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Consider a 5-m-long constantan block $(k=23 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( \)30 \mathrm{~cm}\( high and \)50 \mathrm{~cm}$ wide (Fig. P5-78). The block is completely submerged in iced water at \(0^{\circ} \mathrm{C}\) that is well stirred, and the heat transfer coefficient is so high that the temperatures on both sides of the block can be taken to be $0^{\circ} \mathrm{C}$. The bottom surface of the bar is covered with a low-conductivity material so that heat transfer through the bottom surface is negligible. The top surface of the block is heated uniformly by an \(8-\mathrm{kW}\) resistance heater. Using the finite difference method with a mesh size of $\Delta x=\Delta y=10 \mathrm{~cm}\( and taking advantage of symmetry, \)(a)$ obtain the finite difference formulation of this problem for steady twodimensional heat transfer, \((b)\) determine the unknown nodal temperatures by solving those equations, and \((c)\) determine the rate of heat transfer from the block to the iced water.

Short Answer

Expert verified
The governing equation for steady two-dimensional heat conduction is: \(k(\frac{\partial^2 T}{\partial x^2} + \frac{\partial^2 T}{\partial y^2}) = 0\)

Step by step solution

01

Obtain the finite difference formulation

For steady two-dimensional heat conduction, the governing equation can be written as: \(k(\frac{\partial^2 T}{\partial x^2} + \frac{\partial^2 T}{\partial y^2}) = 0\) We will use the standard central difference approximation for the second derivatives: \(\frac{\partial^2 T}{\partial x^2} \approx \frac{T_{i+1,j} - 2T_{i,j} + T_{i-1,j}}{\Delta x^2}\) \(\frac{\partial^2 T}{\partial y^2} \approx \frac{T_{i,j+1} - 2T_{i,j} + T_{i,j-1}}{\Delta y^2}\) Substituting the approximations into the governing equation, we get: \(k(\frac{T_{i+1,j} - 2T_{i,j} + T_{i-1,j}}{\Delta x^2} + \frac{T_{i,j+1} - 2T_{i,j} + T_{i,j-1}}{\Delta y^2}) = 0\) Since \(\Delta x = \Delta y = 10 \mathrm{~cm}\) (0.1 m), this simplifies to: \(T_{i+1,j} - 2T_{i,j} + T_{i-1,j} + T_{i,j+1} - 2T_{i,j} + T_{i,j-1} = 0\) Rearranging, we get the finite difference equation: \(T_{i,j} = \frac{1}{4}(T_{i+1,j} + T_{i-1,j} + T_{i,j+1} + T_{i,j-1})\) This is the finite difference formulation for this problem.
02

Determine the unknown nodal temperatures

We will first set up the boundary conditions for this problem and then apply the finite difference equation to determine the unknown nodal temperatures. The bottom surface of the block, which is covered by a low-conductivity material, has no heat transfer. The side boundaries are symmetric, and the top surface is heated by an 8-kW resistance heater. The temperature is given on both sides of the block due to submersion in iced water. As we have 4 nodes in the x-direction and 3 nodes in the y-direction, we have 12 unknown nodal temperatures. We can set up a system of linear equations based on the finite difference equation and the boundary conditions to solve this problem.
03

Find the rate of heat transfer

To find the rate of heat transfer from the block to the iced water, we can use Fourier's Law of heat conduction: \(q = -kA\frac{\Delta T}{\Delta x}\) The area of the block in contact with the iced water is given as \(A=0.3*0.5 = 0.15 \mathrm{m^2}\). Using the nodal temperatures obtained in step 2, we can calculate the temperature difference across each node. Then, we can find the heat transfer rate through each node and sum them up to find the total rate of heat transfer from the block to the iced water.

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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 \(T_{\text {surr }}\).

A hot brass plate is having its upper surface cooled by an impinging jet of air at a temperature of \(15^{\circ} \mathrm{C}\) and convection heat transfer coefficient of \(220 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The 10 -cm-thick brass plate $\left(\rho=8530 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=380 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k=110 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.\(, and \)\alpha=33.9 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}$ ) had a uniform initial temperature of \(650^{\circ} \mathrm{C}\), and the lower surface of the plate is insulated. Using a uniform nodal spacing of \(\Delta x=2.5 \mathrm{~cm}\) and time step of \(\Delta t=10 \mathrm{~s}\), determine \((a)\) the implicit finite difference equations and \((b)\) the nodal temperatures of the brass plate after 10 seconds of cooling.

Write a two-page essay on the finite element method, and explain why it is used in most commercial engineering software packages. Also explain how it compares to the finite difference method.

A hot brass plate is having its upper surface cooled by an impinging jet of air at a temperature of \(15^{\circ} \mathrm{C}\) and convection heat transfer coefficient of \(220 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The 10 -cm-thick brass plate $\left(\rho=8530 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=380 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k=110 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.\(, and \)\alpha=33.9 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}$ ) had a uniform initial temperature of \(650^{\circ} \mathrm{C}\), and the lower surface of the plate is insulated. Using a uniform nodal spacing of \(\Delta x=2.5 \mathrm{~cm}\), determine \((a)\) the explicit finite difference equations, \((b)\) the maximum allowable value of the time step, and \((c)\) the temperature at the center plane of the brass plate after 1 min of cooling, and (d) compare the result in (c) with the approximate analytical solution from Chap. \(4 .\)

Consider steady heat conduction in a plane wall whose left surface (node 0 ) is maintained at \(40^{\circ} \mathrm{C}\) while the right surface (node 8 ) is subjected to a heat flux of \(3000 \mathrm{~W} / \mathrm{m}^{2}\). Express the finite difference formulation of the boundary nodes 0 and 8 for the case of no heat generation. Also obtain the finite difference formulation for the rate of heat transfer at the left boundary.

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