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A truncated solid cone is of circular cross section, and its diameter is related to the axial coordinate by an expression of the form \(D=a x^{3 / 2}\), where \(a=1.0 \mathrm{~m}^{-1 / 2}\). The sides are well insulated, while the top surface of the cone at \(x_{1}\) is maintained at \(T_{1}\) and the bottom surface at \(x_{2}\) is maintained at \(T_{2}\). (a) Obtain an expression for the temperature distribution \(T(x)\). (b) What is the rate of heat transfer across the cone if it is constructed of pure aluminum with \(x_{1}=0.075 \mathrm{~m}\), \(T_{1}=100^{\circ} \mathrm{C}, x_{2}=0.225 \mathrm{~m}\), and \(T_{2}=20^{\circ} \mathrm{C}\) ?

Short Answer

Expert verified
To find the temperature distribution T(x) inside the truncated solid cone, we integrate the heat conduction equation with respect to x by considering that A(x) = 蟺((a/2)^2 * x^3). After applying the boundary conditions, we obtain the expression for T(x). Then, we can calculate the rate of heat transfer (Q) using the given values for x1, T1, x2, T2, and the area A(x). This will give us the rate of heat transfer across the cone under the provided conditions.

Step by step solution

01

Determine the area A(x)

To determine the area A(x) of the cone at a certain distance x along the axis, we can use the expression given for the diameter, D(x) = ax^(3/2). The radius, r(x), is half the diameter, so r(x) = (ax^(3/2))/2. Thus, the circular area A(x) = 蟺r^2 = 蟺((ax^(3/2))/2)^2. A(x) = 蟺((a/2)^2 * x^3)
02

Calculate the temperature gradient (鈭俆/鈭倄) using the equation of heat conduction

Fourier's law of heat conduction states that the rate of heat transfer (Q) is directly proportional to the temperature gradient (鈭俆/鈭倄) in the material. Since the sides of the truncated solid cone are well insulated, we only have to consider the radial temperature gradient. Mathematically, this can be written as: Q = -kA(x)(鈭俆/鈭倄) Where k is the thermal conductivity of aluminum, A(x) is the area at axial coordinate x, and (鈭俆/鈭倄) is the temperature gradient, which we need to determine.
03

Integrate to find T(x)

We can rearrange the equation from Step 2 to solve for T(x). (鈭俆/鈭倄) = -Q/(kA(x)) Since A(x) = 蟺((a/2)^2 * x^3), we can substitute it into the equation. (鈭俆/鈭倄) = -Q/(k * 蟺((a/2)^2 * x^3)) Now we can integrate with respect to x to find T(x). T(x) = 鈭(-Q/(k * 蟺((a/2)^2 * x^3)))dx T(x) is obtained after applying the boundary conditions T(x1) = T鈧 and T(x2) = T鈧. This will give us the expression for the temperature distribution T(x) inside the truncated cone.
04

Calculate the rate of heat transfer (Q) for the given conditions

With the given values for x1, T1, x2, and T2, we can plug them into the temperature distribution equation T(x) and solve for Q. x1 = 0.075 m, T1 = 100掳C, x2 = 0.225 m, T2 = 20掳C Thermal conductivity of aluminum, k = 205 W/(m*K) Calculate Q by using the equation Q = -kA(x)(鈭俆/鈭倄) and substituting the given values for T1, T2, x1, x2, and the area A(x). This will give us the rate of heat transfer across the truncated solid cone under the given conditions.

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Key Concepts

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

Temperature Distribution
In the context of heat transfer, understanding the temperature distribution within a solid object is crucial for predicting how heat will move through it. In our exercise, we examine a truncated solid cone and aim to derive an expression for temperature distribution, denoted as \( T(x) \). The temperature distribution tells us how temperature varies at each point along the axis of the cone.

Given that the sides of the cone are well-insulated and only the top and bottom surfaces have specified temperatures, this greatly simplifies our calculations. These specific temperature boundaries ensure that any heat transfer happens only along the axis of the cone, not across the diameter. This means that the temperature distribution along the x-axis can be calculated by analyzing how heat flows from the hotter top to the cooler bottom of the cone, a process governed by Fourier's Law. Our goal is to establish a mathematical function, \( T(x) \), that models this temperature change from \( T_1 = 100^{\circ}C \) at the top to \( T_2 = 20^{\circ}C \) at the bottom.
Fourier's Law
Fourier's Law of heat conduction is fundamental in understanding how heat transfers through materials. It articulates that the rate of heat transfer through a material is directly proportional to the negative of the temperature gradient and the area through which the heat flows.

Mathematically, it is represented as:
  • \( Q = -kA(x) \left( \frac{\partial T}{\partial x} \right) \)
Here,
  • \( Q \) is the heat transfer rate,
  • \( k \) is the thermal conductivity of the material,
  • \( A(x) \) is the cross-sectional area normal to the direction of heat transfer,
  • \( \frac{\partial T}{\partial x} \) is the temperature gradient along the x-axis.
In this exercise, because the sides of the cone are insulated, we focus solely on the axial temperature gradient. Fourier's Law guides us in determining how to distribute the heat flow across the varying cross-sectional area of the cone. By rearranging this relationship, we can find the spatial derivative of the temperature, which, when integrated, provides the desired temperature distribution along the cone.
Thermal Conductivity
Thermal conductivity, represented by the symbol \( k \), is a material-specific property that indicates how well it can conduct heat. In our exercise, the cone is made of pure aluminum, a material known for its high thermal conductivity of \( 205 \, \text{W/(m} \cdot \text{K)} \).

