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Consider transient 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 $\Delta x$. The wall is initially at a specified temperature. Using the energy balance approach, obtain the explicit 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 \(T_{\infty}\). Do not simplify.

Short Answer

Expert verified
Answer: For the boundary nodes 0 and 4, the explicit finite difference formulations are as follows: Node 0: \(T^{n+1}_0 = T^n_0 + \frac{\alpha \Delta t}{\Delta x^2}(T^n_1 - 2 T^n_0) + \frac{\Delta t q}{\rho c_p} + \frac{\dot{q}_{0} \Delta x}{k}\) Node 4: \(T^{n+1}_4 = T^n_4 + \frac{\alpha \Delta t}{\Delta x^2}(T^n_3 - 2 T^n_4) + \frac{\Delta t q}{\rho c_p} + \frac{\Delta x h (T_\infty - T^n_4)}{k}\)

Step by step solution

01

Write down the energy balance equation

For transient heat conduction with variable heat generation (given as \(q\)) and constant thermal conductivity (denoted by \(k\)), we can write the energy balance equation as: \(\frac{\partial T}{\partial t} = \alpha \frac{\partial^2 T}{\partial x^2} + \frac{q}{\rho c_p}\) where \(\alpha\) is the thermal diffusivity, T is the temperature, \(t\) is time, \(\rho\) is the density, and \(c_p\) is the heat capacity.
02

Apply finite difference approximations to the derivatives

To obtain the explicit finite difference formulation, we need to replace the derivatives in the energy balance equation by the finite difference approximations. For the time derivative, we use forward difference: \(\frac{T^{n+1}-T^n}{\Delta t} = \alpha \frac{T_{i+1}^n - 2T_i^n + T_{i-1}^n}{\Delta x^2} + \frac{q}{\rho c_p}\) For the spatial second-order derivative, we use central difference: \(\frac{T_{i+1}^n - 2T_i^n + T_{i-1}^n}{\Delta x^2} = \alpha \frac{T_{i+1}^n - 2T_i^n + T_{i-1}^n}{\Delta x^2} + \frac{q}{\rho c_p}\)
03

Obtain the explicit finite difference formulation for the boundary nodes

For the left boundary (node 0) with uniform heat flux \(\dot{q}_{0}\), we have: \(-\dot{q}_{0} = k\frac{T_1^0 - T_0^0}{\Delta x}\) Now, isolate \(T^0_0\) and use it in the finite difference equation at node 0: \(T^{n+1}_0 = T^n_0 + \frac{\alpha \Delta t}{\Delta x^2}(T^n_1 - 2 T^n_0) + \frac{\Delta t q}{\rho c_p} + \frac{\dot{q}_{0} \Delta x}{k}\) For the right boundary (node 4) with convection, we have: \(-k\frac{T_4^n - T_3^n}{\Delta x} + h(T_4^n - T_\infty) = 0\) Now, using this in the finite difference equation at node 4: \(T^{n+1}_4 = T^n_4 + \frac{\alpha \Delta t}{\Delta x^2}(T^n_3 - 2 T^n_4) + \frac{\Delta t q}{\rho c_p} + \frac{\Delta x h (T_\infty - T^n_4)}{k}\) These are the explicit finite difference formulations for the boundary nodes 0 and 4 in the given problem.

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Most popular questions from this chapter

A composite wall is made of stainless steel $\left(k_{1}=13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \quad 30 \mathrm{~mm}\right.$ thick), concrete $\left(k_{2}=1.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, 30 \mathrm{~mm}\right.\( thick \))\(, and nonmetal \)\left(k_{3}=0.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.\(, \)15 \mathrm{~mm}$ thick) plates. The concrete plate is sandwiched between the stainless steel plate at the bottom and the nonmetal plate at the top. A series of ASTM B21 naval brass bolts are bolted to the nonmetal plate, and the upper surface of the plate is exposed to convection heat transfer with air at \(20^{\circ} \mathrm{C}\) and $h=20 \mathrm{~W} / \mathrm{m}^{2}$.K. At the bottom surface, the stainless steel plate is subjected to a uniform heat flux of $2000 \mathrm{~W} / \mathrm{m}^{2}$. The ASME Code for Process Piping (ASME B31.3-2014, Table A-2M) limits the maximum use temperature for the ASTM B21 bolts to \(149^{\circ} \mathrm{C}\). Using the finite difference method with a uniform nodal spacing of \(\Delta x_{1}=10 \mathrm{~mm}\) for the stainless steel and concrete plates, and \(\Delta x_{2}=5 \mathrm{~mm}\) for the nonmetal plate, determine the temperature at each node. Plot the temperature distribution as a function of \(x\) along the plate thicknesses. Would the ASTM B21 bolts in the nonmetal plate comply with the ASME code?

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.

A stainless steel plate is connected to a copper plate by long ASTM B98 copper-silicon bolts \(9.5 \mathrm{~mm}\) in diameter. The portion of the bolts exposed to convection heat transfer with hot gas is \(5 \mathrm{~cm}\) long. The gas temperature for convection is at \(500^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of $50 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. The thermal conductivity of the bolt is known to be \)36 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$. The stainless steel plate has a uniform temperature of \(100^{\circ} \mathrm{C}\), and the copper plate has a uniform temperature of \(80^{\circ} \mathrm{C}\). According to the ASME Code for Process Piping (ASME B31.3-2014, Table A-2M), the maximum use temperature for an ASTM B98 copper-silicon bolt is \(149^{\circ} \mathrm{C}\). 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. Plot the temperature distribution along the bolt. Compare the numerical results with the analytical solution. Would any part of the ASTM B 98 bolts be above the maximum use temperature of \(149^{\circ} \mathrm{C}\) ?

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.

A cylindrical aluminum fin with adiabatic tip is attached to a wall with surface temperature of \(300^{\circ} \mathrm{C}\), and it is exposed to an ambient air condition of \(15^{\circ} \mathrm{C}\) with convection heat transfer coefficient of \(150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The fin has a uniform cross section with diameter of \(1 \mathrm{~cm}\), length of $5 \mathrm{~cm}\(, and thermal conductivity of \)237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$. Assuming steady one-dimensional heat transfer along the fin and the nodal spacing to be uniformly \(10 \mathrm{~mm},(a)\) obtain the finite difference equations for use with the Gauss-Seidel iterative method, and \((b)\) determine the nodal temperatures using the Gauss-Seidel iterative method, and compare the results with the analytical solution.

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