Consider a cubical furnace with a side length of \(3 \mathrm{~m}\). The top surface is maintained at \(700 \mathrm{~K}\). The base surface has an emissivity of \(0.90\) and is maintained at \(950 \mathrm{~K}\). The side surface is black and is maintained at \(450 \mathrm{~K}\). Heat is supplied from the base surface at a rate of \(340 \mathrm{~kW}\). Determine the emissivity of the top surface and the net rates of heat transfer between the top and the bottom surfaces, and between the bottom and side surfaces.

Short Answer

Expert verified
Answer: To determine the emissivity of the top surface and the net rates of heat transfer between the surfaces, follow the steps provided in the solution. The four steps are: 1. Calculate area and radiosity for each surface. 2. Calculate net radiative heat transfer between surfaces. 3. Find emissivity for the top surface. 4. Find net rates of heat transfer. By following these steps, we will be able to determine the required values for the emissivity of the top surface and the net rates of heat transfer between the top and bottom surfaces, and between the bottom and side surfaces of the cubical furnace.

Step by step solution

01

First, we need to calculate the area, \(A\), of each surface of the cubical furnace: \(A = \text{side length} \times \text{side length} = 3\text{m} \times 3\text{m} = 9\text{ m}^2\). Next, let's calculate the radiosity, \(J_i\), for each surface using the Stefan-Boltzmann Law (\(J_i = \varepsilon_i \sigma T_i^4 + \rho_i \sigma T_{surroundings}^4\)) and the given temperatures, where \(\varepsilon_i\) is the emissivity of the surface, \(\rho_i\) is the reflectivity of the surface (\(\rho_i = 1 - \varepsilon_i\)), \(\sigma\) is the Stefan-Boltzmann constant (\(5.67 \times 10^{-8} \text{W/m}^2\text{K}^4\)), and \(T_i\) is the temperature in Kelvin: Top surface: \(J_1 = \varepsilon_1 \sigma T_1^4 + \rho_1 \sigma T_{surroundings}^4\) Base surface: \(J_2 = \varepsilon_2 \sigma T_2^4 + \rho_2 \sigma T_{surroundings}^4\) Side surface: Since it's black, the emissivity is \(1\), and we can use the simpler Stefan-Boltzmann Law: \(J_3 = \sigma T_3^4\) #Step 2: Calculating net radiative heat transfer between surfaces#

Now we will calculate the net radiative heat transfer between the surfaces, using the formula \(q_{net} = A F_{i \rightarrow j}(J_i - J_j)\), where \(F_{i \rightarrow j}\) represents the view factor between surfaces \(i\) and \(j\) and \(q_{net}\) is the net radiative heat transfer between the two surfaces: Top and base surfaces: \(q_{net, 1 \rightarrow 2} = A F_{1 \rightarrow 2}(J_1 - J_2)\) Within a cube, the surface to surface view factor is \(1/4\) which can be used to calculate the net radiative heat transfer: Bottom and side surfaces: \(q_{net, 2 \rightarrow 3} = A F_{2 \rightarrow 3}(J_2 - J_3)\) #Step 3: Finding emissivity for the top surface#
02

We are given that the heat supplied from the base surface is \(340 \text{ kW}\). This heat is transferred from the base surface to the top and side surfaces. Therefore, the net radiative heat transfer from the base surface should be equal to the heat supplied: \(q_{net, 1 \rightarrow 2} + q_{net, 2 \rightarrow 3} = 340000\text{ W}\) or equivalently: \(A F_{1 \rightarrow 2}(J_1 - J_2) + A F_{2 \rightarrow 3}(J_2 - J_3) = 340000\text{ W}\) Using the known values and solving this equation for the unknown variable, \(\varepsilon_1\), we obtain the emissivity of the top surface. #Step 4: Finding net rates of heat transfer#

Finally, we use the obtained emissivity value for the top surface, and the known values for the base and side surfaces, to calculate the net radiative heat transfer rates between the top and bottom surfaces, and between the bottom and side surfaces: \(q_{net, 1 \rightarrow 2} = A F_{1 \rightarrow 2}(J_1 - J_2)\) \(q_{net, 2 \rightarrow 3} = A F_{2 \rightarrow 3}(J_2 - J_3)\)

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Most popular questions from this chapter

This experiment is conducted to determine the emissivity of a certain material. A long cylindrical rod of diameter \(D_{1}=0.01 \mathrm{~m}\) is coated with this new material and is placed in an evacuated long cylindrical enclosure of diameter \(D_{2}=0.1 \mathrm{~m}\) and emissivity \(\varepsilon_{2}=0.95\), which is cooled externally and maintained at a temperature of \(200 \mathrm{~K}\) at all times. The rod is heated by passing electric current through it. When steady operating conditions are reached, it is observed that the rod is dissipating electric power at a rate of \(8 \mathrm{~W}\) per unit of its length and its surface temperature is \(500 \mathrm{~K}\). Based on these measurements, determine the emissivity of the coating on the rod.

A vertical 2-m-high and 5-m-wide double-pane window consists of two sheets of glass separated by a 3 -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 thermocouple shielded by aluminum foil of emissivity \(0.15\) is used to measure the temperature of hot gases flowing in a duct whose walls are maintained at \(T_{w}=380 \mathrm{~K}\). The thermometer shows a temperature reading of \(T_{\text {th }}=530 \mathrm{~K}\). Assuming the emissivity of the thermocouple junction to be \(\varepsilon=0.7\) and the convection heat transfer coefficient to be \(h=120 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the actual temperature of the gas. What would the thermometer reading be if no radiation shield was used?

13-59 This question deals with steady-state radiation heat transfer between a sphere \(\left(r_{1}=30 \mathrm{~cm}\right)\) and a circular disk \(\left(r_{2}=120 \mathrm{~cm}\right)\), which are separated by a center-to- center distance \(h=60 \mathrm{~cm}\). When the normal to the center of disk passes through the center of the sphere, the radiation view factor is given by $$ F_{12}=0.5\left\\{1-\left[1+\left(\frac{r_{2}}{h}\right)^{2}\right]^{-0.5}\right\\} $$ Surface temperatures of the sphere and the disk are \(600^{\circ} \mathrm{C}\) and \(200^{\circ} \mathrm{C}\), respectively; and their emissivities are \(0.9\) and \(0.5\), respectively. (a) Calculate the view factors \(F_{12}\) and \(F_{21}\). (b) Calculate the net rate of radiation heat exchange between the sphere and the disk. (c) For the given radii and temperatures of the sphere and the disk, the following four possible modifications could increase the net rate of radiation heat exchange: paint each of the two surfaces to alter their emissivities, adjust the distance between them, and provide an (refractory) enclosure. Calculate the net rate of radiation heat exchange between the two bodies if the best values are selected for each of the above modifications.

A cylindrical container whose height and diameter are \(8 \mathrm{~m}\) is filled with a mixture of \(\mathrm{CO}_{2}\) and \(\mathrm{N}_{2}\) gases at \(600 \mathrm{~K}\) and \(1 \mathrm{~atm}\). The partial pressure of \(\mathrm{CO}_{2}\) in the mixture is \(0.15 \mathrm{~atm}\). If the walls are black at a temperature of \(450 \mathrm{~K}\), determine the rate of radiation heat transfer between the gas and the container walls.

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