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The roof of a house consists of a \(15-\mathrm{cm}\)-thick concrete slab \(\left(k=1.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.\) and \(\left.\alpha=0.69 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\right)\) that is \(18 \mathrm{~m}\) wide and \(32 \mathrm{~m}\) long. One evening at $6 \mathrm{p} . \mathrm{m}$., the slab is observed to be at a uniform temperature of \(18^{\circ} \mathrm{C}\). The average ambient air and the night sky temperatures for the entire night are predicted to be \(6^{\circ} \mathrm{C}\) and \(260 \mathrm{~K}\), respectively. The convection heat transfer coefficients at the inner and outer surfaces of the roof can be taken to be $h_{i}=5 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\( and \)h_{o}=12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. The house and the interior surfaces of the walls and the floor are maintained at a constant temperature of \(20^{\circ} \mathrm{C}\) during the night, and the emissivity of both surfaces of the concrete roof is \(0.9\). Considering both radiation and convection heat transfers and using the explicit finite difference method with a time step of \(\Delta t=5 \mathrm{~min}\) and a mesh size of $\Delta x=3 \mathrm{~cm}$, determine the temperatures of the inner and outer surfaces of the roof at 6 a.m. Also, determine the average rate of heat transfer through the roof during that night.

Short Answer

Expert verified
Answer: To find the temperatures of the inner and outer surfaces of the roof at 6 a.m., you will need to apply the explicit finite difference method using the provided equations and initial temperature conditions. After performing 144 time steps, you will find the temperatures of the inner and outer surfaces as \(T_{inner}= T^{144}_5\) and \(T_{outer}= T^{144}_0\). To calculate the average rate of heat transfer through the roof during the night, use the Fourier law for heat conduction at the inner surface and divide the result by the total time of 12 hours to find \(Q\).

Step by step solution

01

List given information and variables

Concrete slab thickness: \(d=15 cm=0.15 m\) Thermal conductivity of concrete: \(k=1.4 W/m \cdot K\) Thermal diffusivity of concrete: \(\alpha=0.69\times10^{-6} m^2/s\) Width: \(W=18m\) Length: \(L=32m\) Initial temperature of slab: \(T_i=18^{\circ}C\) Temperature inside the house: \(T_{house}=20^{\circ}C\) Air temperature: \(T_{air}=6^{\circ}C\) Night sky temperature: \(T_{sky}=260K\) Convection heat transfer coefficient: \(h_{i}=5 W/m^2 \cdot K\) \(h_{o}=12 W/m^2 \cdot K\) Emissivity: \(\epsilon = 0.9\) Time step: \(\Delta t=5 \, \text{min}= 300 \, s\) Mesh size: \(\Delta x=3 cm=0.03 m\)
02

Calculate the time steps and number of meshes

To calculate the temperatures at 6 a.m., we need the total amount of time steps: Number of hours: 12 hours Total time steps: \((12*3600)/300=144\) time steps We also need to calculate the number of meshes inside the concrete slab: Number of meshes: \(d/\Delta x = 0.15/0.03 = 5\)
03

Set up the explicit finite difference method equations

We will need to set up the equations for the explicit finite difference method to calculate the temperature distribution inside the concrete slab. For the internal nodes (\(1\leq i\leq 4\)), the equation is: \(T^{n+1}_{i} = T^{n}_{i} + \frac{\alpha \Delta t}{(\Delta x)^2}\left(T^{n}_{i+1} - 2T^{n}_{i} + T^{n}_{i-1}\right)\) For \(i = 0\) (outer surface node): \(T^{n+1}_{0} = T^n_{0} + \frac{\alpha\Delta t}{(\Delta x)^2}(T^n_{1} - T^n_{0}) + \frac{2 \alpha\Delta t}{\Delta x}\left(\frac{h_o(T_{air} - T^n_{0}) + \epsilon \sigma (T_{sky}^4 - (T^n_{0}+273.15)^4)}{k}\right)\) For \(i = 5\) (inner surface node): \(T^{n+1}_{5} = T^n_{5} + \frac{\alpha\Delta t}{(\Delta x)^2}(T^n_{4} - T^n_{5}) + \frac{2 \alpha\Delta t}{\Delta x}\left(\frac{h_i(T_{house} - T^n_{5})}{k}\right)\)
04

Calculate the temperature distribution

Using the equations from Step 3, perform calculations for 144 time steps given the initial \(T_i\) for each mesh. Apply the method to update the node temperatures at each time step.
05

Temperatures of inner and outer surfaces at 6 a.m.

