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Starting with an energy balance on a cylindrical shell volume element, derive the steady one-dimensional heat conduction equation for a long cylinder with constant thermal conductivity in which heat is generated at a rate of \(\dot{e}_{\text {gen }}\).

Short Answer

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Question: Derive the steady one-dimensional heat conduction equation for a long cylinder with constant thermal conductivity and a heat generation rate within the cylinder. Answer: The steady one-dimensional heat conduction equation for a long cylinder with constant thermal conductivity and heat generation rate \(\dot{e}_{\text {gen }}\) is given by: (d/dr)(k dQ/dr) + \(\dot{e}_{\text {gen }}\)(d(r^2)/dr) = 0

Step by step solution

01

Create the differential cylindrical element

Let's create a cylindrical element with an inner radius r, an outer radius (r+dr), and a length L. The volume of the cylindrical shell ΔV is given by the difference in the volume of the two cylinders: ΔV = π[(r + dr)^2 - r^2]L
02

Calculate the heat generated in the element

If there is a heat generating rate \(\dot{e}_{\text {gen }}\) per unit volume, the total heat generated in the cylindrical shell ΔV is given by: ΔQ_gen = \(\dot{e}_{\text {gen }}\)ΔV
03

Calculate the heat conducted across the element

Using Fourier's law of heat conduction, the rate of heat flow across the inner and outer boundaries of the cylindrical element is given by: q_in = -k(2πrL) (dQ/dr)|_r q_out = -k(2π(r+dr)L) (dQ/dr)|_(r+dr) where k is the constant thermal conductivity.
04

Perform an energy balance on the cylindrical element

Since this is a steady-state system, there is no accumulation of heat within the element. Therefore, the energy balance equation is: Heat conducted into the element + Heat generated in the element = Heat conducted out of the element Which can be rewritten as: q_in + ΔQ_gen = q_out
05

Substitute equations to get the heat conduction equation

Now we substitute the expressions for q_in, q_out, and ΔQ_gen from steps 2 and 3 into the energy balance equation: -k(2πrL) (dQ/dr)|_r + \(\dot{e}_{\text {gen }}\)π[(r + dr)^2 - r^2]L = -k(2π(r+dr)L) (dQ/dr)|_(r+dr)
06

Simplify the equation and remove constants

Now we rearrange and simplify the equation: -k(2πL) [(dQ/dr)|_(r+dr) - (dQ/dr)|_r] = \(\dot{e}_{\text {gen }}\)π[(r + dr)^2 - r^2]L Next, we divide both sides by 2πLΔr to remove the constants and take the limit as dr approaches 0: (1/dr)[-k (dQ/dr)|_(r+dr) + k (dQ/dr)|_r] = (1/dr)[\(\dot{e}_{\text {gen }}\)[(r + dr)^2 - r^2]] In the limit as dr approaches 0: (-d/dr)(k dQ/dr) = \(\dot{e}_{\text {gen }}\) d(r^2)/dr
07

Finalize the heat conduction equation

Rearrange the equation to obtain the one-dimensional heat conduction equation for a long cylinder with constant thermal conductivity and heat generation rate \(\dot{e}_{\text {gen }}\): (d/dr)(k dQ/dr) + \(\dot{e}_{\text {gen }}\)(d(r^2)/dr) = 0 The derived equation represents the heat conduction equation for a long cylinder with constant thermal conductivity and heat generation.

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Most popular questions from this chapter

Consider a short cylinder of radius \(r_{o}\) and height \(H\) in which heat is generated at a constant rate of \(\dot{e}_{\mathrm{gen}}\). Heat is lost from the cylindrical surface at \(r=r_{o}\) by convection to the surrounding medium at temperature \(T_{\infty}\) with a heat transfer coefficient of \(h\). The bottom surface of the cylinder at \(z=0\) is insulated, while the top surface at \(z=H\) is subjected to uniform heat flux \(\dot{q}_{H}\). Assuming constant thermal conductivity and steady two-dimensional heat transfer, express the mathematical formulation (the differential equation and the boundary conditions) of this heat conduction problem. Do not solve.

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Consider a spherical shell of inner radius \(r_{1}\) and outer radius \(r_{2}\) whose thermal conductivity varies linearly in a specified temperature range as \(k(T)=k_{0}(1+\beta T)\) where \(k_{0}\) and \(\beta\) are two specified constants. The inner surface of the shell is maintained at a constant temperature of \(T_{1}\), while the outer surface is maintained at \(T_{2}\). Assuming steady one-dimensional heat transfer, obtain a relation for \((a)\) the heat transfer rate through the shell and (b) the temperature distribution \(T(r)\) in the shell.

A metal spherical tank is filled with chemicals undergoing an exothermic reaction. The reaction provides a uniform heat flux on the inner surface of the tank. The tank has an inner diameter of \(5 \mathrm{~m}\), and its wall thickness is \(10 \mathrm{~mm}\). The tank wall has a variable thermal conductivity given as \(k(T)=k_{0}(1+\beta T)\), where $k_{0}=9.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \beta=0.0018 \mathrm{~K}^{-1}\(, and \)T$ is in \(\mathrm{K}\). The area surrounding the tank has an ambient temperature of \(15^{\circ} \mathrm{C}\), the tank's outer surface experiences convection heat transfer with a coefficient of \(80 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\). Determine the heat flux on the tank's inner surface if the inner surface temperature is \(120^{\circ} \mathrm{C}\).

The variation of temperature in a plane wall is determined to be $T(x)=65 x+25\( where \)x\( is in \)\mathrm{m}\( and \)T\( is in \){ }^{\circ} \mathrm{C}$. If the temperature at one surface is \(38^{\circ} \mathrm{C}\), the thickness of the wall is (a) \(2 \mathrm{~m}\) (b) \(0.4 \mathrm{~m}\) (c) \(0.2 \mathrm{~m}\) (d) \(0.1 \mathrm{~m}\) (e) \(0.05 \mathrm{~m}\)

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