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Two black parallel rectangles with dimensions $3 \mathrm{ft} \times 5 \mathrm{ft}\( are spaced apart by a distance of \)1 \mathrm{ft}$. The two parallel rectangles are experiencing radiation heat transfer as black surfaces, where the top rectangle receives a total of 180,000 $\mathrm{Btu} / \mathrm{h}$ radiation heat transfer rate from the bottom rectangle. If the top rectangle has a uniform temperature of \(60^{\circ} \mathrm{F}\), determine the temperature of the bottom rectangle.

Short Answer

Expert verified
Answer: The temperature of the bottom rectangle is approximately \(125.88^\circ F\).

Step by step solution

01

Define the Stefan-Boltzmann Law for Radiating Surfaces

The Stefan-Boltzmann Law states that the radiation heat transfer rate between two black surfaces depends on their temperatures (\({T_1}\) and \({T_2}\)) and their emissivities (ε). In our case, both surfaces have an emissivity of 1 since they are black. The equation for the radiation heat transfer rate (Q) between two surfaces is given by: $$ Q = A \sigma (T_1^4 - T_2^4) $$ where A is the surface area of one rectangle, \(\sigma\) is the Stefan-Boltzmann constant (\(5.67 × 10^{-8} \mathrm{W} / \mathrm{m}^2 \mathrm{K}^4\)), and \(T_1\) and \(T_2\) are the absolute temperatures of the surfaces in Kelvin.
02

Convert Provided Temperature to Kelvin

We are given the temperature of the top rectangle in Fahrenheit. Convert the temperature to Kelvin and store it as \(T_1\): $$ T_{1(K)} = \frac{5}{9}(T_{1(°F)} - 32) + 273.15 $$ $$ T_{1(K)} = \frac{5}{9}(60 °F - 32) + 273.15 = 288.71 K $$ Note that \(T_{1}\) (top rectangle temperature) is provided in degrees Fahrenheit, which must be converted to Kelvin to be used in the Stefan-Boltzmann equation.
03

Convert the Radiation Heat Transfer Rate to \(\mathrm{W}\)

The radiation heat transfer rate (Q) between the rectangles is given in \(\mathrm{Btu/h}\). We need to convert this value to the SI unit of Watts (W) to use in our calculations: $$ Q_{(W)} = Q_{(\mathrm{Btu/h})} \times \frac{1055.06\, \mathrm{J}}{1\, \mathrm{Btu}} \times \frac{1\, \mathrm{h}}{3600\, \mathrm{s}} $$ $$ Q_{(W)} = 180,000\, \mathrm{Btu/h} \times \frac{1055.06\, \mathrm{J}}{1\, \mathrm{Btu}} \times \frac{1\, \mathrm{h}}{3600\, \mathrm{s}} = 52981.7\, \mathrm{W} $$
04

Calculate the Surface Area of One Rectangle

The dimensions of each rectangle are given in feet, but we need to use the SI unit of meters (m) in our calculations. Convert the dimensions to meters and calculate the surface area (A): $$ 3\, \mathrm{ft} \times 5\, \mathrm{ft} \times \frac{1\, \mathrm{m}}{3.28084\, \mathrm{ft}} \times \frac{1\, \mathrm{m}}{3.28084\, \mathrm{ft}} = 0.929\, \mathrm{m}^{2} $$
05

Determine the Temperature of the Bottom Rectangle

Plug in the known values (Q, A, \(\sigma\), and \(T_1\)) into the Stefan-Boltzmann equation and solve for \(T_2\): $$ 52981.7\, \mathrm{W} = 0.929\, \mathrm{m}^2 (5.67 \times 10^{-8} \mathrm{W} / \mathrm{m}^2 \mathrm{K}^4)(T_2^4 - 288.71^4\, \mathrm{K}^4) $$ Solve for \(T_2^4\) : $$ T_2^4 = \frac{52981.7\, \mathrm{W} + 0.929 \, \mathrm{m}^2 (5.67 \times 10^{-8} \mathrm{W} / \mathrm{m}^2 \mathrm{K}^4)(288.71^4 \, \mathrm{K}^4)}{0.929\, \mathrm{m}^2(5.67 \times 10^{-8} \mathrm{W} / \mathrm{m}^2 \mathrm{K}^4)} $$ $$ T_2^4 = 123116.55 $$ Now, take the fourth root to find \(T_2\) : $$ T_2 = \sqrt[4]{123116.55} = 326.84\, \mathrm{K} $$
06

Convert the Bottom Rectangle Temperature Back to Fahrenheit

Finally, convert the bottom rectangle's temperature from Kelvin to Fahrenheit: $$ T_{2(°F)} = \frac{9}{5}(T_{2(K)} - 273.15) + 32 $$ $$ T_{2(°F)} = \frac{9}{5}(326.84\, \mathrm{K} - 273.15) + 32 = 125.88^{\circ} \mathrm{F} $$ The temperature of the bottom rectangle is approximately \(125.88^\circ F\).

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Most popular questions from this chapter

Consider an equimolar mixture of \(\mathrm{CO}_{2}\) and \(\mathrm{O}_{2}\) gases at \(800 \mathrm{~K}\) and a total pressure of \(0.5 \mathrm{~atm}\). For a path length of \(1.2 \mathrm{~m}\), determine the emissivity of the gas.

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.

Two thin radiation shields with emissivities of \(\varepsilon_{3}=0.10\) and \(\varepsilon_{4}=0.15\) on both sides are placed between two very large parallel plates, which are maintained at uniform temperatures $T_{1}=600 \mathrm{~K}\( and \)T_{2}=300 \mathrm{~K}$ and have emissivities \(\varepsilon_{1}=0.6\) and \(\varepsilon_{2}=0.7\), respectively (Fig. P13-103). Determine the net rates of radiation heat transfer between the two plates with and without the shields per unit surface area of the plates, and the temperatures of the radiation shields in steady operation.

Consider a \(4-\mathrm{m} \times 4-\mathrm{m} \times 4-\mathrm{m}\) cubical furnace whose floor and ceiling are black and whose side surfaces are reradiating. The floor and the ceiling of the furnace are maintained at temperatures of \(550 \mathrm{~K}\) and \(1100 \mathrm{~K}\), respectively. Determine the net rate of radiation heat transfer between the floor and the ceiling of the furnace.

Two parallel disks of diameter \(D=0.6 \mathrm{~m}\) separated by $L=0.4 \mathrm{~m}$ are located directly on top of each other. Both disks are black and are maintained at a temperature of \(450 \mathrm{~K}\). The back sides of the disks are insulated, and the environment that the disks are in can be considered to be blackbodies at \(300 \mathrm{~K}\). Determine the net rate of radiation heat transfer from the disks to the environment. Answer: $781 \mathrm{~W}$

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