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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 subjected to specified heat flux, express the stability criterion for this problem in its simplest form.

Short Answer

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Define the stability criterion for a transient one-dimensional heat conduction problem in a plane wall with specified heat flux on both sides using the explicit method. The stability criterion for this problem, using the explicit method, is given by the maximum allowable time step, and it can be expressed in its simplest form as: Δt ≤ (Δx²) / (2α) where Δt is the time step, Δx is the spatial step, and α is the thermal diffusivity of the material.

Step by step solution

01

Understand the explicit method for solving heat conduction problems

In the explicit method, the temperature at a point (i, j) in the grid depends on the temperatures at points (i-1, j), (i+1, j), and (i, j-1) at the previous time step. The general equation for the explicit method is given by: T_i^{n+1} = T_i^n + \Delta t \cdot \frac{\alpha}{\Delta x^2} (T_{i+1}^n - 2T_i^n + T_{i-1}^n) where T_i^n is the temperature at a spatial grid point i and time step n, \Delta t is the time step, \Delta x is the spatial step, and \alpha is the thermal diffusivity of the material.
02

Find the stability criterion

The stability criterion for the explicit method is given by: Fo \leq \frac{1}{2} where Fo is the Fourier number, defined as: Fo = \frac{\alpha \Delta t}{\Delta x^2} Rearranging to solve for the maximum allowable time step, the stability criterion becomes: \Delta t \leq \frac{\Delta x^2}{2\alpha}
03

Simplify the stability criterion

In this case, there are specified heat fluxes on both sides of the plane wall, which implies a constant rate of heat flow. However, the stability criterion derived in Step 2 is a general one and does not account for this specific boundary condition. As both sides are subjected to specified heat flux, the behavior of temperatures within the wall remains the same and the stability criterion does not change. Thus, the simplest form of the stability criterion for this problem is: \Delta t \leq \frac{\Delta x^2}{2\alpha}

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Most popular questions from this chapter

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. \(4 .\)

What happens to the discretization and the roundoff errors as the step size is decreased?

Starting with an energy balance on a volume element, obtain the two- dimensional transient implicit 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.

Consider a long concrete dam $(k=0.6 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\left.\alpha_{s}=0.7\right)$ of triangular cross section whose exposed surface is subjected to solar heat flux of $\dot{q}_{s}=800 \mathrm{~W} / \mathrm{m}^{2}$ and to convection and radiation to the environment at \(25^{\circ} \mathrm{C}\) with a combined heat transfer coefficient of \(30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The 2-m-high vertical section of the dam is subjected to convection by water at \(15^{\circ} \mathrm{C}\) with a heat transfer coefficient of $150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, and heat transfer through the 2 -m-long base is considered to be negligible. Using the finite difference method with a mesh size of \(\Delta x=\Delta y=1 \mathrm{~m}\) and assuming steady two-dimensional heat transfer, determine the temperature of the top, middle, and bottom of the exposed surface of the dam. Answers: \(21.3^{\circ} \mathrm{C}\). $43.2^{\circ} \mathrm{C}, 43.6^{\circ} \mathrm{C}$

Consider transient heat conduction in a plane wall whose left surface (node 0 ) is maintained at \(80^{\circ} \mathrm{C}\) while the right surface (node 6) is subjected to a solar heat flux of \(600 \mathrm{~W} / \mathrm{m}^{2}\). The wall is initially at a uniform temperature of \(50^{\circ} \mathrm{C}\). Express the explicit finite difference formulation of the boundary nodes 0 and 6 for the case of no heat generation. Also, obtain the finite difference formulation for the total amount of heat transfer at the left boundary during the first three time steps.

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