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

Short Answer

Expert verified
#Short Answer# The finite difference equation for a general interior node (i, j) in the case of variable thermal conductivity and uniform heat generation is: $$ k_{i+\frac{1}{2},j}(T_{i+1,j} - T_{i,j}) - k_{i-\frac{1}{2},j}(T_{i,j} - T_{i-1,j}) + k_{i,j+\frac{1}{2}}(T_{i,j+1} - T_{i,j}) - k_{i,j-\frac{1}{2}}(T_{i,j} - T_{i,j-1}) = Gh^2 $$

Step by step solution

01

Write the energy balance equation for the given conditions

We consider a general interior node \((x, y)\) of a volume element. The energy balance equation states that the heat generation (Q) is equal to the conduction heat loss (C), under steady-state conditions: $$ Q = C $$ Considering variable thermal conductivity (\(k(x, y)\)) and uniform heat generation (\(G\)), the equation can be written as: $$ G = \nabla \cdot (k(x, y) \nabla T(x, y)) $$
02

Expand the divergence term in rectangular coordinates

Let's now expand the divergence term in rectangular coordinates: $$ \nabla \cdot (k(x, y) \nabla T(x, y)) = \frac{\partial}{\partial x}(k(x, y) \frac{\partial T}{\partial x}) + \frac{\partial}{\partial y}(k(x, y) \frac{\partial T}{\partial y}) $$
03

Replace the derivatives with finite difference approximations

We will replace the partial derivatives in the previous equation with finite difference approximations for a general interior node \((i, j)\) in a grid with mesh spacing \(h\) in both \(x\) and \(y\) direction. Let's consider the finite-difference approximations for the required derivatives: $$ \frac{\partial}{\partial x}(k(x, y) \frac{\partial T}{\partial x}) \approx \frac{(k_{i+\frac{1}{2},j} (T_{i+1,j} - T_{i,j}) - k_{i-\frac{1}{2},j} (T_{i,j} - T_{i-1,j}))}{h^2} $$ $$ \frac{\partial}{\partial y}(k(x, y) \frac{\partial T}{\partial y}) \approx \frac{(k_{i,j+\frac{1}{2}} (T_{i,j+1} - T_{i,j}) - k_{i,j-\frac{1}{2}} (T_{i,j} - T_{i,j-1}))}{h^2} $$ Now, substitute these approximations in the energy balance equation and rearrange terms:
04

Obtain the finite difference equation

Substituting the approximations in the energy balance equation, we get: $$ G \approx \frac{(k_{i+\frac{1}{2},j} (T_{i+1,j} - T_{i,j}) - k_{i-\frac{1}{2},j} (T_{i,j} - T_{i-1,j}))}{h^2} + \frac{(k_{i,j+\frac{1}{2}} (T_{i,j+1} - T_{i,j}) - k_{i,j-\frac{1}{2}} (T_{i,j} - T_{i,j-1}))}{h^2} $$ Rearranging terms, the finite difference equation for a general interior node \((i, j)\) in the case of variable thermal conductivity and uniform heat generation becomes: $$ k_{i+\frac{1}{2},j}(T_{i+1,j} - T_{i,j}) - k_{i-\frac{1}{2},j}(T_{i,j} - T_{i-1,j}) + k_{i,j+\frac{1}{2}}(T_{i,j+1} - T_{i,j}) - k_{i,j-\frac{1}{2}}(T_{i,j} - T_{i,j-1}) = Gh^2 $$

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Most popular questions from this chapter

Hot combustion gases of a furnace are flowing through a concrete chimney \((k=1.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) of rectangular cross section. The flow section of the chimney is $20 \mathrm{~cm} \times 40 \mathrm{~cm}\(, and the thickness of the wall is \)10 \mathrm{~cm}$. The average temperature of the hot gases in the chimney is \(T_{i}=280^{\circ} \mathrm{C}\), and the average convection heat transfer coefficient inside the chimney is \(h_{l}=75 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The chimney is losing heat from its outer surface to the ambient air at $T_{0}=15^{\circ} \mathrm{C}\( by convection with a heat transfer coefficient of \)h_{o}=18 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ and to the sky by radiation. The emissivity of the outer surface of the wall is \(\varepsilon=0.9\), and the effective sky temperature is estimated to be \(250 \mathrm{~K}\). Using the finite difference method with \(\Delta x=\Delta y=10 \mathrm{~cm}\) and taking full advantage of symmetry, \((a)\) obtain the finite difference formulation of this problem for steady two-dimensional heat transfer, (b) determine the temperatures at the nodal points of a cross section, and \((c)\) evaluate the rate of heat loss for a \(1-m\)-long section of the chimney.

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.

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 a 5-m-long constantan block $(k=23 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( \)30 \mathrm{~cm}\( high and \)50 \mathrm{~cm}$ wide (Fig. P5-78). The block is completely submerged in iced water at \(0^{\circ} \mathrm{C}\) that is well stirred, and the heat transfer coefficient is so high that the temperatures on both sides of the block can be taken to be $0^{\circ} \mathrm{C}$. The bottom surface of the bar is covered with a low-conductivity material so that heat transfer through the bottom surface is negligible. The top surface of the block is heated uniformly by an \(8-\mathrm{kW}\) resistance heater. Using the finite difference method with a mesh size of $\Delta x=\Delta y=10 \mathrm{~cm}\( and taking advantage of symmetry, \)(a)$ obtain the finite difference formulation of this problem for steady twodimensional heat transfer, \((b)\) determine the unknown nodal temperatures by solving those equations, and \((c)\) determine the rate of heat transfer from the block to the iced water.

Consider a uranium nuclear fuel element $(k=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\rho=19,070 \mathrm{~kg} / \mathrm{m}^{3}\(, and \)\left.c_{p}=116 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( of radius \)10 \mathrm{~cm}$ that experiences a volumetric heat generation at a rate of $4 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$ because of the nuclear fission reaction. The nuclear fuel element initially at a temperature of \(500^{\circ} \mathrm{C}\) is enclosed inside a cladding made of stainless steel material $\left(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=8055 \mathrm{~kg} / \mathrm{m}^{3}\right.\(, and \)\left.c_{p}=480 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( of thickness \)4 \mathrm{~cm}$. The fuel element is cooled by passing pressurized heavy water over the cladding surface. The pressurized water has a bulk temperature of \(50^{\circ} \mathrm{C}\), and the convective heat transfer coefficient is $1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Assuming one-dimensional transient heat conduction in Cartesian coordinates, determine the temperature in the fuel rod and in the cladding after 10,20 , and \(30 \mathrm{~min}\). Use the implicit finite difference formulation with a uniform mesh size of \(2 \mathrm{~cm}\) and a time step of $1 \mathrm{~min}$.

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