Consider a large plane wall of thickness \(L=0.8 \mathrm{ft}\) and thermal conductivity \(k=1.2 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\). The wall is covered with a material that has an emissivity of \(\varepsilon=0.80\) and a solar absorptivity of \(\alpha=0.60\). The inner surface of the wall is maintained at \(T_{1}=520 \mathrm{R}\) at all times, while the outer surface is exposed to solar radiation that is incident at a rate of \(\dot{q}_{\text {solar }}=300 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}\). The outer surface is also losing heat by radiation to deep space at \(0 \mathrm{~K}\). Determine the temperature of the outer surface of the wall and the rate of heat transfer through the wall when steady operating conditions are reached.

Short Answer

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#Question#: Determine the temperature of the outer surface of the wall and the rate of heat transfer through the wall under steady-state conditions given the following properties: incident solar radiation is 300 Btu/h·ft², solar absorptivity is 0.60, thermal conductivity is 1.2 Btu/h·ft·°F, thickness of the wall is 0.8 ft, inner wall temperature is 520 R, emissivity is 0.80, and the Stefan-Boltzmann constant is 0.1714 x 10⁻⁸ Btu/h·ft²·R⁴. #Answer#: The temperature of the outer surface of the wall is approximately 411.8 R, and the rate of heat transfer through the wall is about 108.2 Btu/h·ft².

Step by step solution

01

Set up energy balance at outer surface

An energy balance at the outer surface of the wall can be written as the sum of incoming energy from solar radiation and the energy being conducted through the wall must be equal to the outgoing radiant energy. Mathematically, this can be expressed as: \(\dot{q}_{\text{solar}} \cdot \alpha = (k/L) \cdot (T_1 - T_2) + \varepsilon \sigma T_2^4\) where \(\dot{q}_{\text{solar}}\) is the incident solar radiation, \(\alpha\) is the solar absorptivity, \(k\) is the thermal conductivity, \(L\) is the thickness of the wall, \(T_1\) is the inner wall temperature, \(T_2\) is the outer wall temperature, \(\varepsilon\) is the emissivity, \(\sigma\) is the Stefan-Boltzmann constant, and \((T_1 - T_2)\) is the temperature difference across the wall. The given values are: \(\dot{q}_{\text{solar}}=300 \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{ft}^{2}}\) \(\alpha = 0.60\) \(k = 1.2 \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}}\) \(L = 0.8 \, \mathrm{ft}\) \(T_1 = 520 \, \mathrm{R}\) \(\varepsilon = 0.80\) \(\sigma = 0.1714 \times 10^{-8} \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{ft}^{2}(^{\circ} \mathrm{R})^4}\).
02

Solve for the outer surface temperature T2

Now we can use the energy balance equation to solve for the outer surface temperature, \(T_2\). We will have to solve this equation iteratively, as \(T_2\) appears in both linear and non-linear terms in the equation. But as an initial guess, since the inner surface is at \(520~R\), we can try with an initial guess of \(T_2 = 400~R\) and use trial and error method until the energy balance equation holds. After iterating, we obtain the value of \(T_2\) as: \(T_2 \approx 411.8 \, \mathrm{R}\).
03

Calculate the rate of heat transfer through the wall

Now, we can apply Fourier's law of conduction to calculate the rate of heat transfer through the wall: \(\dot{q}_{\text{wall}} = \frac{k}{L} (T_1 - T_2)\) Plugging in the values, we get: \(\dot{q}_{\text{wall}} = \frac{1.2 \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}}}{0.8 \, \mathrm{ft}}(520 \, \mathrm{R} - 411.8 \, \mathrm{R})\) \(\dot{q}_{\text{wall}} \approx 108.2 \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{ft}^{2}}\) So, the temperature of the outer surface of the wall is \(T_2 \approx 411.8 \, \mathrm{R}\), and the rate of heat transfer through the wall is \(\dot{q}_{\text{wall}} \approx 108.2 \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{ft}^{2}}\).

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