Consider steady one-dimensional heat conduction in a plane wall with variable heat generation and constant thermal conductivity. The nodal network of the medium consists of nodes \(0,1,2,3\), and 4 with a uniform nodal spacing of \(\Delta x\). Using the finite difference form of the first derivative (not the energy balance approach), obtain the finite difference formulation of the boundary nodes for the case of uniform heat flux \(q_{0}\) at the left boundary (node 0 ) and convection at the right boundary (node 4) with a convection coefficient of \(h\) and an ambient temperature of \(T_{\infty}\).

Short Answer

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Answer: The finite difference formulations for the boundary nodes are: $$ T_{0} = T_{1} - \frac{q_{0} \Delta x}{\kappa} $$ $$ T_{4} = \frac{h \Delta x T_\infty + \kappa T_{3}}{h \Delta x + \kappa} $$

Step by step solution

01

Write the general heat conduction equation

Consider the steady one-dimensional heat conduction with variable heat generation, the general equation can be given as $$-\kappa \frac{d^{2} T}{d x^{2}}=q_{g}(x)$$ where \(\kappa\) is the constant thermal conductivity and \(q_{g}(x)\) is the heat generation term.
02

Write the finite difference form of the first derivative

Using the central difference approximation for the second derivative, the finite difference form can be written as $$ \frac{d^2 T}{d x^2} \approx \frac{T_{i+1} - 2T_{i} + T_{i-1}}{(\Delta x)^2} $$ Now, substituting the finite difference form back to the general equation, we get $$ -\kappa \frac{T_{i+1} - 2T_{i} + T_{i-1}}{(\Delta x)^2} = q_{g}(x) $$
03

Apply the boundary conditions and find the finite difference formulations for the boundary nodes

The given boundary conditions are: 1. Uniform heat flux \(q_{0}\) at the left boundary (node 0) 2. Convection at the right boundary (node 4) with a convection coefficient \(h\) and ambient temperature \(T_{\infty}\) To incorporate Boundary condition 1, we apply the heat flux relation: $$ q_{0} = -\kappa \frac{dT}{dx} \approx -\kappa \frac{T_{1}-T_{0}}{\Delta x} $$ We want to express \(T_{0}\) in terms of the other variables, so we rearrange the equation as: $$ T_{0} = T_{1} - \frac{q_{0} \Delta x}{\kappa} $$ Now, for boundary condition 2, we apply the convection condition at node 4: $$ -\kappa \frac{dT}{dx} = h (T_{4}-T_{\infty}) $$ Approximate the first derivative at node 4 as $$ -\kappa \frac{dT}{dx} \approx -\kappa \frac{T_{4}-T_{3}}{\Delta x} $$ Therefore, $$ -\kappa \frac{T_{4}-T_{3}}{\Delta x} = h (T_{4}-T_{\infty}) $$ Rearrange the equation to express \(T_{4}\) in terms of other variables, we get $$ T_{4} = \frac{h \Delta x T_\infty + \kappa T_{3}}{h \Delta x + \kappa} $$ The finite difference formulations for the boundary nodes are: $$ T_{0} = T_{1} - \frac{q_{0} \Delta x}{\kappa} $$ $$ T_{4} = \frac{h \Delta x T_\infty + \kappa T_{3}}{h \Delta x + \kappa} $$

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Most popular questions from this chapter

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 left surface boundary node exposed to constant heat flux and right surface boundary node exposed to 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.

Consider a 2-m-long and 0.7-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.

The wall of a heat exchanger separates hot water at \(T_{A}=90^{\circ} \mathrm{C}\) from cold water at \(T_{B}=10^{\circ} \mathrm{C}\). To extend the heat transfer area, two-dimensional ridges are machined on the cold side of the wall, as shown in Fig. P5-76. This geometry causes non-uniform thermal stresses, which may become critical for crack initiation along the lines between two ridges. To predict thermal stresses, the temperature field inside the wall must be determined. Convection coefficients are high enough so that the surface temperature is equal to that of the water on each side of the wall. (a) Identify the smallest section of the wall that can be analyzed in order to find the temperature field in the whole wall. (b) For the domain found in part \((a)\), construct a twodimensional grid with \(\Delta x=\Delta y=5 \mathrm{~mm}\) and write the matrix equation \(A T=C\) (elements of matrices \(A\) and \(C\) must be numbers). Do not solve for \(T\). (c) A thermocouple mounted at point \(M\) reads \(46.9^{\circ} \mathrm{C}\). Determine the other unknown temperatures in the grid defined in part (b).

A 1-m-long and 0.1-m-thick steel plate of thermal conductivity \(35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) is well insulated on its both sides, while the top surface is exposed to a uniform heat flux of \(5500 \mathrm{~W} / \mathrm{m}^{2}\). The bottom surface is convectively cooled by a fluid at \(10^{\circ} \mathrm{C}\) having a convective heat transfer coefficient of \(150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Assuming one dimensional heat conduction in the lateral direction, find the temperature at the midpoint of the plate. Discretize the plate thickness into four equal parts.

Consider steady one-dimensional heat conduction in a composite plane wall consisting of two layers \(A\) and \(B\) in perfect contact at the interface. The wall involves no heat generation. The nodal network of the medium consists of nodes 0,1 (at the interface), 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 insulation at the left boundary (node 0 ) and radiation at the right boundary (node 2) with an emissivity of \(\varepsilon\) and surrounding temperature of \(T_{\text {surr }}\)

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