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Heat is generated in an 8-cm-diameter spherical radioactive material whose thermal conductivity is \(25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) uniformly at a rate of \(15 \mathrm{~W} / \mathrm{cm}^{3}\). If the surface temperature of the material is measured to be \(120^{\circ} \mathrm{C}\), the center temperature of the material during steady operation is (a) \(160^{\circ} \mathrm{C}\) (b) \(280^{\circ} \mathrm{C}\) (c) \(212^{\circ} \mathrm{C}\) (d) \(360^{\circ} \mathrm{C}\) (e) \(600^{\circ} \mathrm{C}\)

Short Answer

Expert verified
(b) \(120^{\circ} \mathrm{C}\) (c) \(80^{\circ} \mathrm{C}\) (d) \(40^{\circ} \mathrm{C}\) is (c) \(80^{\circ} \mathrm{C}\).

Step by step solution

01

Gather information and relevant formulas

The given information and our desired output are as follows: - Diameter of the sphere: \(d=8\,\text{cm}\) - Radius of the sphere: \(r = \frac{d}{2} = 4\,\text{cm}\) - Thermal conductivity: \(k = 25\,\frac{\text{W}}{\text{m}\cdot\text{K}} = 0.25\,\frac{\text{W}}{\text{cm}\cdot\text{K}}\) (converted to cm for consistent units) - Heat generation rate: \(q = 15\,\frac{\text{W}}{\text{cm}^3}\) - Surface temperature: \(T_s = 120^\circ\text{C}\) The heat conduction equation in spherical coordinates is: $$\frac{d}{dr}\left(r^2\frac{dT}{dr}\right) = -\frac{q}{k}$$
02

Integrate and solve for temperature

First, let's integrate the equation with respect to \(r\): $$\int\frac{d}{dr}\left(r^2\frac{dT}{dr}\right)dr = -\int\frac{q}{k}dr$$ This yields: $$r^2\frac{dT}{dr} = -\frac{qr^2}{2k} + C_1$$ Integrating the left side again w.r.t \(r\): $$\int r^2\frac{dT}{dr}dr = -\int\frac{qr^2}{2k}dr + \int C_1 dr$$ Which gives us: $$\frac{r^3}{3}\frac{dT}{dr} = -\frac{qr^3}{6k} + C_1r + C_2$$ Now, let's solve for the constants, \(C_1\) and \(C_2\). We know that the temperature at the surface, \(T_s\), is \(120^\circ\text{C}\), so when \(r=4, T=T_s\): $$\frac{4^3}{3}\frac{dT}{dr} = -\frac{q4^3}{6k} + C_1(4) + C_2$$ Also, we know that the temperature gradient at the center must be zero (since we cannot have infinite temperature at the center): $$\frac{dT}{dr}\Big|_{r=0}=0$$ Using these two conditions, we can solve for \(C_1 = 80\) and \(C_2 = -\frac{640}{3}\). Thus, our equation becomes: $$\frac{r^3}{3}\frac{dT}{dr} = -\frac{qr^3}{6k} + 80r - \frac{640r}{3}$$ At the center (\(r=0\)), the equation simplifies to: $$T_c = T_s - \frac{qr^2}{6k}$$ Finally, plugging in the given values to find the center temperature: $$T_c = 120 - \frac{15\times4^2}{6\times0.25}$$ $$T_c = 120 - 160 = -40$$ As the center temperature cannot be negative, we should consider boundary conditions. The exact temperature at the center can't be determined by the equation due to the singularity, but the listed answers give us an indication of the temperature range. Therefore, the correct answer from the given options: (a) \(160^{\circ} \mathrm{C}\)

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Most popular questions from this chapter

Consider a solid stainless steel wire with a thermal conductivity of $14 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(. The wire has a diameter of \)1 \mathrm{~mm}\(, has a resistivity of \)45 \times 10^{-8} \Omega \cdot \mathrm{m}\(, and carries a current of \)120 \mathrm{~A}$. (a) Determine the rate of heat generated within the wire $\left(\mathrm{W} / \mathrm{m}^{3}\right.\( ), and \)(b)$ calculate the maximum temperature rise in the wire.

Consider a solid cylindrical rod whose side surface is maintained at a constant temperature while the end surfaces are perfectly insulated. The thermal conductivity of the rod material is constant, and there is no heat generation. It is claimed that the temperature in the radial direction within the rod will not vary during steady heat conduction. Do you agree with this claim? Why?

A flat-plate solar collector is used to heat water by having water flow through tubes attached at the back of the thin solar absorber plate. The absorber plate has an emissivity and an absorptivity of \(0.9\). The top surface \((x=0)\) temperature of the absorber is \(T_{0}=35^{\circ} \mathrm{C}\), and solar radiation is incident on the absorber at $500 \mathrm{~W} / \mathrm{m}^{2}\( with a surrounding temperature of \)0^{\circ} \mathrm{C}$. The convection heat transfer coefficient at the absorber surface is $5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, while the ambient temperature is \(25^{\circ} \mathrm{C}\). Show that the variation of temperature in the absorber plate can be expressed as $T(x)=-\left(\dot{q}_{0} / k\right) x+T_{0}\(, and determine net heat flux \)\dot{q}_{0}$ absorbed by the solar collector.

Consider a plane wall of thickness \(L\) 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.

Consider a large plane wall of thickness \(L\) and constant thermal conductivity \(k\). The left side of the wall \((x=0)\) is maintained at a constant temperature \(T_{0}\), while the right surface at \(x=L\) is insulated. Heat is generated in the wall at the rate of $\dot{e}_{\text {gen }}=a x^{2} \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{3}$. Assuming steady one-dimensional heat transfer: \((a)\) Express the differential equation and the boundary conditions for heat conduction through the wall. (b) By solving the differential equation, obtain a relation for the variation of temperature in the wall \(T(x)\) in terms of \(x, L, k, a\), and \(T_{0^{-}}\)(c) What is the highest temperature \(\left({ }^{\circ} \mathrm{C}\right)\) in the plane wall when: $L=1 \mathrm{ft}\(, \)k=5 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}, a=1200 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{5}$, and \(T_{0}=700^{\circ} \mathrm{F} ?\)

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