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Consider a large uranium plate of thickness \(5 \mathrm{~cm}\) and thermal conductivity \(k=34 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) in which heat is generated uniformly at a constant rate of $\dot{e}=6 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$. One side of the plate is insulated, while the other side is subjected to convection to an environment at \(30^{\circ} \mathrm{C}\) with a heat transfer coefficient of $h=60 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. Considering six equally spaced nodes with a nodal spacing of \)1 \mathrm{~cm},(a)$ obtain the finite difference formulation of this problem and (b) determine the nodal temperatures under steady conditions by solving those equations.

Short Answer

Expert verified
Answer: The governing equation for this problem, considering convection and heat generation, is given by: \(\frac{d^2 T}{d x^2} - \frac{\dot{e}}{k} = 0\)

Step by step solution

01

Understanding the Finite Difference Method (FDM)

FDM is a numerical technique that can be used to approximate solutions of partial differential equations (PDEs) arising from heat transfer problems. It discretizes the problem domain into a finite number of nodes and represents the PDEs at these nodes using Taylor series expansions. By solving the resulting linear algebraic system, we can compute the nodal values.
02

Discretize the Uranium Plate with Nodes

Divide the uranium plate into six equally spaced nodes, with a spacing of 1cm. Let's denote the nodal spacing as \(\Delta x\). The nodal temperatures are denoted by \(T_i\), where \(i\) is the node number (\(i=1,2,3,4,5,6\)), and \(T_1\) corresponds to the insulated side of the plate.
03

Derive the Finite Difference Equation of the Problem

For this problem, considering convection and heat generation, the governing equation is given by: \(\frac{d^2 T}{d x^2} - \frac{\dot{e}}{k} = 0\) Applying the finite difference formulation for the second-order derivative of temperature with respect to x, we have: \(\frac{T_{i+1} - 2T_i + T_{i-1}}{(\Delta x)^2} - \frac{\dot{e}}{k} = 0\) for \(i = 2, 3, 4, 5\) Except at \(i=1\) and \(i=6\) nodes, where there are boundary conditions. At the insulated side (node 1), the boundary condition is \(-k(dT_1/dx) = 0\), which results in \(T_{1} = T_{2}\). At the convective side (node 6), the boundary condition is \(-k(dT_{6}/dx) = h(T_6 - T_{\infty})\), where \(T_{\infty}\) is the environment temperature. Applying finite difference approximation, we have: \(-k \frac{T_6 - T_5}{\Delta x} = h(T_6 - T_{\infty})\) Now, we have derived the finite difference equations for the problem.
04

Formulate the Linear Algebraic System

Express the finite difference equations for all six nodes in terms of unknown nodal temperatures: (1) \(T_{1} = T_{2}\) (2) \(T_{2} - 2T_3 + T_4 = \frac{\dot{e}(\Delta x)^2}{k}\) (3) \(T_{3} - 2T_4 + T_5 = \frac{\dot{e}(\Delta x)^2}{k}\) (4) \(\frac{k(T_6 - T_5)}{\Delta x} = h(T_6 - T_{\infty})\)
05

Solve the Linear Algebraic System

Solving these equations simultaneously, we can obtain the nodal temperatures under steady-state conditions. You can use a scientific calculator, software, or even manual calculation to solve this linear system. Knowing the provided values: \(k = 34 \mathrm{~W~m^{-1}~K^{-1}}\), \(\dot{e} = 6 \times 10^5 \mathrm{~W~m^{-3}}\), \(\Delta x = 0.01 \mathrm{~m}\), \(h = 60 \mathrm{~W~m^{-2}~K^{-1}}\), and \(T_{\infty} = 30^{\circ} \mathrm{C}\), you can plug in these values and find the nodal temperatures. With this, the finite difference formulation of the problem is obtained (part a), and the nodal temperatures under steady conditions are determined by solving these finite difference equations (part b).

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Most popular questions from this chapter

The unsteady forward-difference heat conduction for a constant-area \((A)\) pin fin with perimeter \(p\), when exposed to air whose temperature is \(T_{0}\) with a convection heat transfer coefficient of \(h\), is $$ \begin{aligned} T_{m}^{*+1}=& \frac{k}{\rho c_{p} \Delta x^{2}}\left[T_{m-1}^{*}+T_{m+1}^{*}+\frac{h p \Delta x^{2}}{A} T_{0}\right] \\\ &-\left[1-\frac{2 k}{\rho c_{p} \Delta x^{2}}-\frac{h p}{\rho c_{p} A}\right] T_{m}^{*} \end{aligned} $$ In order for this equation to produce a stable solution, the quantity $\frac{2 k}{\rho c_{p} \Delta x^{2}}+\frac{h p}{\rho c_{p} A}$ must be (a) negative (b) zero (c) positive (d) greater than 1 (e) less than 1

A nonmetal plate is connected to a stainless steel plate by long ASTM A437 B4B stainless steel bolts \(9.5 \mathrm{~mm}\) in diameter. The portion of the bolts exposed to convection heat transfer with a cryogenic fluid is \(5 \mathrm{~cm}\) long. The fluid temperature for convection is at \(-50^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of $100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. The thermal conductivity of the bolts is known to be \)23.9 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$. Both the nonmetal and stainless steel plates maintain a uniform temperature of \(0^{\circ} \mathrm{C}\). According to the ASME Code for Process Piping (ASME B31.3-2014, Table A-2M), the minimum temperature suitable for ASTM A437 B4B stainless steel bolts is \(-30^{\circ} \mathrm{C}\). Using the finite difference method with a uniform nodal spacing of \(\Delta x=5 \mathrm{~mm}\) along the bolt, determine the temperature at each node. Compare the numerical results with the analytical solution. Plot the temperature distribution along the bolt. Would any part of the ASTM A437 B4B bolts be lower than the minimum suitable temperature of \(-30^{\circ} \mathrm{C}\) ?

Consider steady two-dimensional heat conduction in a square cross section $(3 \mathrm{~cm} \times 3 \mathrm{~cm}, k=20 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \alpha=6.694 \times\( \)10^{-6} \mathrm{~m}^{2} / \mathrm{s}$ ) with constant prescribed temperature of \(100^{\circ} \mathrm{C}\) and $300^{\circ} \mathrm{C}$ at the top and bottom surfaces, respectively. The left surface is exposed to a constant heat flux of \(1000 \mathrm{~W} / \mathrm{m}^{2}\), while the right surface is in contact with a convective environment $\left(h=45 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\right)\( at \)20^{\circ} \mathrm{C}\(. Using a uniform mesh size of \)\Delta x=\Delta y\(, determine \)(a)$ finite difference equations and \((b)\) the nodal temperatures using the Gauss- Seidel iteration method.

Starting with an energy balance on the volume element, obtain the three- dimensional transient explicit finite difference equation for a general interior node in rectangular coordinates for \(T(x, y, z, t)\) for the case of constant thermal conductivity and no heat generation.

Starting with an energy balance on a volume element, obtain the two- dimensional transient explicit finite difference equation for a general interior node in rectangular coordinates for \(T(x, y, t)\) for the case of constant thermal conductivity and no heat generation.

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