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Consider a cylindrical shell of length \(L\), inner radius \(r_{1}\), and outer radius \(r_{2}\) whose thermal conductivity varies in a specified temperature range as \(k(T)=k_{0}\left(1+\beta T^{2}\right)\) 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 onedimensional heat transfer, obtain a relation for the heat transfer rate through the shell.

Short Answer

Expert verified
#Answer# The heat transfer rate through the cylindrical shell with varying thermal conductivity is given by the formula: $$ Q = k_0 \left[ (T_2-T_1) + \frac{\beta}{3}(T_2^3-T_1^3) \right] $$ Where \(k_0\) is the initial thermal conductivity, \(\beta\) is a constant related to the variation of conductivity with temperature, and \(T_1\) and \(T_2\) are the temperatures at the inner and outer surfaces of the shell, respectively.

Step by step solution

01

Write down the general heat transfer equation for a cylindrical shell

The general heat transfer equation for a cylindrical shell is: $$ \frac{d}{dr}\left( k(r) \frac{dT(r)}{dr} \right) = 0 $$ Where \(k(r)\) is the thermal conductivity, \(r\) is the radial distance, and \(T(r)\) is the temperature as a function of radial distance.
02

Express the thermal conductivity as a function of temperature

We are given that the thermal conductivity varies with temperature as \(k(T)=k_{0}\left(1+\beta T^{2}\right)\). We can substitute it in the above equation: $$ \frac{d}{dr}\left( k(T(r)) \frac{dT(r)}{dr} \right) = 0 $$
03

Solve the differential equation

Let's write the above equation as: $$ \frac{d}{dr}\left[ k(T) \frac{dT}{dr} \right] = \frac{dk(T)}{dT} \frac{dT}{dr} \frac{dT}{dr} = 0 $$ Now, integrate the equation $$ \int_{r_1}^{r_2} \frac{dk(T)}{dT} \frac{dT}{dr} \frac{dT}{dr} dr = 0 $$ Let's assume \(dT(r)=u\) and \(dr=v\). Then, $$ \int_{T_1}^{T_2} k(T) \frac{du}{dv} dv = 0 $$ Now separate and integrate again: $$ \int_{T_1}^{T_2} k(T) dT = \int_{r_1}^{r_2} \frac{du}{dv} dv $$
04

Integrate and apply boundary conditions to find the heat transfer rate

Integrate the left-side of the equation: $$ \int_{T_1}^{T_2} k_0(1+\beta T^{2}) dT = k_0\left[ \left. T\right\rvert_{T_1}^{T_2} + \frac{\beta}{3}\left. T^{3}\right\rvert_{T_1}^{T_2} \right] $$ Integrate the right-side of the equation: $$ \int_{r_1}^{r_2} \frac{du}{dv} dv = Q = \left. u\right\rvert_{r_1}^{r_2} $$ Where Q is the heat transfer rate through the shell. Now we have: $$ k_0 \left[ \left. (T_2-T_1) + \frac{\beta}{3}(T_2^3-T_1^3) \right]\right. = Q $$ So, the relation for the heat transfer rate through the shell is: $$ Q = k_0 \left[ (T_2-T_1) + \frac{\beta}{3}(T_2^3-T_1^3) \right] $$

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Most popular questions from this chapter

Consider steady one-dimensional heat conduction in a plane wall in which the thermal conductivity varies linearly. The error involved in heat transfer calculations by assuming constant thermal conductivity at the average temperature is \((a)\) none, \((b)\) small, or \((c)\) significant.

Consider a large 5 -cm-thick brass plate \((k=111\) $\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\( in which heat is generated uniformly at a rate of \)2 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$. One side of the plate is insulated, while the other side is exposed to an environment at \(25^{\circ} \mathrm{C}\) with a heat transfer coefficient of $44 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$. Explain where in the plate the highest and the lowest temperatures will occur, and determine their values.

Can a differential equation involve more than one independent variable? Can it involve more than one dependent variable? Give examples.

The temperature of a plane wall during steady onedimensional heat conduction varies linearly when the thermal conductivity is constant. Is this still the case when the thermal conductivity varies linearly with temperature?

A large plane wall has a thickness \(L=50 \mathrm{~cm}\) and thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). On the left surface \((x=0)\), it is subjected to a uniform heat flux \(\dot{q}_{0}\) while the surface temperature \(T_{0}\) is constant. On the right surface, it experiences convection and radiation heat transfer while the surface temperature is \(T_{L}=225^{\circ} \mathrm{C}\) and the surrounding temperature is \(25^{\circ} \mathrm{C}\). The emissivity and the convection heat transfer coefficient on the right surface are \(0.7\) and $15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. (a) Show that the variation of temperature in the wall can be expressed as $T(x)=\left(\dot{q}_{0} / k\right)(L-x)+T_{L},(b)\( calculate the heat flux \)\dot{q}_{0}$ on the left face of the wall, and (c) determine the temperature of the left surface of the wall at \(x=0\).

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