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For a one-dimensional, steady-state, variable thermal conductivity heat conduction with uniform internal heat generation, develop a generalized finite difference formulation for the interior nodes, with the left surface boundary node exposed to constant heat flux and the right surface boundary node exposed to a convective environment. The variable conductivity is modeled such that the thermal conductivity varies linearly with the temperature as \(k(T)=k_{o}(1+\beta T)\) where \(T\) is the average temperature between the two nodes.

Short Answer

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Question: Develop a finite difference formulation for a one-dimensional, steady-state heat conduction problem with variable thermal conductivity and uniform internal heat generation. Consider linear temperature-dependence of thermal conductivity. The left surface boundary node is exposed to a constant heat flux, and the right surface boundary is exposed to a convective environment. Answer: The finite difference formulation for interior nodes (2 to N-1) is given by: \(k_{o}(1+\beta T_{i})\frac{T_{i+1}-2T_{i}+T_{i-1}}{(\Delta x)^2} + q_{gen} = 0\) For the boundary nodes, we have: 1. Left boundary node (i=1): \(k_{o}(1+\beta T_{1})\frac{T_{2}-T_{1}}{\Delta x} = q_{f}\) 2. Right boundary node (i=N): \(k_{o}(1+\beta T_{N})\frac{T_{N}-T_{N-1}}{\Delta x} = h(T_{N}-T_{\infty})\) These equations, combined with the given boundary conditions, can be used to solve for the temperature distribution across the spatial domain.

Step by step solution

01

Understand the problem and given data

We are given a one-dimensional, steady-state heat conduction problem with variable thermal conductivity and uniform internal heat generation. The conductivity varies linearly with the temperature as \(k(T)=k_{o}(1+\beta T)\). The left surface boundary node is exposed to a constant heat flux, and the right surface boundary is exposed to a convective environment.
02

Write the general heat conduction equation

For one-dimensional, steady-state heat conduction with variable thermal conductivity and uniform internal heat generation, the general heat conduction equation is: \(\frac{d}{dx}\left[k(T)\frac{dT}{dx}\right] + q_{gen} = 0\)
03

Apply the finite difference method

We can discretize the spatial domain into N nodes, and the equation becomes: \(\frac{d}{dx}\left[k(T_{i})\frac{T_{i+1}-T_{i-1}}{2\Delta x}\right] + q_{gen} = 0\)
04

Rearrange the equation for interior nodes and incorporate the variable conductivity

We will now rewrite the equation for the interior nodes by substituting the given conductivity expression and rearrange to obtain an expression for node i: \(k_{o}(1+\beta T_{i})\frac{T_{i+1}-2T_{i}+T_{i-1}}{(\Delta x)^2} + q_{gen} = 0\)
05

Implement boundary conditions

We need to apply the boundary conditions at the left and right surface nodes. Suppose that at the left boundary, we have a constant heat flux \(q_{f}\) and we can use a forward difference approximation: \(k_{o}(1+\beta T_{1})\frac{T_{2}-T_{1}}{\Delta x} = q_{f}\) For the right boundary, assume that it is exposed to a convective environment with convective heat transfer coefficient \(h\) and ambient temperature \(T_{\infty}\). Then, we apply the Newton's law of cooling to the right boundary node, N: \(k_{o}(1+\beta T_{N})\frac{T_{N}-T_{N-1}}{\Delta x} = h(T_{N}-T_{\infty})\)
06

Develop the finite difference formulation

With all the derived expressions and boundary conditions, we can construct a linear system of N equations for N unknown temperatures. The finite difference formulation for interior nodes (2 to N-1) is given by: \(k_{o}(1+\beta T_{i})\frac{T_{i+1}-2T_{i}+T_{i-1}}{(\Delta x)^2} + q_{gen} = 0\) For the boundary nodes, we have: 1. Left boundary node (i=1): \(k_{o}(1+\beta T_{1})\frac{T_{2}-T_{1}}{\Delta x} = q_{f}\) 2. Right boundary node (i=N): \(k_{o}(1+\beta T_{N})\frac{T_{N}-T_{N-1}}{\Delta x} = h(T_{N}-T_{\infty})\) We can solve this system of linear equations to obtain the temperature distribution across the spatial domain under the specified conditions.

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Most popular questions from this chapter

The unsteady forward-difference heat conduction for a constant-area \((A)\) pin fin with perimeter \(p\), when exposed to air whose temperature is \(T_{0}\) with a convection heat transfer coefficient of \(h\), is $$ \begin{aligned} T_{m}^{*+1}=& \frac{k}{\rho c_{p} \Delta x^{2}}\left[T_{m-1}^{*}+T_{m+1}^{*}+\frac{h p \Delta x^{2}}{A} T_{0}\right] \\\ &-\left[1-\frac{2 k}{\rho c_{p} \Delta x^{2}}-\frac{h p}{\rho c_{p} A}\right] T_{m}^{*} \end{aligned} $$ In order for this equation to produce a stable solution, the quantity $\frac{2 k}{\rho c_{p} \Delta x^{2}}+\frac{h p}{\rho c_{p} A}$ must be (a) negative (b) zero (c) positive (d) greater than 1 (e) less than 1

Consider a large plane wall of thickness \(L=0.3 \mathrm{~m}\), thermal conductivity \(k=1.8 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and surface area \(A=24 \mathrm{~m}^{2}\). The left side of the wall is subjected to a heat flux of \(\dot{q}_{0}=350 \mathrm{~W} / \mathrm{m}^{2}\), while the temperature at that surface is measured to be \(T_{0}=60^{\circ} \mathrm{C}\). Assuming steady one-dimensional heat transfer and taking the nodal spacing to be $6 \mathrm{~cm},(a)$ obtain the finite difference formulation for the six nodes and \((b)\) determine the temperature of the other surface of the wall by solving those equations.

Consider a large uranium plate of thickness \(L=9 \mathrm{~cm}\), thermal conductivity \(k=28 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and thermal diffusivity \(\alpha=12.5 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\) that is initially at a uniform temperature of \(100^{\circ} \mathrm{C}\). Heat is generated uniformly in the plate at a constant rate of $\dot{e}=10^{6} \mathrm{~W} / \mathrm{m}^{3}\(. At time \)t=0$, the left side of the plate is insulated while the other side is subjected to convection with an environment at \(T_{\infty}=20^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(h=35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Using the explicit finite difference approach with a uniform nodal spacing of $\Delta x=1.5 \mathrm{~cm}\(, determine \)(a)$ the temperature distribution in the plate after \(5 \mathrm{~min}\) and \((b)\) how long it will take for steady conditions to be reached in the plate.

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 $1 \mathrm{~cm}$.

Explain how the finite difference form of a heat conduction problem is obtained by the energy balance method.

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