After performing calculations for the 144 time steps, determine the temperatures of inner and outer surfaces of the concrete roof: \(T_{inner}= T^{144}_5\) \(T_{outer}= T^{144}_0\)
06

Calculate the average rate of heat transfer

To determine the average rate of heat transfer through the roof during the entire night (12 hours), we will use the Fourier law for heat conduction at the inner surface: $$q = k A\frac{\Delta T}{d}$$ where \(A = WL\) is the area of the roof, and \(\Delta T = T_{inner} - T_{outer}\). Now we can find the average rate of heat transfer through the roof: \(Q = \frac{q}{(12 \,\text{hours} \cdot 3600 \,\text{s/hour})}\). The final results are the temperatures of the inner and outer surfaces of the roof at 6 a.m. and the average rate of heat transfer through the roof during the night.

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Most popular questions from this chapter

The implicit method is unconditionally stable and thus any value of time step \(\Delta t\) can be used in the solution of transient heat conduction problems. To minimize the computation time, someone suggests using a very large value of \(\Delta t\) since there is no danger of instability. Do you agree with this suggestion? Explain.

Consider transient heat conduction in a plane wall whose left surface (node 0 ) is maintained at \(80^{\circ} \mathrm{C}\) while the right surface (node 6) is subjected to a solar heat flux of \(600 \mathrm{~W} / \mathrm{m}^{2}\). The wall is initially at a uniform temperature of \(50^{\circ} \mathrm{C}\). Express the explicit finite difference formulation of the boundary nodes 0 and 6 for the case of no heat generation. Also, obtain the finite difference formulation for the total amount of heat transfer at the left boundary during the first three time steps.

Consider a uranium nuclear fuel element $(k=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\rho=19,070 \mathrm{~kg} / \mathrm{m}^{3}\(, and \)\left.c_{p}=116 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( of radius \)10 \mathrm{~cm}$ that experiences a volumetric heat generation at a rate of $4 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$ because of the nuclear fission reaction. The nuclear fuel element initially at a temperature of \(500^{\circ} \mathrm{C}\) is enclosed inside a cladding made of stainless steel material $\left(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=8055 \mathrm{~kg} / \mathrm{m}^{3}\right.\(, and \)\left.c_{p}=480 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( of thickness \)4 \mathrm{~cm}$. The fuel element is cooled by passing pressurized heavy water over the cladding surface. The pressurized water has a bulk temperature of \(50^{\circ} \mathrm{C}\), and the convective heat transfer coefficient is $1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Assuming one-dimensional transient heat conduction in Cartesian coordinates, determine the temperature in the fuel rod and in the cladding after 10,20 , and \(30 \mathrm{~min}\). Use the implicit finite difference formulation with a uniform mesh size of \(2 \mathrm{~cm}\) and a time step of $1 \mathrm{~min}$.

A circular fin of uniform cross section, with diameter of \(10 \mathrm{~mm}\) and length of \(50 \mathrm{~mm}\), is attached to a wall with a surface temperature of \(350^{\circ} \mathrm{C}\). The fin is made of material with thermal conductivity of \(240 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), it is exposed to an ambient air condition of \(25^{\circ} \mathrm{C}\), and the convection heat transfer coefficient is \(250 \mathrm{~W} / \mathrm{m}^{2}\). \(\mathrm{K}\). Assume steady one-dimensional heat transfer along the fin and the nodal spacing to be uniformly \(10 \mathrm{~mm}\). (a) Using the energy balance approach, obtain the finite difference equations to determine the nodal temperatures. (b) Determine the nodal temperatures along the fin by solving those equations, and compare the results with the analytical solution. (c) Calculate the heat transfer rate, and compare the result with the analytical solution.

Consider a 2-m-long and \(0.7-\mathrm{m}\)-wide stainless steel plate whose thickness is \(0.1 \mathrm{~m}\). The left surface of the plate is exposed to a uniform heat flux of \(2000 \mathrm{~W} / \mathrm{m}^{2}\), while the right surface of the plate is exposed to a convective environment at $0^{\circ} \mathrm{C}\( with \)h=400 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The thermal conductivity of the stainless steel plate can be assumed to vary linearly with temperature range as \(k(T)=k_{o}(1+\beta T)\) where $k_{o}=48 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\( and \)\beta=9.21 \times 10^{-4 \circ} \mathrm{C}^{-1}$. The stainless steel plate experiences a uniform volumetric heat generation at a rate of $8 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$. Assuming steady-state one-dimensional heat transfer, determine the temperature distribution along the plate thickness.

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