Two aligned parallel rectangles with dimensions \(6 \mathrm{~m} \times\) \(8 \mathrm{~m}\) are spaced apart by a distance of \(2 \mathrm{~m}\). If the two parallel rectangles are experiencing radiation heat transfer as black surfaces, determine the percentage of change in radiation heat transfer rate when the rectangles are moved \(8 \mathrm{~m}\) apart.

Short Answer

Expert verified
Answer: The percentage change in radiation heat transfer rate when the distance between the rectangles is increased from 2m to 8m is 33.33%.

Step by step solution

01

Calculate the total surface area of both rectangles

To calculate the total surface area of both rectangles, we simply multiply the dimensions of the rectangles: \(A_1 = 6 \cdot 8 = 48 \text{~m}^2\) Since there are two rectangles, the combined surface area is: \(A_{1\&2} = 2 \cdot A_1 = 2 \cdot 48 = 96 \text{~m}^2\)
02

Determine the shape factor between the two rectangles

The shape factor is a dimensionless number that represents the proportion of radiant energy leaving one surface that arrives at the second surface. In this case, the shape factor can be determined through the following formula: \(F_{1 \rightarrow 2} = 1 - \frac{1}{1 + \frac{A_{1\&2}}{A_1} \frac{d}{L_{1 \times 2}}}\) where \(d\) is the distance between rectangles, and \(L_{1 \times 2}\) represents the length of the emitting surface onto the receiving surface.
03

Calculate the radiation heat transfer rate in both cases

The radiation heat transfer rate between two black surfaces can be defined as follows: \(Q = c \cdot A_1 \cdot F_{1 \rightarrow 2} \cdot \Delta Temp\) In this exercise, the temperature difference and the constant \(c\) remain the same, so the only thing affected by the change in distance between rectangles is the shape factor. Thus, we need to calculate the shape factor for both cases. a) When the rectangles are 2m apart: \(d_1 = 2m\) We have: \(F_{1 \rightarrow 2}(2m) = 1 - \frac{1}{1 + \frac{96}{48} \frac{2}{8}} = 1 - \frac{1}{2} = 0.5\) b) When the rectangles are 8m apart: \(d_2 = 8m\) We have: \(F_{1 \rightarrow 2}(8m) = 1 - \frac{1}{1 + \frac{96}{48} \frac{8}{8}} = 1 - \frac{1}{1 + 2} = \frac{2}{3}\) Now, knowing the shape factors for both cases, we can calculate the radiation heat transfer rates. \(Q_1 = c \cdot A_1 \cdot F_{1 \rightarrow 2}(2m) = k \cdot 48 \cdot 0.5\) \(Q_2 = c \cdot A_1 \cdot F_{1 \rightarrow 2}(8m) = k \cdot 48 \cdot \frac{2}{3}\)
04

Determine the percentage change in radiation heat transfer rate

Finally, we can find the percentage change between the two radiation heat transfer rates: \(Percentage\,change = \frac{Q_2 - Q_1}{Q_1} \cdot 100\) \(Percentage\,change = \frac{k \cdot 48 \cdot \frac{2}{3} - k \cdot 48 \cdot 0.5}{k \cdot 48 \cdot 0.5} \cdot 100\) \(Percentage\,change = \frac{\frac{2}{3} - 0.5}{0.5} \cdot 100\) The percentage change in radiation heat transfer rate when the rectangles are moved to 8m apart is: \(Percentage\,change = \frac{1}{3} \cdot 100 = 33.33\%\) Thus, the radiation heat transfer rate increases by 33.33% when the distance between the rectangles is increased from 2m to 8m.

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Most popular questions from this chapter

Consider a hemispherical furnace with a flat circular base of diameter \(D\). Determine the view factor from the dome of this furnace to its base.

A 2-m-internal-diameter double-walled spherical tank is used to store iced water at \(0^{\circ} \mathrm{C}\). Each wall is \(0.5 \mathrm{~cm}\) thick, and the \(1.5\)-cm-thick air space between the two walls of the tank is evacuated in order to minimize heat transfer. The surfaces surrounding the evacuated space are polished so that each surface has an emissivity of \(0.15\). The temperature of the outer wall of the tank is measured to be \(20^{\circ} \mathrm{C}\). Assuming the inner wall of the steel tank to be at \(0^{\circ} \mathrm{C}\), determine \((a)\) the rate of heat transfer to the iced water in the tank and \((b)\) the amount of ice at \(0^{\circ} \mathrm{C}\) that melts during a 24-h period.

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 \(900 \mathrm{~K}\), respectively. If the view factor from the base surface to the top surface is \(0.2\), the net radiation heat transfer from the bottom surface is (a) \(-93.6 \mathrm{~kW}\) (b) \(-86.1 \mathrm{~kW}\) (c) \(0 \mathrm{~kW}\) (d) \(86.1 \mathrm{~kW}\) (e) \(93.6 \mathrm{~kW}\)

The base surface of a cubical furnace with a side length of \(3 \mathrm{~m}\) has an emissivity of \(0.80\) and is maintained at \(500 \mathrm{~K}\). If the top and side surfaces also have an emissivity of \(0.80\) and are maintained at \(900 \mathrm{~K}\), the net rate of radiation heat transfer from the top and side surfaces to the bottom surface is (a) \(194 \mathrm{~kW}\) (b) \(233 \mathrm{~kW}\) (c) \(288 \mathrm{~kW}\) (d) \(312 \mathrm{~kW}\) (e) \(242 \mathrm{~kW}\)

13-144 In a natural-gas fired boiler, combustion gases pass through 6-m-long 15 -cm-diameter tubes immersed in water at 1 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 atm and \(1200 \mathrm{~K}\) 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.

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