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Consider steady 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 energy balance approach, obtain the finite difference formulation of the boundary nodes for the case of uniform heat flux \(\dot{q}_{0}\) 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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#Question# Using the energy balance approach, obtain the finite difference formulation for the boundary nodes of a nodal network that consists of nodes 0 through 4, evenly spaced by a distance of Δx. The left boundary (node 0) has a uniform heat flux \(q_0\), and the right boundary (node 4) has convection with a convection coefficient h, and an ambient temperature \(T_\infty\). #Answer# For node 0: \(T_{0} = T_{1} + \frac{\dot{q}_{0}\Delta x}{k}\) For node 4: \(T_{4} = \frac{h\Delta x T_{\infty} + k T_{3}}{h\Delta x + k}\)

Step by step solution

01

Analyze boundary node 0 conditions

At node 0, there's a uniform heat flux \(\dot{q}_{0}\). Using Fourier's law of heat conduction, we have: \(\dot{q}_{0} = -k\frac{dT}{dx}|_{x=0}\), where \(k\) is the thermal conductivity.
02

Apply a finite difference approximation to the temperature gradient

The spatial derivative of the temperature at node 0 can be approximated using a forward finite difference method: \(\frac{dT}{dx}|_{x=0} \approx \frac{T_{1} - T_{0}}{\Delta x}\)
03

Calculate the temperature at node 0

Using the results from Step 1 and Step 2, we can now write an equation for the temperature at node 0: \(\dot{q}_{0} = -k\frac{T_{1} - T_{0}}{\Delta x}\) Now, isolate \(T_{0}\): \(T_{0} = T_{1} + \frac{\dot{q}_{0}\Delta x}{k}\)
04

Analyze boundary node 4 conditions

At node 4, we have convection with convection coefficient \(h\) and an ambient temperature of \(T_{\infty}\). Using Newton's law of cooling, we have: \(\dot{q}_{conv} = h(T_{4} - T_{\infty})\)
05

Apply a finite difference approximation to the energy balance equation

At node 4, the energy balance equation can be given as: \(\dot{q}_{conv} = -k\frac{dT}{dx}|_{x=4\Delta x}\) Using a backward finite difference approximation for the spatial derivative at node 4: \(\frac{dT}{dx}|_{x=4\Delta x} \approx \frac{T_{4} - T_{3}}{\Delta x}\)
06

Calculate the temperature at node 4

Using the results from Step 4 and Step 5, we can now write an equation for the temperature at node 4: \(h(T_{4} - T_{\infty}) = -k\frac{T_{4} - T_{3}}{\Delta x}\) Solving for \(T_{4}\), we get: \(T_{4} = \frac{h\Delta x T_{\infty} + k T_{3}}{h\Delta x + k}\) We've now obtained the finite difference formulation for the boundary nodes: - For node 0: \(T_{0} = T_{1} + \frac{\dot{q}_{0}\Delta x}{k}\) - For node 4: \(T_{4} = \frac{h\Delta x T_{\infty} + k T_{3}}{h\Delta x + k}\)

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Most popular questions from this chapter

Starting with an energy balance on a volume element, obtain the steady two- dimensional finite difference equation for a general interior node in rectangular coordinates for \(T(x, y)\) for the case of variable thermal conductivity and uniform heat generation.

Consider a rectangular metal block $(k=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( of dimensions \)100 \mathrm{~cm} \times 75 \mathrm{~cm}$ subjected to a sinusoidal temperature variation at its top surface while its bottom surface is insulated. The two sides of the metal block are exposed to a convective environment at \(15^{\circ} \mathrm{C}\) and have a heat transfer coefficient of \(50 \mathrm{~W} / \mathrm{m}^{2}\). \(\mathrm{K}\). The sinusoidal temperature distribution at the top surface is given as $100 \sin (\pi x / L)\(. Using a uniform mesh size of \)\Delta x=\Delta y=25 \mathrm{~cm}$, determine \((a)\) finite difference equations and \((b)\) the nodal temperatures.

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

A hot surface at \(100^{\circ} \mathrm{C}\) is to be cooled by attaching \(3-\mathrm{cm}-\) long, \(0.25-\mathrm{cm}\)-diameter aluminum pin fins $(k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})$ with a center-to-center distance of \(0.6 \mathrm{~cm}\). The temperature of the surrounding medium is \(30^{\circ} \mathrm{C}\), and the combined heat transfer coefficient on the surfaces is \(35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Assuming steady one-dimensional heat transfer along the fin and taking the nodal spacing to be \(0.5 \mathrm{~cm}\), determine \((a)\) the finite difference formulation of this problem, \((b)\) the nodal temperatures along the fin by solving these equations, \((c)\) the rate of heat transfer from a single fin, and \((d)\) the rate of heat transfer from a \(1-\mathrm{m} \times 1-\mathrm{m}\) section of the plate.

A series of long stainless steel bolts (ASTM A437 B4B) are fastened into a metal plate with a thickness of \(4 \mathrm{~cm}\). The bolts have a thermal conductivity of \(23.9 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), a specific heat of \(460 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), and a density of \(7.8 \mathrm{~g} / \mathrm{cm}^{3}\). For the metal plate, the specific heat, thermal conductivity, and density are $500 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, 16.3 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, and \)8 \mathrm{~g} / \mathrm{cm}^{3}$, respectively. The upper surface of the plate is occasionally exposed to cryogenic fluid at \(-70^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of $300 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The lower surface of the plate is exposed to convection with air at \(10^{\circ} \mathrm{C}\) and a convection heat transfer coefficient of \(10 \mathrm{~W} / \mathrm{m}^{2}\). K. The bolts are fastened into the metal plate from the bottom surface, and the distance measured from the plate's upper surface to the bolt tips is \(1 \mathrm{~cm}\). The ASME Code for Process Piping limits the minimum suitable temperature for ASTM A437 B4B stainless steel bolt to \(-30^{\circ} \mathrm{C}\) (ASME B31.3-2014, Table A-2M). If the initial temperature of the plate is \(10^{\circ} \mathrm{C}\) and the plate's upper surface is exposed to the cryogenic fluid for \(9 \mathrm{~min}\), would the bolts fastened in the plate still comply with the ASME code? Using the explicit finite difference formulations with a uniform nodal spacing of \(\Delta x=1 \mathrm{~cm}\), determine the temperature at each node for the duration of the upper surface being exposed to the cryogenic fluid. Plot the nodal temperatures as a function of time.

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