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Consider steady one-dimensional 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 \(\Delta x\). Using the finite difference form of the first derivative (not the energy balance approach), obtain the finite difference formulation of the boundary nodes for the case of uniform heat flux \(q_{0}\) 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 \(T_{\infty}\).

Short Answer

Expert verified
Answer: The finite difference formulations for the boundary nodes are: $$ T_{0} = T_{1} - \frac{q_{0} \Delta x}{\kappa} $$ $$ T_{4} = \frac{h \Delta x T_\infty + \kappa T_{3}}{h \Delta x + \kappa} $$

Step by step solution

01

Write the general heat conduction equation

Consider the steady one-dimensional heat conduction with variable heat generation, the general equation can be given as $$-\kappa \frac{d^{2} T}{d x^{2}}=q_{g}(x)$$ where \(\kappa\) is the constant thermal conductivity and \(q_{g}(x)\) is the heat generation term.
02

Write the finite difference form of the first derivative

Using the central difference approximation for the second derivative, the finite difference form can be written as $$ \frac{d^2 T}{d x^2} \approx \frac{T_{i+1} - 2T_{i} + T_{i-1}}{(\Delta x)^2} $$ Now, substituting the finite difference form back to the general equation, we get $$ -\kappa \frac{T_{i+1} - 2T_{i} + T_{i-1}}{(\Delta x)^2} = q_{g}(x) $$
03

Apply the boundary conditions and find the finite difference formulations for the boundary nodes

The given boundary conditions are: 1. Uniform heat flux \(q_{0}\) at the left boundary (node 0) 2. Convection at the right boundary (node 4) with a convection coefficient \(h\) and ambient temperature \(T_{\infty}\) To incorporate Boundary condition 1, we apply the heat flux relation: $$ q_{0} = -\kappa \frac{dT}{dx} \approx -\kappa \frac{T_{1}-T_{0}}{\Delta x} $$ We want to express \(T_{0}\) in terms of the other variables, so we rearrange the equation as: $$ T_{0} = T_{1} - \frac{q_{0} \Delta x}{\kappa} $$ Now, for boundary condition 2, we apply the convection condition at node 4: $$ -\kappa \frac{dT}{dx} = h (T_{4}-T_{\infty}) $$ Approximate the first derivative at node 4 as $$ -\kappa \frac{dT}{dx} \approx -\kappa \frac{T_{4}-T_{3}}{\Delta x} $$ Therefore, $$ -\kappa \frac{T_{4}-T_{3}}{\Delta x} = h (T_{4}-T_{\infty}) $$ Rearrange the equation to express \(T_{4}\) in terms of other variables, we get $$ T_{4} = \frac{h \Delta x T_\infty + \kappa T_{3}}{h \Delta x + \kappa} $$ The finite difference formulations for the boundary nodes are: $$ T_{0} = T_{1} - \frac{q_{0} \Delta x}{\kappa} $$ $$ T_{4} = \frac{h \Delta x T_\infty + \kappa T_{3}}{h \Delta x + \kappa} $$

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Finite Difference Method
The Finite Difference Method is a numerical technique used to approximate solutions to differential equations. In heat conduction problems, it helps us discretize the continuous domain into a set of discrete points or nodes. This approach allows us to turn differential equations into a set of algebraic equations that are easier to solve.

In the context of the given exercise, we're dealing with a one-dimensional system. The finite difference method involves approximating derivatives by differences between neighboring nodes. For instance, we use the central difference approximation for the second derivative:
  • \( \frac{d^2 T}{d x^2} \approx \frac{T_{i+1} - 2T_{i} + T_{i-1}}{(\Delta x)^2} \)
This equation helps us replace the continuous differential terms with discrete counterparts, making the problem solvable with respect to each node.
Boundary Conditions
Boundary conditions are essential in solving heat conduction problems as they describe how the system exchanges heat with its surroundings. In this exercise, two specific boundary conditions are considered:

  • **At the left boundary (node 0)**: There is a uniform heat flux \(q_{0}\). This condition is related to the rate at which heat is flowing into or out of the material. It is mathematically expressed as:
    • \( q_{0} = -\kappa \frac{T_{1}-T_{0}}{\Delta x} \)
  • **At the right boundary (node 4)**: Convection occurs with the surroundings, characterized by a convection coefficient \(h\) and an ambient temperature \(T_{\infty}\). This is given by:
    • \( -\kappa \frac{T_{4}-T_{3}}{\Delta x} = h (T_{4}-T_{\infty}) \)
These conditions are crucial for determining the temperature distribution across the nodes and ensure that the physical constraints of the problem are respected.
Heat Generation
Heat generation refers to the internal production of heat within a material. It can vary spatially (as \(q_{g}(x)\) in our equation) and influences the temperature distribution.

