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Consider steady one-dimensional heat conduction in a pin fin of constant diameter \(D\) with constant thermal conductivity. The fin is losing heat by convection with the ambient air at \(T_{\infty}\left(\right.\) in ${ }^{\circ} \mathrm{C}\( ) with a convection coefficient of \)h$, and by radiation to the surrounding surfaces at an average temperature of \(T_{\text {sur }}\) (in \(\mathrm{K}\) ). 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 finite difference formulation of this problem for the case of a specified temperature at the fin base and convection and radiation heat transfer at the fin tip.

Short Answer

Expert verified
Question: Analyze the steady one-dimensional heat conduction in a pin fin, using an energy balance approach and obtain the finite difference formulation for the case of a specified temperature at the fin base and convection and radiation heat transfer at the fin tip. Assume a pin fin with constant diameter and thermal conductivity. Answer: The finite difference formulations for node 1 (fin middle) and node 2 (fin tip) are: Node 1: \((T_0 - T_1) + (T_2 - T_1) = \frac{hP\Delta{x}}{kA}(T_1 - T_{\infty})\) Node 2: \[\frac{kA}{\sigma \varepsilon PD\Delta{x}}(T_1 - T_2) = \frac{hP}{\sigma \varepsilon PD\Delta{x}}(T_2 - T_{\infty}) + (T_2^4 - T_{\text{sur}}^4)\]

Step by step solution

01

Energy balance at node 0 (fin base)

At node 0, there is a specified temperature (\(T_0\)). Therefore, there is no need to set up an energy balance equation since we already have the temperature information for this node.
02

Energy balance at node 1 (fin middle)

At node 1, we'll have heat conduction from node 0, heat conduction to node 2, and heat loss by convection from the surface of the fin. Write down the energy balance using Fourier's law and Newton's law of cooling: \[k\frac{A}{\Delta{x}}(T_0 - T_1) + k\frac{A}{\Delta{x}}(T_2 - T_1) = hP(T_1 - T_{\infty})\] Here, A is the cross-sectional area of the fin, and P is the perimeter of the fin.
03

Energy balance at node 2 (fin tip)

At node 2, we'll have heat conduction from node 1, heat loss by convection from the surface of the fin, and heat loss by radiation. Write down the energy balance using Fourier's law, Newton's law of cooling and Stefan-Boltzmann law: \[k\frac{A}{\Delta{x}}(T_1 - T_2) = hP(T_2 - T_{\infty}) + \sigma \varepsilon P(D\Delta{x})(T_2^4 - T_{\text {sur }}^4)\] Here, \(\sigma\) is the Stefan-Boltzmann constant, and \(\varepsilon\) is the emissivity of the fin's surface.
04

Rewrite the equations in finite difference form

Divide each term by \(kA/\Delta{x}\) in the equation for node 1 and by \(\sigma \varepsilon PD\Delta{x}\) in the equation for node 2 to obtain the finite difference equations. For node 1, \[(T_0 - T_1) + (T_2 - T_1) = \frac{hP\Delta{x}}{kA}(T_1 - T_{\infty})\] For node 2, \[\frac{kA}{\sigma \varepsilon PD\Delta{x}}(T_1 - T_2) = \frac{hP}{\sigma \varepsilon PD\Delta{x}}(T_2 - T_{\infty}) + (T_2^4 - T_{\text{sur}}^4)\] These are the finite difference formulations of the problem for the given case.

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Most popular questions from this chapter

Consider one-dimensional transient heat conduction in a composite plane wall that consists of two layers \(A\) and \(B\) with perfect contact at the interface. The wall involves no heat generation and initially is at a specified temperature. 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 explicit 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 \(T_{\text {surr }}\).

In many engineering applications variation in thermal properties is significant, especially when there are large temperature gradients or the material is not homogeneous. To account for these variations in thermal properties, develop a finite difference formulation for an internal node in the case of a three-dimensional, steady-state heat conduction equation with variable thermal conductivity.

What are the two basic methods of solution of transient problems based on finite differencing? How do heat transfer terms in the energy balance formulation differ in the two methods?

Consider transient two-dimensional heat conduction in a rectangular region that is to be solved by the explicit method. If all boundaries of the region are either insulated or at specified temperatures, express the stability criterion for this problem in its simplest form.

Two 3-m-long and \(0.4\)-cm-thick cast iron \((k=52 \mathrm{~W} /\) $\mathrm{m} \cdot \mathrm{K}, \varepsilon=0.8)\( steam pipes of outer diameter \)10 \mathrm{~cm}$ are connected to each other through two 1 -cm-thick flanges of outer diameter \(20 \mathrm{~cm}\). The steam flows inside the pipe at an average temperature of \(250^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(180 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The outer surface of the pipe is exposed to convection with ambient air at $12^{\circ} \mathrm{C}\( with a heat transfer coefficient of \)25 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$ as well as radiation with the surrounding surfaces at an average temperature of \(T_{\text {surr }}=290 \mathrm{~K}\). Assuming steady onedimensional heat conduction along the flanges and taking the nodal spacing to be \(1 \mathrm{~cm}\) along the flange, \((a)\) obtain the finite difference formulation for all nodes, \((b)\) determine the temperature at the tip of the flange by solving those equations, and \((c)\) determine the rate of heat transfer from the exposed surfaces of the flange.

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