/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 96 A cylindrical shell of inner and... [FREE SOLUTION] | 91Ó°ÊÓ

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A cylindrical shell of inner and outer radii, \(r_{i}\) and \(r_{o}\), respectively, is filled with a heat-generating material that provides a uniform volumetric generation rate \(\left(\mathrm{W} / \mathrm{m}^{3}\right)\) of \(\dot{q}\). The inner surface is insulated, while the outer surface of the shell is exposed to a fluid at \(T_{\infty}\) and a convection coefficient \(h\). (a) Obtain an expression for the steady-state temperature distribution \(T(r)\) in the shell, expressing your result in terms of \(r_{i}, r_{o}, \dot{q}, h, T_{\infty}\), and the thermal conductivity \(k\) of the shell material. (b) Determine an expression for the heat rate, \(q^{\prime}\left(r_{o}\right)\), at the outer radius of the shell in terms of \(\dot{q}\) and shell dimensions.

Short Answer

Expert verified
The steady-state temperature distribution in the shell is given by: \[ T(r) = - \frac{\dot{q}}{6k} r^3 + \frac{\dot{q}}{6k} r_i^2 r + T_\infty - \frac{\dot{q}}{6k}(r_i^2-r_o^2)\] The heat rate at the outer radius is given by: \[ q'(r_o) = \pi\dot{q}r_o\left(\frac{1}{3} r_i^2 - \frac{1}{2} r_o^2\right) \]

Step by step solution

01

Write down the heat equation for a cylindrical coordinate system with heat generation

The equation governing the temperature distribution in a cylindrical coordinate system, in radial direction only and considering the heat generation, is given by: \[\frac{1}{r}\frac{d}{dr}\left(r\frac{dT}{dr}\right) + \frac{\dot{q}}{k} = 0\]
02

Solve the heat equation for T(r)

Let's integrate the equation twice to find the temperature distribution T(r) within the shell. The first integration gives: \[ \int \left( r \frac{dT}{dr} \right) dr = -\int \frac{\dot{q}}{k} r dr + C_1\] \[ r \frac{dT}{dr} = - \frac{\dot{q}}{2k} r^2 + C_1\] Now, we'll integrate it again to get T(r): \[ \int \frac{dT}{dr} dr = - \int \frac{\dot{q}}{2k} r dr + \int C_1 dr\] \[ T(r) = - \frac{\dot{q}}{6k} r^3 + C_1 r + C_2\]
03

Apply the boundary conditions

We have two boundary conditions for this problem: 1. The inner surface is insulated, which means there is no radial heat flux, and so \( \frac{dT}{dr}(r_i) = 0 \). 2. The outer surface of the shell is exposed to a fluid at temperature \(T_\infty\) with a convection coefficient h. Applying the first boundary condition gives us the value of \(C_1\): \[ 0 = - \frac{\dot{q}}{6k} r_i^3 + C_1 r_i\] Hence, \[ C_1 = \frac{\dot{q}}{6k} r_i^2\] For the second boundary condition, we need to use Newton's Law of Cooling at the outer surface: \[ q''(r_o) = -k \frac{dT}{dr}(r_o) = h\left(T(r_o) - T_\infty\right)\]
04

Temperature distribution within the shell

Now we'll substitute \(C_1\) into the temperature distribution formula and simplify: \[ T(r) = - \frac{\dot{q}}{6k} r^3 + \frac{\dot{q}}{6k} r_i^2 r + C_2\] To solve for \(C_2\), we can use Newton's Law of Cooling at the outer surface. Rewrite the temperature distribution formula for \(r = r_o\): \[ T(r_o) - T_\infty = - \frac{\dot{q}}{6k} r_o^3 + \frac{\dot{q}}{6k} r_i^2 r_o + C_2 - T_\infty\] Substitute the Newton's Law of Cooling expression into the equation: \[ \frac{k \frac{dT}{dr}(r_o)}{h} = - \frac{\dot{q}}{6k} r_o^3 + \frac{\dot{q}}{6k} r_i^2 r_o + C_2 - T_\infty\] Differentiate T(r) with respect to r, and evaluate it at \(r=r_o\): \[ \frac{dT}{dr}(r_o) = - \frac{\dot{q}}{2k} r_o^2 + \frac{\dot{q}}{6k} r_i^2\] Substitute the expression for \(\frac{dT}{dr}(r_o)\) in the equation, and solve for \(C_2\): \[ C_2 = T_\infty - \frac{\dot{q}}{6k}(r_i^2-r_o^2)\] Now we have the temperature distribution T(r) within the shell: \[ T(r) = - \frac{\dot{q}}{6k} r^3 + \frac{\dot{q}}{6k} r_i^2 r + T_\infty - \frac{\dot{q}}{6k}(r_i^2-r_o^2)\]
05

Step 5. Calculate heat rate at the outer radius

The heat rate \(q'(r_o)\) can be calculated using the following equation: \[ q'(r_o) = -2\pi r_o k \frac{dT}{dr}(r_o)\] Substitute our previously derived expression for \(\frac{dT}{dr}(r_o)\): \[ q'(r_o) = -2\pi r_o k \left( - \frac{\dot{q}}{2k} r_o^2 + \frac{\dot{q}}{6k} r_i^2 \right)\] Simplify to get the final expression for the heat rate at the outer radius: \[ q'(r_o) = \pi\dot{q}r_o\left(\frac{1}{3} r_i^2 - \frac{1}{2} r_o^2\right) \]

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Key Concepts

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

Steady-State Temperature Distribution
Understanding the steady-state temperature distribution in cylindrical coordinates is crucial when dealing with problems involving long-term heat conduction in systems like pipes, rods, and other cylindrical objects. The term 'steady-state' implies that the temperature at any given point does not change with time. It reaches an equilibrium where the amount of heat entering a particular section is equal to the heat leaving that section.

