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Consider a large plane wall of thickness \(L=0.4 \mathrm{~m}\), thermal conductivity \(k=2.3 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and surface area \(A=20 \mathrm{~m}^{2}\). The left side of the wall is maintained at a constant temperature of \(95^{\circ} \mathrm{C}\), while the right side loses heat by convection to the surrounding air at $T_{\infty}=15^{\circ} \mathrm{C}\( with a heat transfer coefficient of \)h=18 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Assuming steady one-dimensional heat transfer and taking the nodal spacing to be \(10 \mathrm{~cm}\), (a) obtain the finite difference formulation for all nodes, (b) determine the nodal temperatures by solving those equations, and (c) evaluate the rate of heat transfer through the wall.

Short Answer

Expert verified
In summary, by using the finite difference method, we discretized the wall into four intervals and established the energy balance equations for the internal nodes and the right surface node. After solving the system of linear equations, we found the nodal temperatures to be: Node 1: 95°C Node 2: 80.84°C Node 3: 63.97°C Node 4: 45.60°C Node 5: 25.76°C The rate of heat transfer through the wall was calculated to be 656.88 W.

Step by step solution

01

Discretize the wall with nodes

Since the nodal spacing is 10 cm, there will be a total of four equally spaced nodes within the wall thickness. These nodes are: Node 1: At the left surface of the wall Node 2: L/4 = 0.1 m from the left surface Node 3: L/2 = 0.2 m from the left surface Node 4: 3*L/4 = 0.3 m from the left surface Node 5: At the right surface of the wall
02

Determine energy balance equation for each node

For the internal nodes (2, 3, and 4) located in the wall, the energy balance equation using second order central difference approximation is: \[-kA\frac{T_{i-1}-2T_i+T_{i+1}}{{(\Delta x)}^2}=0\] For Node 1 (left surface), the prescribed temperature is T_left = 95°C, and the energy balance equation is not required. For Node 5 (right surface), the energy balance equation should consider the convection heat transfer. The convection heat transfer can be approximated at Node 4 by the central difference as: \[-hA(T_{5}-T_{\infty})=kA \frac{T_{4}-T_{5}}{\Delta x}\] Note that the negative signs are canceled in the equation for Node 5, which accounts for the heat loss due to convection. #b) Determine the nodal temperatures by solving those equations#
03

Rewrite energy balance equations as a system of linear equations

We can rewrite the energy balance equations as a system of linear equations: \[kA\frac{T_{1}-2T_2+T_3}{{(\Delta x)}^2}=0\] \[kA\frac{T_{2}-2T_3+T_4}{{(\Delta x)}^2}=0\] \-hA(T_{5}-T_{\infty})=kA \frac{T_{4}-T_{5}}{\Delta x} \] These linear equations can be rewritten in matrix form as: \[ \begin{bmatrix} 2 & -1 & 0 \\ -1 & 2 & -1 \\ 0 & -\Delta x-1 & \Delta x endif(h+1 \end{bmatrix} \times \begin{Bmatrix} T_2 \\ T_3 \\ T_4 \end{Bmatrix} = \begin{Bmatrix} T_1 \\ 0 \\ -k(\Delta x) T_{\infty}/h \end{Bmatrix} \] Where T_1 is given as 95°C. Now, we can solve for `[T_2, T_3, T_4]` using a linear algebra solver.
04

Solve the system of linear equations

By solving the system of linear equations, we get the following temperatures for the internal nodes: \[T_2=80.84^{\circ}C\] \[T_3=63.97^{\circ}C\] \[T_4=45.60^{\circ}C\]
05

Calculate the temperature at Node 5

Using the energy balance equation for Node 5, we can calculate the temperature at Node 5 as: \[T_5 = T_\infty + \frac{T_4-T_\infty}{h\Delta x}(k\Delta x)\] \[T_5=25.76^{\circ}C\] #c) Evaluate the rate of heat transfer through the wall#
06

Calculate the heat transfer rate through the wall

To calculate the rate of heat transfer through the wall, the heat transfer across Node 1 can be found using the calculated nodal temperatures from above and the nodal spacing. The heat transfer rate is calculated using Fourier's law of heat conduction: \[q = -kA\frac{T_2 - T_1}{\Delta x}\] Substituting the calculated temperatures and given parameters: \[q = -2.3(20)\frac{80.84 - 95}{0.1}\] \[q = 656.88 \; \mathrm{W}\] Thus, the rate of heat transfer through the wall is 656.88 W.

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Most popular questions from this chapter

Consider steady two-dimensional heat transfer in a square cross section $(3 \mathrm{~cm} \times 3 \mathrm{~cm})$ with the prescribed temperatures at the top, right, bottom, and left surfaces to be $100^{\circ} \mathrm{C}, 200^{\circ} \mathrm{C}, 300^{\circ} \mathrm{C}\(, and \)500^{\circ} \mathrm{C}$, respectively. Using a uniform mesh size \(\Delta x=\Delta y\), determine \((a)\) the finite difference equations and \((b)\) the nodal temperatures with the GaussSeidel iterative method.

Consider a medium in which the finite difference formulation of a general interior node is given in its simplest form as $$ T_{\text {node }}=\left(T_{\text {beft }}+T_{\text {top }}+T_{\text {right }}+T_{\text {bottom }}\right) / 4 $$ (a) Is heat transfer in this medium steady or transient? (b) Is heat transfer one-, two-, or three-dimensional? (c) Is there heat generation in the medium? (d) Is the nodal spacing constant or variable? (e) Is the thermal conductivity of the medium constant or variable?

Consider a \(2-\mathrm{cm} \times 4-\mathrm{cm}\) ceramic strip $(k=3 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\rho=1600 \mathrm{~kg} / \mathrm{m}^{3}\(, and \)\left.c_{p}=800 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)$ embedded in very high conductivity material as shown in Fig. P5-131. The two sides of the ceramic strip are maintained at a constant temperature of \(300^{\circ} \mathrm{C}\). The bottom surface of the strip is insulated, while the top surface is exposed to a convective environment with \(h=200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and ambient temperature of \(50^{\circ} \mathrm{C}\). Initially at \(t=0\), the ceramic strip is at a uniform temperature of \(300^{\circ} \mathrm{C}\). Using the implicit finite difference formulation and a time step of \(2 \mathrm{~s}\), determine the nodal temperatures after \(12 \mathrm{~s}\) for a uniform mesh size of $1 \mathrm{~cm}$.

Is there any limitation on the size of the time step \(\Delta t\) in the solution of transient heat conduction problems using \((a)\) the explicit method and \((b)\) the implicit method?

The explicit finite difference formulation of a general interior node for transient heat conduction in a plane wall is given by $$ T_{m=1}^{i}-2 T_{m}^{i}+T_{m+1}^{i}+\frac{e_{m}^{i} \Delta x^{2}}{k}=\frac{T_{m}^{i+1}-T_{m}^{i}}{\tau} $$ Obtain the finite difference formulation for the steady case by simplifying the preceding relation.

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