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A spherical shell with thermal conductivity \(k\) has inner and outer radii of \(r_{1}\) and \(r_{2}\), respectively. The inner surface of the shell is subjected to a uniform heat flux of \(\dot{q}_{1}\), while the outer surface of the shell is exposed to convection heat transfer with a coefficient \(h\) and an ambient temperature \(T_{\infty}\). Determine the variation of temperature in the shell wall, and show that the outer surface temperature of the shell can be expressed as $T\left(r_{2}\right)=\left(\dot{q}_{1} / h\right)\left(r_{1} / r_{2}\right)^{2}+T_{\infty}$

Short Answer

Expert verified
Question: Determine the temperature distribution within a spherical shell with given thermal properties and boundary conditions, and show that the outer surface temperature can be expressed as \(T(r_2)=\left(\frac{q_1}{h}\right)\left(\frac{r_1}{r_2}\right)^2 + T_\infty\). Answer: The temperature distribution within a spherical shell with given thermal properties and boundary conditions is given by \(T(r)=-\frac{q_1}{2r_1}\frac{r^2}{2}+\frac{q_1}{2r_2}\ln{r}+T_\infty\), and the outer surface temperature can be expressed as \(T(r_2)=\left(\frac{q_1}{h}\right)\left(\frac{r_1}{r_2}\right)^2 + T_\infty\).

Step by step solution

01

Governing Equation for Heat Transfer in Spherical Coordinates

To determine the temperature distribution, we first need to consider the general heat conduction equation in spherical coordinates: \(\frac{1}{r^{2}}\frac{d}{d r}\left(r^{2} k \frac{d T}{d r}\right)=0\)
02

Simplify the Governing Equation

Since the thermal conductivity k is constant, we can simplify the governing equation further by dividing both sides by k: \(\frac{1}{r^{2}}\frac{d}{d r}\left(r^{2} \frac{d T}{d r}\right)=0\)
03

Integrate the Governing Equation

Integrate the simplified governing equation to obtain the first-order differential equation for temperature: \(\int{\frac{1}{r^{2}}\frac{d}{d r}\left(r^{2} \frac{d T}{d r}\right)dr}=C_{1} \Rightarrow r^{2}\frac{dT}{dr}=C_{1}\) Now, integrate once more to get the temperature distribution function: \(\int{r \frac{dT}{dr}=C_{1} dr} \Rightarrow T(r) = C_{2}\ln{r} + C_{1}\frac{r^2}{2} + C_{3}\)
04

Apply Boundary Conditions

We will now apply the boundary conditions to determine the constants C1, C2, and C3. Boundary condition 1: At r = r1, the heat flux q1 is given: \(q_{1}=-k\left.\frac{dT}{d r}\right|_{r=r_{1}}\). Apply this boundary condition using the given formula, and solve for C1: \(r^{2}\frac{dT}{dr} \Rightarrow 2C_{1}r_{1}= -\dot{q}_{1}\), so \(C_{1} = -\frac{q_{1}}{2r_{1}}\) Boundary condition 2: At r = r2, the convection boundary condition applies: \(-k\left.\frac{dT}{dr}\right|_{r=r_{2}} = h\left[T\left(r_{2}\right) - T_{\infty}\right]\). Apply this boundary condition and substitute C1 into the equation, then solve for C2: \(C_{2} = \frac{q_{1}}{2r_{2}} - h\left[T(r_2) - T_{\infty}\right]\) Boundary condition 3: We don't need to apply another boundary condition since the temperature is obtained through the constants C2 and C3. Thus, the equation for temperature in the shell becomes: \(T\left(r\right)=-\frac{\dot{q}_{1}}{2r_{1}}\frac{r^{2}}{2}+\frac{q_{1}}{2r_{2}}\ln{r}+T_{\infty}\)
05

Show the Outer Surface Temperature Expression

To determine the outer surface temperature of the shell, evaluate the temperature function at r = r2: \(T\left(r_{2}\right)=-\frac{\dot{q}_{1}}{2 \cdot r_{1}}\left(\frac{r_{2}^{2}}{2}\right)+\frac{q_{1}}{2 \cdot r_{2}}\ln{r_{2}}+T_{\infty}\) Now express the equation in the desired form: \(T\left(r_{2}\right)=\left(\frac{\dot{q}_{1}}{h}\right)\left(\frac{r_{1}}{r_{2}}\right)^{2}+T_{\infty}\)

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Most popular questions from this chapter

Consider a 20 -cm-thick concrete plane wall \((k=0.77\) $\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\( subjected to convection on both sides with \)T_{\infty 1}=27^{\circ} \mathrm{C}\( and \)h_{1}=5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( on the inside and \)T_{\infty 22}=8^{\circ} \mathrm{C}$ and \(\mathrm{h}_{2}=12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) on the outside. Assuming constant thermal conductivity with no heat generation and negligible radiation, (a) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the wall, \((b)\) obtain a relation for the variation of temperature in the wall by solving the differential equation, and \((c)\) evaluate the temperatures at the inner and outer surfaces of the wall.

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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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