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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

An air heater consists of a steel tube \((k=20 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\), with inner and outer radii of \(r_{1}=13 \mathrm{~mm}\) and \(r_{2}=16\) \(\mathrm{mm}\), respectively, and eight integrally machined longitudinal fins, each of thickness \(t=3 \mathrm{~mm}\). The fins extend to a concentric tube, which is of radius \(r_{3}=\) \(40 \mathrm{~mm}\) and insulated on its outer surface. Water at a temperature \(T_{\infty, i}=90^{\circ} \mathrm{C}\) flows through the inner tube, while air at \(T_{\infty, o}=25^{\circ} \mathrm{C}\) flows through the annular region formed by the larger concentric tube. (a) Sketch the equivalent thermal circuit of the heater and relate each thermal resistance to appropriate system parameters. (b) If \(h_{i}=5000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(h_{o}=200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), what is the heat rate per unit length? (c) Assess the effect of increasing the number of fins \(N\) and/or the fin thickness \(t\) on the heat rate, subject to the constraint that \(N t<50 \mathrm{~mm}\).

One modality for destroying malignant tissue involves imbedding a small spherical heat source of radius \(r_{o}\) within the tissue and maintaining local temperatures above a critical value \(T_{c}\) for an extended period. Tissue that is well removed from the source may be assumed to remain at normal body temperature \(\left(T_{b}=37^{\circ} \mathrm{C}\right)\). Obtain a general expression for the radial temperature distribution in the tissue under steady- state conditions for which heat is dissipated at a rate \(q\). If \(r_{o}=0.5 \mathrm{~mm}\), what heat rate must be supplied to maintain a tissue temperature of \(T \geq T_{c}=42^{\circ} \mathrm{C}\) in the domain \(0.5 \leq r \leq\) \(5 \mathrm{~mm}\) ? The tissue thermal conductivity is approximately \(0.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). Assume negligible perfusion.

An uninsulated, thin-walled pipe of \(100-\mathrm{mm}\) diameter is used to transport water to equipment that operates outdoors and uses the water as a coolant. During particularly harsh winter conditions, the pipe wall achieves a temperature of \(-15^{\circ} \mathrm{C}\) and a cylindrical layer of ice forms on the inner surface of the wall. If the mean water temperature is \(3^{\circ} \mathrm{C}\) and a convection coefficient of \(2000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) is maintained at the inner surface of the ice, which is at \(0^{\circ} \mathrm{C}\), what is the thickness of the ice layer?

The outer surface of a hollow sphere of radius \(r_{2}\) is subjected to a uniform heat flux \(q_{2}^{\prime \prime}\). The inner surface at \(r_{1}\) is held at a constant temperature \(T_{s, 1}\). (a) Develop an expression for the temperature distribution \(T(r)\) in the sphere wall in terms of \(q_{2}^{\prime \prime}, T_{s, 1}, r_{1}, r_{2}\), and the thermal conductivity of the wall material \(k\). (b) If the inner and outer tube radii are \(r_{1}=50 \mathrm{~mm}\) and \(r_{2}=100 \mathrm{~mm}\), what heat flux \(q_{2}^{\prime \prime}\) is required to maintain the outer surface at \(T_{s, 2}=50^{\circ} \mathrm{C}\), while the inner surface is at \(T_{s, 1}=20^{\circ} \mathrm{C}\) ? The thermal conductivity of the wall material is \(k=10 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

A very long rod of \(5-\mathrm{mm}\) diameter and uniform thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) is subjected to a heat treatment process. The center, 30 -mm-long portion of the rod within the induction heating coil experiences uniform volumetric heat generation of \(7.5 \times 10^{6} \mathrm{~W} / \mathrm{m}^{3}\). The unheated portions of the rod, which protrude from the heating coil on either side, experience convection with the ambient air at \(T_{\infty}=20^{\circ} \mathrm{C}\) and \(h=10 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Assume that there is no convection from the surface of the rod within the coil. (a) Calculate the steady-state temperature \(T_{o}\) of the rod at the midpoint of the heated portion in the coil. (b) Calculate the temperature of the rod \(T_{b}\) at the edge of the heated portion.

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