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Consider transient heat conduction in a plane wall with variable heat generation and constant thermal conductivity. The nodal network of the medium consists of nodes 0,1 , \(2,3,4\), and 5 with a uniform nodal spacing of $\Delta x$. The wall is initially at a specified temperature. Using the energy balance approach, obtain the explicit finite difference formulation of the boundary nodes for the case of insulation at the left boundary (node 0 ) and radiation at the right boundary (node 5) with an emissivity of \(\varepsilon\) and surrounding temperature of \(T_{\text {surr }}\)

Short Answer

Expert verified
The explicit finite difference formulation for transient heat conduction in this scenario involves discretizing the energy balance equation using the finite difference method, with the following equations for each node: \begin{equation} \frac{T_i^{n+1} - T_i^n}{\Delta t} = \alpha \frac{T_{i+1}^n - 2 T_i^n + T_{i-1}^n}{(\Delta x)^2} + Q_i^n \end{equation} For the boundary nodes, we have: Node 0 (Left boundary, insulation): \begin{equation} T_1^n = T_{-1}^n \end{equation} Node 5 (Right boundary, radiation): \begin{equation} k \frac{T_5^n - T_4^n}{\Delta x} = \varepsilon\sigma\left({T_5^n}^4 - {T_{\text{surr}}}^4\right) \end{equation}

Step by step solution

01

Set up the energy balance equation

The energy balance equation for heat conduction in a plane wall with variable heat generation and constant thermal conductivity can be written as: \begin{equation} \frac{\partial T}{\partial t} = \alpha \frac{\partial^2 T}{\partial x^2} + Q \end{equation} where \(T\) is the temperature, \(t\) is the time, \(\alpha\) is the thermal diffusivity, and \(Q\) is the heat generation term.
02

Discretize the equation using finite difference

We can discretize the energy balance equation using the finite difference method with uniform nodal spacing of \(\Delta x\). The explicit finite difference equation for node \(i\) is given by: \begin{equation} \frac{T_i^{n+1} - T_i^n}{\Delta t} = \alpha \frac{T_{i+1}^n - 2 T_i^n + T_{i-1}^n}{(\Delta x)^2} + Q_i^n \end{equation} where \(T_i^n\) represents the temperature at node \(i\) at time step \(n\), and \(\Delta t\) is the time step.
03

Apply the boundary conditions

We have insulation at the left boundary (node 0) and radiation at the right boundary (node 5) with an emissivity \(\varepsilon\) and surrounding temperature \(T_{\text{surr}}\). For the left boundary (node 0), insulation implies no heat flux, which translates to: \begin{equation} \frac{\partial T_0}{\partial x} = 0 \end{equation} For the right boundary (node 5), radiation is considered, and the boundary condition is given by: \begin{equation} -k \frac{\partial T_5}{\partial x} = \varepsilon\sigma(T_5^4 - T_{\text{surr}}^4) \end{equation} where \(k\) is the thermal conductivity and \(\sigma\) is the Stefan-Boltzmann constant.
04

Obtain finite difference equations for boundary nodes

Using the finite difference discretization from Step 2, we can obtain the equations for the boundary nodes as: Node 0 (Left boundary, insulation): \begin{equation} T_1^n = T_{-1}^n \end{equation} Node 5 (Right boundary, radiation): \begin{equation} k \frac{T_5^n - T_4^n}{\Delta x} = \varepsilon\sigma\left({T_5^n}^4 - {T_{\text{surr}}}^4\right) \end{equation} With the above equations, we have obtained the explicit finite difference formulation for the boundary nodes in the given transient heat conduction problem.

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Most popular questions from this chapter

Consider a large uranium plate of thickness \(5 \mathrm{~cm}\) and thermal conductivity \(k=34 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) in which heat is generated uniformly at a constant rate of $\dot{e}=6 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$. One side of the plate is insulated, while the other side is subjected to convection to an environment at \(30^{\circ} \mathrm{C}\) with a heat transfer coefficient of $h=60 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. Considering six equally spaced nodes with a nodal spacing of \)1 \mathrm{~cm},(a)$ obtain the finite difference formulation of this problem and (b) determine the nodal temperatures under steady conditions by solving those equations.

A plane wall with surface temperature of \(350^{\circ} \mathrm{C}\) is attached with straight rectangular fins $(k=235 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\(. The fins are exposed to an ambient air condition of \)25^{\circ} \mathrm{C}\(, and the convection heat transfer coefficient is \)154 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\(. Each fin has a length of \)50 \mathrm{~mm}$, a base \(5 \mathrm{~mm}\) thick, and a width of \(100 \mathrm{~mm}\). For a single fin, using a uniform nodal spacing of \(10 \mathrm{~mm}\), determine \((a)\) the finite difference equations, (b) the nodal temperatures by solving the finite difference equations, and \((c)\) the heat transfer rate and compare the result with the analytical solution.

A stainless steel plate is connected to an insulation plate by square ASTM A479 904L stainless steel bars. Each square bar has a thickness of $1 \mathrm{~cm}\( and a length of \)5 \mathrm{~cm}$. The bars are exposed to convection heat transfer with a hot gas. The temperature of the hot gas is \(300^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of $25 \mathrm{~W} / \mathrm{m}^{2}$. . The thermal conductivity for ASTM A479 904L stainless steel is known to be \(12 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The stainless steel plate maintains a uniform temperature of $100^{\circ} \mathrm{C}$. According to the ASME Code for Process Piping (ASME B31.3-2014, Table A-1M), the maximum use temperature for ASTM A479 904L stainless steel bar is \(260^{\circ} \mathrm{C}\). Using the finite difference method with a uniform nodal spacing of \(\Delta x=5 \mathrm{~mm}\) along the bar, determine the temperature at each node. Compare the numerical results with the analytical solution. Plot the temperature distribution along the bar. Would any part of the ASTM A479 904L bars be above the maximum use temperature of \(260^{\circ} \mathrm{C}\) ?

What is a practical way of checking if the discretization error has been significant in calculations?

Consider steady one-dimensional heat conduction in a plane wall with variable heat generation and variable thermal conductivity. The nodal network of the medium consists of nodes 0,1 , and 2 with a uniform nodal spacing of $\Delta x$. Using the energy balance approach, obtain the finite difference formulation of this problem for the case of specified heat flux \(\dot{q}_{0}\) to the wall and convection at the left boundary (node 0 ) with a convection coefficient of \(h\) and ambient temperature of \(T_{\infty^{+}}\) and radiation at the right boundary (node 2 ) with an emissivity of \(\varepsilon\) and surrounding surface temperature of \(T_{\text {surr }}\)

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