In the differential heat conduction equation:
  • \( -\kappa \frac{d^{2} T}{d x^{2}} = q_{g}(x) \)
The function \(q_{g}(x)\) represents this generated heat. The presence of heat generation adds complexity to the problem as it introduces another source affecting the temperature. The finite difference method allows approximating the effect of this term directly on the nodes, helping calculate how much each point is heated from within.
Thermal Conductivity
Thermal conductivity, denoted by \(\kappa\), is a material property that measures a material's ability to conduct heat. It is critical in defining how heat moves through a solid.

In the equation:
  • \( -\kappa \frac{d^2 T}{d x^2} = q_{g}(x) \)
\(\kappa\) helps determine the rate of heat flow per unit area per temperature gradient. In this exercise, it is constant, simplifying the calculations.

A higher \(\kappa\) indicates that the material conducts heat better, affecting both internal heat distribution and how it interacts with boundary conditions. The finite difference equations use \(\kappa\) to calculate temperature differences between nodes, providing insight into flow behavior across the material.

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Most popular questions from this chapter

How is an insulated boundary handled in finite difference formulation of a problem? How does a symmetry line differ from an insulated boundary in the finite difference formulation?

Consider a large plane wall of thickness \(L=0.3 \mathrm{~m}\), thermal conductivity \(k=2.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and surface area \(A=24 \mathrm{~m}^{2}\). The left side of the wall is subjected to a heat flux of \(\dot{q}_{0}=350 \mathrm{~W} / \mathrm{m}^{2}\) while the temperature at that surface is measured to be \(T_{0}=60^{\circ} \mathrm{C}\). Assuming steady one-dimensional heat transfer and taking the nodal spacing to be \(6 \mathrm{~cm},(a)\) obtain the finite difference formulation for the six nodes and (b) determine the temperature of the other surface of the wall by solving those equations.

Can the global (accumulated) discretization error be less than the local error during a step? Explain.

The wall of a heat exchanger separates hot water at \(T_{A}=90^{\circ} \mathrm{C}\) from cold water at \(T_{B}=10^{\circ} \mathrm{C}\). To extend the heat transfer area, two-dimensional ridges are machined on the cold side of the wall, as shown in Fig. P5-76. This geometry causes non-uniform thermal stresses, which may become critical for crack initiation along the lines between two ridges. To predict thermal stresses, the temperature field inside the wall must be determined. Convection coefficients are high enough so that the surface temperature is equal to that of the water on each side of the wall. (a) Identify the smallest section of the wall that can be analyzed in order to find the temperature field in the whole wall. (b) For the domain found in part \((a)\), construct a twodimensional grid with \(\Delta x=\Delta y=5 \mathrm{~mm}\) and write the matrix equation \(A T=C\) (elements of matrices \(A\) and \(C\) must be numbers). Do not solve for \(T\). (c) A thermocouple mounted at point \(M\) reads \(46.9^{\circ} \mathrm{C}\). Determine the other unknown temperatures in the grid defined in part (b).

Design a fire-resistant safety box whose outer dimensions are \(0.5 \mathrm{~m} \times 0.5 \mathrm{~m} \times 0.5 \mathrm{~m}\) that will protect its combustible contents from fire which may last up to \(2 \mathrm{~h}\). Assume the box will be exposed to an environment at an average temperature of \(700^{\circ} \mathrm{C}\) with a combined heat transfer coefficient of \(70 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and the temperature inside the box must be below \(150^{\circ} \mathrm{C}\) at the end of \(2 \mathrm{~h}\). The cavity of the box must be as large as possible while meeting the design constraints, and the insulation material selected must withstand the high temperatures to which it will be exposed. Cost, durability, and strength are also important considerations in the selection of insulation materials.

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