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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.

Short Answer

Expert verified
Based on the provided solution for finite difference formulation for steady-state heat conduction in a plane wall, the final equation we derived is: $$ T_{m-1}^{i} - 2T_{m}^{i} + T_{m+1}^{i} + \frac{e_{m}^{i} \Delta x^{2}}{k} = 0 $$

Step by step solution

01

Identify Steady-State Condition

For the steady-state case, the temperature does not change with time. So, the change in temperature between two successive time steps will be zero: $$ T_{m}^{i+1} - T_{m}^{i} = 0 $$
02

Substitute the Steady-State Condition into the Transient Equation

Replace the \((T_{m}^{i+1} - T_{m}^{i})\) term in the given transient equation with zero, as identified in Step 1: $$ T_{m=1}^{i} - 2T_{m}^{i} + T_{m+1}^{i} + \frac{e_{m}^{i} \Delta x^{2}}{k} = \frac{0}{\tau} $$
03

Simplify the Equation

Now, let's simplify the equation by removing the fraction: $$ T_{m-1}^{i} - 2T_{m}^{i} + T_{m+1}^{i} + \frac{e_{m}^{i} \Delta x^{2}}{k} = 0 $$ This is the finite difference formulation for steady-state heat conduction in a plane wall.

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Most popular questions from this chapter

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.

What are the basic steps involved in solving a system of equations with the Gauss-Seidel method?

A cylindrical aluminum fin with adiabatic tip is attached to a wall with surface temperature of \(300^{\circ} \mathrm{C}\), and it is exposed to an ambient air condition of \(15^{\circ} \mathrm{C}\) with convection heat transfer coefficient of \(150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The fin has a uniform cross section with diameter of \(1 \mathrm{~cm}\), length of $5 \mathrm{~cm}\(, and thermal conductivity of \)237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$. Assuming steady one-dimensional heat transfer along the fin and the nodal spacing to be uniformly \(10 \mathrm{~mm},(a)\) obtain the finite difference equations for use with the Gauss-Seidel iterative method, and \((b)\) determine the nodal temperatures using the Gauss-Seidel iterative method, and compare the results with the analytical solution.

Suggest some practical ways of reducing the roundoff error.

Consider transient one-dimensional heat conduction in a pin fin of constant diameter \(D\) with constant thermal conductivity. The fin is losing heat by convection to the ambient air at \(T_{\infty}\) with a heat transfer coefficient of \(h\) and by radiation to the surrounding surfaces at an average temperature of \(T_{\text {surr }}\) The nodal network of the fin consists of nodes 0 (at the base), 1 (in the middle), and 2 (at the fin tip) with a uniform nodal spacing of \(\Delta x\). Using the energy balance approach, obtain the explicit finite difference formulation of this problem for the case of a specified temperature at the fin base and negligible heat transfer at the fin tip.

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