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Consider transient one-dimensional heat conduction in a plane wall that is to be solved by the explicit method. If both sides of the wall are at specified temperatures, express the stability criterion for this problem in its simplest form.

Short Answer

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Answer: The stability criterion for one-dimensional transient heat conduction in a plane wall using the explicit method is \(S \leq 0.5\), where \(S\) is defined as \(S = \frac{\alpha \Delta t}{(\Delta x)^2}\) with \(\alpha\) representing the thermal diffusivity of the material, \(\Delta t\) representing the time step, and \(\Delta x\) representing the grid spacing. It is important to ensure this criterion is met to avoid numerical instability.

Step by step solution

01

Understand the explicit method

The explicit method is a numerical technique used for solving partial differential equations (PDEs), in this case, the heat conduction equation. The explicit method uses a finite difference approximation of derivatives to advance the solution in time.
02

The heat conduction equation

One-dimensional transient heat conduction in a plane wall can be described by the following PDE: \[ \frac{\partial T}{\partial t} = \alpha \frac{\partial^2 T}{\partial x^2} \] Where \(T\) is the temperature, \(t\) is time, \(x\) is the spatial coordinate, and \(\alpha\) is the thermal diffusivity of the material.
03

Discretizing the heat conduction equation

We will now discretize the heat conduction equation for the plane wall using the explicit method, which involves replacing partial derivatives with finite difference approximations. For this exercise, we can use forward difference in time and central difference in space. This will transform the PDE into the following equation: \[ \frac{T^{n+1}_i - T^n_i}{\Delta t} = \alpha \frac{T^n_{i+1} - 2T^n_i + T^n_{i-1}}{(\Delta x)^2} \]
04

Rewrite the equation for stability criteria

To determine stability, we need to rewrite the equation: \[ T^{n+1}_i = T^n_i + S\left(T^n_{i+1} - 2T^n_i + T^n_{i-1}\right) \] Where \(S = \frac{\alpha \Delta t}{(\Delta x)^2}\) is the stability criteria.
05

Apply the stability criterion

The explicit method is stable if the stability criterion, \(S\), is less than or equal to 0.5, which can be formally expressed as: \[ S \leq 0.5 \] This is the simplest form of the stability criterion for this problem. It is essential to ensure this criterion is met while choosing the time step and grid spacing to avoid numerical instability.

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Most popular questions from this chapter

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.

A hot surface at \(120^{\circ} \mathrm{C}\) is to be cooled by attaching 8-cm- long, \(0.8-\mathrm{cm}\) - diameter aluminum pin fins ( $k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\( and \)\left.\alpha=97.1 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\right)$ to it with a center-to-center distance of \(1.6 \mathrm{~cm}\). The temperature of the surrounding medium is $15^{\circ} \mathrm{C}\(, and the heat transfer coefficient on the surfaces is \)35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Initially, the fins are at a uniform temperature of \(30^{\circ} \mathrm{C}\), and at time \(t=0\), the temperature of the hot surface is raised to \(120^{\circ} \mathrm{C}\). Assuming one-dimensional heat conduction along the fin and taking the nodal spacing to be \(\Delta x=2 \mathrm{~cm}\) and a time step to be \(\Delta t=0.5 \mathrm{~s}\), determine the nodal temperatures after \(10 \mathrm{~min}\) by using the explicit finite difference method. Also, determine how long it will take for steady conditions to be reached.

Using appropriate software, solve these systems of algebraic equations. (a) $$ \begin{aligned} 3 x_{1}+2 x_{2}-x_{3}+x_{4} &=6 \\ x_{1}+2 x_{2}-x_{4} &=-3 \\ -2 x_{1}+x_{2}+3 x_{3}+x_{4} &=2 \\ 3 x_{2}+x_{3}-4 x_{4} &=-6 \end{aligned} $$ (b) $$ \begin{aligned} 3 x_{1}+x_{2}^{2}+2 x_{3} &=8 \\ -x_{1}^{2}+3 x_{2}+2 x_{3} &=-6.293 \\ 2 x_{1}-x_{2}^{4}+4 x_{3} &=-12 \end{aligned} $$

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

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?

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