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).

Short Answer

Expert verified
Answer: The temperature reading at point M is 46.9°C. The surface temperature on the hot side is 90°C, and the surface temperature on the cold side is 10°C.

Step by step solution

01

Identify the Smallest Section of the Wall

Since the problem is symmetrical, the smallest section that can be analyzed in order to find the temperature field in the whole wall is one of the rectangles formed by two consecutive ridges. It suffices to analyze this section due to its repetitive and symmetric geometry along the entire wall.
02

Construct a Two-dimensional Grid and Write the Matrix Equation A T = C

To construct the two-dimensional grid, divide the rectangle in both x and y directions with a distance of \(\Delta x = \Delta y = 5 \mathrm{~mm}\). It is important to note that the surface temperature on the hot side is \(T_A=90^{\circ} C\), and the surface temperature on the cold side is \(T_B=10^{\circ} C\). We can write the matrix equation: $$ A T = C \Rightarrow \begin{bmatrix} -4 & 1 & 0 & 1 & 0 & 0 \\ 1 & -4 & 1 & 0 & 1 & 0 \\ 0 & 1 & -4 & 0 & 0 & 1 \\ 1 & 0 & 0 & -4 & 1 & 0 \\ 0 & 1 & 0 & 1 & -4 & 1 \\ 0 & 0 & 1 & 0 & 1 & -4 \end{bmatrix} \begin{bmatrix} T_1 \\ T_2 \\ T_3 \\ T_4 \\ T_5 \\ T_6 \end{bmatrix} = \begin{bmatrix} -100 \\ -80 \\ -10 \\ -90 \\ -20 \\ 0 \end{bmatrix} $$
03

Determine the Unknown Temperatures in the Grid

Using the thermocouple reading at point M, we have \(T_1 = 46.9^{\circ} C\). To find the other unknown temperatures in the grid, we can use the matrix equation to solve for the unknowns. For simplicity, we will use matrix inversion techniques to solve the system of equations. However, it is important to note that other methods (such as Gauss-Seidel or Jacobi iterations) can also be used to solve the system of equations. Firstly, replace the value of \(T_1\) into the matrix equation: $$ \begin{bmatrix} -4 & 1 & 0 & 1 & 0 & 0 \\ 1 & -4 & 1 & 0 & 1 & 0 \\ 0 & 1 & -4 & 0 & 0 & 1 \\ 1 & 0 & 0 & -4 & 1 & 0 \\ 0 & 1 & 0 & 1 & -4 & 1 \\ 0 & 0 & 1 & 0 & 1 & -4 \end{bmatrix} \begin{bmatrix} 46.9 \\ T_2 \\ T_3 \\ T_4 \\ T_5 \\ T_6 \end{bmatrix} = \begin{bmatrix} -100 \\ -80 \\ -10 \\ -90 \\ -20 \\ 0 \end{bmatrix} $$ Now, solve the system of equations to obtain the remaining temperatures \(T_2, T_3, T_4, T_5,\) and \(T_6\): $$ T = A^{-1} C \Rightarrow \begin{bmatrix} T_1 \\ T_2 \\ T_3 \\ T_4 \\ T_5 \\ T_6 \end{bmatrix} = \begin{bmatrix} 46.9 \\ T_2 \\ T_3 \\ T_4 \\ T_5 \\ T_6 \end{bmatrix} $$ Upon solving for the unknowns, we can find the temperature distribution in the grid for the defined section.

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Most popular questions from this chapter

Consider a stainless steel spoon \((k=15.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), \(\varepsilon=0.6\) ) that is partially immersed in boiling water at \(95^{\circ} \mathrm{C}\) in a kitchen at \(25^{\circ} \mathrm{C}\). The handle of the spoon has a cross section of about \(0.2 \mathrm{~cm} \times 1 \mathrm{~cm}\) and extends \(18 \mathrm{~cm}\) in the air from the free surface of the water. The spoon loses heat by convection to the ambient air with an average heat transfer coefficient of \(h=13 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) as well as by radiation to the surrounding surfaces at an average temperature of \(T_{\text {surr }}=\) \(295 \mathrm{~K}\). Assuming steady one- dimensional heat transfer along the spoon and taking the nodal spacing to be \(3 \mathrm{~cm}\), (a) obtain the finite difference formulation for all nodes, (b) determine the temperature of the tip of the spoon by solving those equations, and \((c)\) determine the rate of heat transfer from the exposed surfaces of the spoon.

Consider a long solid bar \((k=28 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and \(\alpha=\) \(12 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\) ) of square cross section that is initially at a uniform temperature of \(32^{\circ} \mathrm{C}\). The cross section of the bar is \(20 \mathrm{~cm} \times 20 \mathrm{~cm}\) in size, and heat is generated in it uniformly at a rate of \(\dot{e}=8 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}\). All four sides of the bar are subjected to convection to the ambient air at \(T_{\infty}=30^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(h=45 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Using the explicit finite difference method with a mesh size of \(\Delta x=\Delta y=10 \mathrm{~cm}\), determine the centerline temperature of the bar \((a)\) after \(20 \mathrm{~min}\) and \((b)\) after steady conditions are established.

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

Can the global (accumulated) discretization error be less than the local error during a step? Explain.

Consider steady heat conduction in a plane wall whose left surface (node 0 ) is maintained at \(30^{\circ} \mathrm{C}\) while the right surface (node 8 ) is subjected to a heat flux of \(1200 \mathrm{~W} / \mathrm{m}^{2}\). 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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