In a cylindrical shell with uniform volumetric heat generation, as described in the exercise, we're looking for a temperature profile, denoted as \(T(r)\), which should remain constant over time. The inner surface insulation prevents heat from flowing through it, which imposes a boundary condition for our mathematical model. We further apply Newton's Law of Cooling at the shell's outer surface, which interacts with the surrounding fluid.

To make this concept more accessible, think of the cylindrical shell as a circular rod uniformly producing heat along its length. The inner surface acts like a perfect insulator—no heat escapes from it—while the outer surface loses heat to the surrounding environment. Our goal is to understand how the temperature varies from the insulated inner surface to the convective outer surface based on the supplied thermal parameters.
Volumetric Heat Generation
Volumetric heat generation is a common phenomenon in materials that produce heat due to internal mechanisms such as chemical reactions, radioactive decay, or electrical resistance. It refers to the amount of heat produced per unit volume of the material. In the provided exercise, this is depicted by the symbol \(\frac{W}{m^3}\) or \(\dot{q}\).

Let's visualize this concept using a real-world example. Take an electric heater's coil: as electricity passes through the coil, it produces heat. The volumetric heat generation would be the heat produced throughout the volume of the coil. In the case of the cylindrical shell, the heat is assumed to be generated uniformly throughout its volume. This assumption simplifies our calculations, as we can treat the heat generation rate as a constant when solving the heat conduction equation.

In practice, the rate of heat generation can be influenced by various factors such as material properties, the geometry of the material, and the specific mechanisms of heat production. In cases where heat generation is not uniform, the problem becomes more complex and may require a more sophisticated approach to solve.
Radial Heat Conduction Equation
The radial heat conduction equation in cylindrical coordinates is a mathematical expression that describes how heat is transferred radially in a cylindrical object. For problems involving radial symmetry and steady-state conditions, this equation acts as the governing equation for heat conduction.

In essence, the radial heat conduction equation balances the heat flowing through a cylindrical shell with the heat generated inside it. It is derived by applying the law of conservation of energy to a differential volume element in radial coordinates. The equation considers not just the heat flowing in and out of the cylindrical shell but also accounts for any heat being generated or absorbed within the material.

In the exercise, the equation \(\frac{1}{r}\frac{d}{dr}\left(r\frac{dT}{dr}\right) + \frac{\dot{q}}{k} = 0\) is the starting point. Through integration, it yields the temperature distribution function \(T(r)\). Here, \(\dot{q}\) represents the volumetric heat generation, and \(k\) is the material's thermal conductivity—a measure of a material's ability to conduct heat. Finally, the equation is solved subject to the boundary conditions described in the exercise, completing the model that describes radial heat flow in the shell.

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Most popular questions from this chapter

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.

The exposed surface \((x=0)\) of a plane wall of thermal conductivity \(k\) is subjected to microwave radiation that causes volumetric heating to vary as $$ \dot{q}(x)=\dot{q}_{o}\left(1-\frac{x}{L}\right) $$ where \(\dot{q}_{o}\left(\mathrm{~W} / \mathrm{m}^{3}\right)\) is a constant. The boundary at \(x=L\) is perfectly insulated, while the exposed surface is maintained at a constant temperature \(T_{o}\). Determine the temperature distribution \(T(x)\) in terms of \(x, L, k, \dot{q}_{o}\), and \(T_{o}\).

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 \(T_{2}=20^{\circ} \mathrm{C}\) ?

A rod of diameter \(D=25 \mathrm{~mm}\) and thermal conductivity \(k=60 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) protrudes normally from a furnace wall that is at \(T_{w}=200^{\circ} \mathrm{C}\) and is covered by insulation of thickness \(L_{\text {ins }}=200 \mathrm{~mm}\). The rod is welded to the furnace wall and is used as a hanger for supporting instrumentation cables. To avoid damaging the cables, the temperature of the rod at its exposed surface, \(T_{o}\), must be maintained below a specified operating limit of \(T_{\max }=100^{\circ} \mathrm{C}\). The ambient air temperature is \(T_{\infty}=\) \(25^{\circ} \mathrm{C}\), and the convection coefficient is \(h=15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) Derive an expression for the exposed surface temperature \(T_{o}\) as a function of the prescribed thermal and geometrical parameters. The rod has an exposed length \(L_{o}\), and its tip is well insulated. (b) Will a rod with \(L_{o}=200 \mathrm{~mm}\) meet the specified operating limit? If not, what design parameters would you change? Consider another material, increasing the thickness of the insulation, and increasing the rod length. Also, consider how you might attach the base of the rod to the furnace wall as a means to reduce \(T_{o}\).

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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