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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.

Short Answer

Expert verified
Derive the steady three-dimensional finite difference equation for a general interior node in rectangular coordinates considering constant thermal conductivity and uniform heat generation. Solution: The steady three-dimensional finite difference equation for a general interior node in rectangular coordinates considering constant thermal conductivity and uniform heat generation is given by: \(T_{i,j,k} = \frac{1}{2k(\Delta x^2 + \Delta y^2 + \Delta z^2)}\Big((k\Delta y^2\Delta z^2)(T_{i+1,j,k} + T_{i-1,j,k}) + (k\Delta x^2\Delta z^2)(T_{i,j+1,k} + T_{i,j-1,k}) + (k\Delta x^2\Delta y^2)(T_{i,j,k+1} + T_{i,j,k-1}) - Q\Delta x^2\Delta y^2\Delta z^2\Big)\)

Step by step solution

01

Consider an arbitrary volume element

Consider an arbitrary volume element (\(\Delta x\), \(\Delta y\), \(\Delta z\)) within the 3-dimensional rectangular coordinate system. Our objective is to obtain the rate of heat transfer in and out of this volume element, taking into account the heat generation within the volume element.
02

Perform an energy balance on the volume element

Perform an energy balance on the volume element, considering heat transfer due to conduction along the x, y, z directions, and the heat generation within the volume element. The energy balance equation can be written as: \(\frac{\partial}{\partial x}(k_x\frac{\partial T}{\partial x}) + \frac{\partial}{\partial y}(k_y\frac{\partial T}{\partial y}) + \frac{\partial}{\partial z}(k_z\frac{\partial T}{\partial z}) + Q = 0 \) Since the thermal conductivity is constant, we can rewrite the energy balance equation as: \(k \Big(\frac{\partial^2 T}{\partial x^2} + \frac{\partial^2 T}{\partial y^2} + \frac{\partial^2 T}{\partial z^2} \Big) + Q = 0\)
03

Discretize the spatial dimensions

We need to discretize the spatial dimensions (\(x, y, z\)) by dividing the domain into a grid with nodes representing the temperature \(T_i\). In this case, we can represent the location of each node by the general coordinates: \((x_i, y_j, z_k)\) where \(i\), \(j\), and \(k\) denote the spatial indices in each dimension.
04

Apply finite difference approximations

The second-order central difference scheme for the second derivatives in the spatial dimensions can be written as: \(\frac{\partial^2 T}{\partial x^2} = \frac{T_{i+1,j,k} - 2T_{i,j,k} + T_{i-1,j,k}}{\Delta x^2}\) \(\frac{\partial^2 T}{\partial y^2} = \frac{T_{i,j+1,k} - 2T_{i,j,k} + T_{i,j-1,k}}{\Delta y^2}\) \(\frac{\partial^2 T}{\partial z^2} = \frac{T_{i,j,k+1} - 2T_{i,j,k} + T_{i,j,k-1}}{\Delta z^2}\) Substituting these approximations into the energy balance equation, we obtain \(k\Big(\frac{T_{i+1,j,k} - 2T_{i,j,k} + T_{i-1,j,k}}{\Delta x^2} + \frac{T_{i,j+1,k} - 2T_{i,j,k} + T_{i,j-1,k}}{\Delta y^2} + \frac{T_{i,j,k+1} - 2T_{i,j,k} + T_{i,j,k-1}}{\Delta z^2}\Big) + Q = 0\)
05

Rearrange the finite difference equation for a general interior node

Rearrange the terms in the equation to obtain the final steady three-dimensional finite difference equation for a general interior node in rectangular coordinates considering constant thermal conductivity and uniform heat generation: \(T_{i,j,k} = \frac{1}{2k(\Delta x^2 + \Delta y^2 + \Delta z^2)}\Big((k\Delta y^2\Delta z^2)(T_{i+1,j,k} + T_{i-1,j,k}) + (k\Delta x^2\Delta z^2)(T_{i,j+1,k} + T_{i,j-1,k}) + (k\Delta x^2\Delta y^2)(T_{i,j,k+1} + T_{i,j,k-1}) - Q\Delta x^2\Delta y^2\Delta z^2\Big)\)

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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.

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.

Quench hardening is a mechanical process in which the ferrous metals or alloys are first heated and then quickly cooled down to improve their physical properties and avoid phase transformation. Consider a $40-\mathrm{cm} \times 20-\mathrm{cm}\( block of copper alloy \)\left(k=120 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \alpha=3.91 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\right)$ being heated uniformly until it reaches a temperature of \(800^{\circ} \mathrm{C}\). It is then suddenly immersed into the water bath maintained at \(15^{\circ} \mathrm{C}\) with $h=100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ for quenching process. However, the upper surface of the metal is not submerged in the water and is exposed to air at $15^{\circ} \mathrm{C}\( with a convective heat transfer coefficient of \)10 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Using an explicit finite difference formulation, calculate the temperature distribution in the copper alloy block after 10 min have elapsed using \(\Delta t=10 \mathrm{~s}\) and a uniform mesh size of \(\Delta x=\Delta y=10 \mathrm{~cm}\).

Consider steady two-dimensional heat transfer in a long solid bar of square cross section in which heat is generated uniformly at a rate of $\dot{e}=0.19 \times 10^{5} \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{3}$. The cross section of the bar is \(0.5 \mathrm{ft} \times 0.5 \mathrm{ft}\) in size, and its thermal conductivity is $k=16 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}$. All four sides of the bar are subjected to convection with the ambient air at \(T_{\infty}=70^{\circ} \mathrm{F}\) with a heat transfer coefficient of $h=7.9 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}$. Using the finite difference method with a mesh size of \(\Delta x=\Delta y=0.25 \mathrm{ft}\), determine \((a)\) the temperatures at the nine nodes and \((b)\) the rate of heat loss from the bar through a 1-ft-long section.

Consider a medium in which the finite difference formulation of a general interior node is given in its simplest form as $$ \frac{T_{m-1}-2 T_{m}+T_{m+1}}{\Delta x^{2}}+\frac{\dot{e}_{m}}{k}=0 $$ (a) Is heat transfer in this medium steady or transient? (b) Is heat transfer one-, two-, or three-dimensional? (c) Is there heat generation in the medium? (d) Is the nodal spacing constant or variable? (e) Is the thermal conductivity of the medium constant or variable?

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