Thermal conductivity plays a pivotal role in the equation derived from Fourier's Law. It affects the rate at which heat flows across the cone. Materials with high thermal conductivity, like aluminum, allow heat to move more readily, which directly influences the temperature distribution \( T(x) \). This constant \( k \) remains integral in each step of solving for both the temperature gradient and the overall heat transfer rate \( Q \). By using aluminum's thermal conductivity in our calculations, we align with real-world conditions, ensuring our model accurately reflects the cone's behaviour under the given temperature differences.
Boundary Conditions
Boundary conditions are essential in solving differential equations related to heat transfer because they provide the necessary constraints to find a unique solution. In the case of our truncated cone, the boundary conditions are given by the fixed temperatures at the top and bottom surfaces.

We know:
  • At \( x_1 = 0.075 \, \text{m} \), the temperature \( T_1 = 100^{\circ}C \).
  • At \( x_2 = 0.225 \, \text{m} \), the temperature \( T_2 = 20^{\circ}C \).
These conditions are applied when integrating to find the temperature distribution \( T(x) \). By integrating with these specific temperature boundaries, we ensure that the solution for \( T(x) \) adheres to the physical constraints of the problem, accurately representing how the temperature changes along the length of the cone. The boundary conditions effectively anchor the solution, validating that the mathematical model reflects the actual thermal behaviour of the truncated cone, making the findings both feasible and applicable.

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Most popular questions from this chapter

A thin metallic wire of thermal conductivity \(k\), diameter \(D\), and length \(2 L\) is annealed by passing an electrical current through the wire to induce a uniform volumetric heat generation \(\dot{q}\). The ambient air around the wire is at a temperature \(T_{\infty}\), while the ends of the wire at \(x=\pm L\) are also maintained at \(T_{\infty}\). Heat transfer from the wire to the air is characterized by the convection coefficient \(h\). Obtain expressions for the following: (a) The steady-state temperature distribution \(T(x)\) along the wire, (b) The maximum wire temperature. (c) The average wire temperature.

To maximize production and minimize pumping costs, crude oil is heated to reduce its viscosity during transportation from a production field. (a) Consider a pipe-in-pipe configuration consisting of concentric steel tubes with an intervening insulating material. The inner tube is used to transport warm crude oil through cold ocean water. The inner steel pipe \(\left(k_{s}=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\) has an inside diameter of \(D_{i, 1}=150 \mathrm{~mm}\) and wall thickness \(t_{i}=10 \mathrm{~mm}\) while the outer steel pipe has an inside diameter of \(D_{i, 2}=250 \mathrm{~mm}\) and wall thickness \(t_{o}=t_{i}\). Determine the maximum allowable crude oil temperature to ensure the polyurethane foam insulation \(\left(k_{p}=\right.\) \(0.075 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) between the two pipes does not exceed its maximum service temperature of \(T_{p, \max }=\) \(70^{\circ} \mathrm{C}\). The ocean water is at \(T_{\infty, o}=-5^{\circ} \mathrm{C}\) and provides an external convection heat transfer coefficient of \(h_{o}=500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The convection coefficient associated with the flowing crude oil is \(h_{i}=450 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (b) It is proposed to enhance the performance of the pipe-in-pipe device by replacing a thin \(\left(t_{a}=5 \mathrm{~mm}\right)\) section of polyurethane located at the outside of the inner pipe with an aerogel insulation material \(\left(k_{a}=0.012 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\). Determine the maximum allowable crude oil temperature to ensure maximum polyurethane temperatures are below \(T_{p, \max }=70^{\circ} \mathrm{C}\).

Measurements show that steady-state conduction through a plane wall without heat generation produced a convex temperature distribution such that the midpoint temperature was \(\Delta T_{o}\) higher than expected for a linear temperature distribution. Assuming that the thermal conductivity has a linear dependence on temperature, \(k=k_{o}(1+\alpha T)\), where \(\alpha\) is a constant, develop a relationship to evaluate \(\alpha\) in terms of \(\Delta T_{o}, T_{1}\), and \(T_{2}\).

Consider a plane composite wall that is composed of two materials of thermal conductivities \(k_{\mathrm{A}}=0.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and \(k_{\mathrm{B}}=0.04 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and thicknesses \(L_{\mathrm{A}}=10 \mathrm{~mm}\) and \(L_{\mathrm{B}}=20 \mathrm{~mm}\). The contact resistance at the interface between the two materials is known to be \(0.30 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\). Material A adjoins a fluid at \(200^{\circ} \mathrm{C}\) for which \(h=10\) \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and material \(\mathrm{B}\) adjoins a fluid at \(40^{\circ} \mathrm{C}\) for which \(h=20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) What is the rate of heat transfer through a wall that is \(2 \mathrm{~m}\) high by \(2.5 \mathrm{~m}\) wide? (b) Sketch the temperature distribution.

Consider uniform thermal energy generation inside a one-dimensional plane wall of thickness \(L\) with one surface held at \(T_{s, 1}\) and the other surface insulated. (a) Find an expression for the conduction heat flux to the cold surface and the temperature of the hot surface \(T_{s, 2}\), expressing your results in terms of \(k, \dot{q}, L\), and \(T_{s, 1}\). (b) Compare the heat flux found in part (a) with the heat flux associated with a plane wall without energy generation whose surface temperatures are \(T_{s, 1}\) and \(T_{s, 2}\).

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