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Consider a \(3-\mathrm{m} \times 3-\mathrm{m} \times 3-\mathrm{m}\) cubical furnace. The base surface of the furnace is black and has a temperature of \(550 \mathrm{~K}\). The radiosities for the top and side surfaces are calculated to be \(7500 \mathrm{~W} / \mathrm{m}^{2}\) and $3200 \mathrm{~W} / \mathrm{m}^{2}$, respectively. The net rate of radiation heat transfer to the bottom surface is (a) \(10 \mathrm{~kW}\) (b) \(54 \mathrm{~kW}\) (c) \(61 \mathrm{~kW}\) (d) \(113 \mathrm{~kW}\) (e) \(248 \mathrm{~kW}\)

Short Answer

Expert verified
(a) 45kW (b) 53kW (c) 61kW (d) 71kW Answer: (c) 61kW

Step by step solution

01

Calculate the surface areas

Cube sides have length 3m. So, we can find the area of the base surface (A_base), the area of the top surface (A_top), and the area of one of the side surfaces (A_side): \(A_{base} = A_{top} = 3 \times 3 = 9 \, \mathrm{m}^{2}\), \(A_{side} = 3 \times 3 = 9 \, \mathrm{m}^{2}\).
02

Calculate heat absorbed by the bottom surface

The heat absorbed by the bottom surface due to its own thermal radiation can be obtained using the Stefan-Boltzmann law. The Stefan-Boltzmann law states that the radiative heat flux is proportional to the fourth power of the absolute temperature, q = σ*T^4, where q is the heat flux, σ is the Stefan-Boltzmann constant \((5.67 × 10^{-8} \, \mathrm{W} \cdot \mathrm{m}^{-2} \cdot \mathrm{K}^{-4})\), and T is the temperature in Kelvin. \(q_{base} = \sigma \times T_{base}^{4} = (5.67 \times 10^{-8} \, \mathrm{W} \cdot \mathrm{m}^{-2} \cdot \mathrm{K}^{-4}) \times (550\, \mathrm{K})^4 = 5076.36 \, \mathrm{W} \cdot \mathrm{m}^{-2}\).
03

Calculate total heat emitted by the top and side surfaces

The sum of heat emitted by the top and side surfaces needs to be calculated. Please note that there are a total of 4 side surfaces. Total heat emitted (Q_out) is the sum of the heat emitted by the top and side surfaces. \(Q_{out} = A_{top} \times q_{top} + 4 \times A_{side} \times q_{side} = (9 \, \mathrm{m}^{2}) \times (7500 \, \mathrm{W} \cdot \mathrm{m}^{-2}) + 4 \times (9 \, \mathrm{m}^{2}) \times (3200 \, \mathrm{W} \cdot \mathrm{m}^{-2}) = 113400 \, \mathrm{W}\).
04

Find net heat transfer rate to the bottom surface

Finally, we need to find the net heat transfer rate to the bottom surface, which is the difference between the heat absorbed by the bottom surface due to its own thermal radiation, and the heat emitted by the top and side surfaces: Q_net = - (A_base × q_base - Q_out) = - (9m² × 5076.36W/m² - 113400W) = - (45486.24W - 113400W) = 67913.76W = 67.91kW. The closest answer to the result we calculated is (c) 61kW. The net rate of radiation heat transfer to the bottom surface is approximately 61kW.

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Most popular questions from this chapter

In a natural gas-fired boiler, combustion gases pass through 6-m-long,15-cm- diameter tubes immersed in water at \(1 \mathrm{~atm}\) pressure. The tube temperature is measured to be \(105^{\circ} \mathrm{C}\), and the emissivity of the inner surfaces of the tubes is estimated to be \(0.9\). Combustion gases enter the tube at \(1 \mathrm{~atm}\) and \(1000 \mathrm{~K}\) at a mean velocity of \(3 \mathrm{~m} / \mathrm{s}\). The mole fractions of \(\mathrm{CO}_{2}\) and \(\mathrm{H}_{2} \mathrm{O}\) in combustion gases are 8 percent and 16 percent, respectively. Assuming fully developed flow and using properties of air for combustion gases, determine \((a)\) the rates of heat transfer by convection and by radiation from the combustion gases to the tube wall and \((b)\) the rate of evaporation of water.

Air is flowing between two infinitely large parallel plates. The upper plate is at \(500 \mathrm{~K}\) and has an emissivity of \(0.7\), while the lower plate is a black surface with temperature at \(330 \mathrm{~K}\). If the air temperature is \(290 \mathrm{~K}\), determine the convection heat transfer coefficient associated with the air.

Consider a gray and opaque surface at \(0^{\circ} \mathrm{C}\) in an environment at \(25^{\circ} \mathrm{C}\). The surface has an emissivity of \(0.8\). If the radiation incident on the surface is \(240 \mathrm{~W} / \mathrm{m}^{2}\), the radiosity of the surface is (a) \(38 \mathrm{~W} / \mathrm{m}^{2}\) (b) \(132 \mathrm{~W} / \mathrm{m}^{2}\) (c) \(240 \mathrm{~W} / \mathrm{m}^{2}\) (d) \(300 \mathrm{~W} / \mathrm{m}^{2}\) (e) \(315 \mathrm{~W} / \mathrm{m}^{2}\)

A furnace is of cylindrical shape with a diameter of \(1.2 \mathrm{~m}\) and a length of \(1.2 \mathrm{~m}\). The top surface has an emissivity of \(0.60\) and is maintained at \(450 \mathrm{~K}\). The bottom surface has an emissivity of \(0.50\) and is maintained at \(800 \mathrm{~K}\). The side surface has an emissivity of \(0.40\). Heat is supplied from the base surface at a net rate of \(1400 \mathrm{~W}\). Determine the temperature of the side surface and the net rates of heat transfer between the top and the bottom surfaces and between the bottom and side surfaces.

A large ASTM B152 copper plate is placed in parallel near a large ceramic plate. The ceramic plate is at a temperature of \(520^{\circ} \mathrm{C}\). The copper and ceramic plates have emissivity values of \(0.15\) and \(0.92\), respectively. For the ASTM B152 copper plate, the ASME Code for Process Piping specifies the maximum use temperature at \(260^{\circ} \mathrm{C}\) (ASME B31.3-2014, Table A-1M). If the net radiation heat flux between the two parallel plates is \(2000 \mathrm{~W} / \mathrm{m}^{2}\), determine whether the ASTM B 152 copper plate would comply with the ASME code.

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