of \(12 \mathrm{ft} \times 12 \mathrm{ft}\) is to be heated by electric resistance heaters placed on the ceiling, which is maintained at a uniform temperature of \(90^{\circ} \mathrm{F}\) at all times. The floor of the room is at \(65^{\circ} \mathrm{F}\) and has an emissivity of \(0.8\). The side surfaces are well insulated. Treating the ceiling as a blackbody, determine the rate of heat loss from the room through the floor.

Short Answer

Expert verified
Answer: The rate of heat loss from the room through the floor is approximately 1032.54 Watts.

Step by step solution

01

Identify constants and variables

First, let's list the given information: - Room dimensions: height of 9ft, base area of 12ft x 12ft - Ceiling temperature: \(T_c = 90^{\circ} F = (90 + 459.67) \,\mathrm {Rankine} = 549.67 \, \mathrm{R}\) (converted to Rankine for calculations) - Floor temperature: \(T_f = 65^{\circ} F = (65 + 459.67) \,\mathrm {Rankine} = 524.67 \, \mathrm{R}\) (converted to Rankine for calculations) - Emissivity of the floor: \(ε = 0.8\) - Ceiling treated as a blackbody (emissivity = 1)
02

Calculate the heat loss using the Stefan-Boltzmann Law

We need to find the heat loss rate through the floor using the Stefan-Boltzmann Law: $$q = εσA(T_c^4 - T_f^4)$$ where: - \(q\) is the heat loss rate - \(ε\) is the emissivity - \(σ\) is the Stefan-Boltzmann constant, \(5.67 \times 10^{-8} \, \frac {\mathrm{W}} {\mathrm{m^2} \cdot \mathrm{K^4}}\) - \(A\) is the area of the floor - \(T_c\) is the temperature of the ceiling in Rankine - \(T_f\) is the temperature of the floor in Rankine
03

Convert the area to metric units

Since we are using metric units for our Stefan-Boltzmann constant, we need to convert the base area of the room to metric units: $$A = 12 \,\mathrm{ft} × 12 \,\mathrm{ft} = 144\, \mathrm{ft^2} = 13.38 \,\mathrm{m^2}$$
04

Calculate the heat loss rate

Now we can plug in the values we found in Steps 1-3 into the Stefan-Boltzmann Law and solve for \(q\): $$q = 0.8 \times 5.67 \times 10^{-8}\, \frac {\mathrm{W}} {\mathrm{m^2} \cdot \mathrm{K^4}} \times 13.38\, \mathrm{m^2}((549.67\, \mathrm{R})^4 - (524.67\, \mathrm{R})^4)$$ After calculating, we find: $$q \approx 1032.54 \, \mathrm{W}$$ So, the rate of heat loss from the room through the floor is approximately 1032.54 Watts.

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Most popular questions from this chapter

Two very large parallel plates are maintained at uniform temperatures of \(T_{1}=1100 \mathrm{~K}\) and \(T_{2}=700 \mathrm{~K}\) and have emissivities of \(\varepsilon_{1}=\varepsilon_{2}=0.5\), respectively. It is desired to reduce the net rate of radiation heat transfer between the two plates to one-fifth by placing thin aluminum sheets with an emissivity of \(0.1\) on both sides between the plates. Determine the number of sheets that need to be inserted.

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.

A 5-m-diameter spherical furnace contains a mixture of \(\mathrm{CO}_{2}\) and \(\mathrm{N}_{2}\) gases at \(1200 \mathrm{~K}\) and \(1 \mathrm{~atm}\). The mole fraction of \(\mathrm{CO}_{2}\) in the mixture is \(0.15\). If the furnace wall is black and its temperature is to be maintained at \(600 \mathrm{~K}\), determine the net rate of radiation heat transfer between the gas mixture and the furnace walls.

A large number of long tubes, each of diameter \(D\), are placed parallel to each other and at a center-to-center distance of s. Since all of the tubes are geometrically similar and at the same temperature, these could be treated collectively as one surface \(\left(A_{j}\right)\) for radiation heat transfer calculations. As shown in Fig. P13-140, the tube bank \(\left(A_{j}\right)\) is placed opposite a large flat wall \(\left(A_{j}\right)\) such that the tube bank is parallel to the wall. (a) Calculate the view factors \(F_{i j}\) and \(F_{j i}\) for $s=3.0 \mathrm{~cm}\( and \)D=1.5 \mathrm{~cm}$. (b) Calculate the net rate of radiation heat transfer between the wall and the tube bank per unit area of the wall when $T_{i}=900^{\circ} \mathrm{C}, T_{j}=60^{\circ} \mathrm{C}, \varepsilon_{i}=0.8\(, and \)\varepsilon_{j}=0.9$. (c) A fluid flows through the tubes at an average temperature of $40^{\circ} \mathrm{C}\(, resulting in a heat transfer coefficient of \)2.0 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\(. Assuming \)T_{i}=900^{\circ} \mathrm{C}, \varepsilon_{i}=0.8\( and \)\varepsilon_{j}=0.9$ (as above) and neglecting the tube wall thickness and convection from the outer surface, calculate the temperature of the tube surface in steady operation.

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

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