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A spherical container of inner radius \(r_{1}=2 \mathrm{~m}\), outer radius \(r_{2}=2.1 \mathrm{~m}\), and thermal conductivity $k=30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\( is filled with iced water at \)0^{\circ} \mathrm{C}$. The container is gaining heat by convection from the surrounding air at \(T_{\infty}=25^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(h=18 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\). Assuming the inner surface temperature of the container to be \(0^{\circ} \mathrm{C},(a)\) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the container, (b) obtain a relation for the variation of temperature in the container by solving the differential equation, and \((c)\) evaluate the rate of heat gain to the iced water.

Short Answer

Expert verified
Answer: The rate of heat gain to the iced water inside the spherical container is 1335 W, and the temperature variation relation is T(r) = -66.75(r^3)/3 + 267.

Step by step solution

01

(a) Differential equation and boundary conditions

The heat conduction equation for a spherical container in steady-state and one-dimensional condition is given by: \( \frac{1}{r^2} \frac{d}{dr}\left( r^2 \frac{dT}{dr} \right) = 0 \) To determine the boundary conditions, we have the following: 1. At the inner surface (r = r1), the temperature is 0°C (T = 0). 2. At the outer surface (r = r2), the rate of heat transfer by convection is equal to the rate of heat transfer by conduction. So, we can write: \( -k \frac{dT}{dr}\Big|_{r=r2} = h(T_{\infty} - T)\Big|_{r=r2} \)
02

(b) Temperature variation relation

To obtain the relation for the variation of temperature, we first solve the differential equation: \( \frac{1}{r^2} \frac{d}{dr}\left( r^2 \frac{dT}{dr} \right) = 0 \) Integrating both sides, we get: \( r^2 \frac{dT}{dr} = C_{1} \) Integrating again, we get: \( T(r) = \frac{C_1}{3}r^3 + C_2 \) Now, we can use the boundary conditions to determine the constants: 1. At r = r1, T = 0: \( 0 = \frac{C_1}{3}r_{1}^{3} + C_2 \) From which, we get: \( C_2 = -\frac{C_1}{3}r_{1}^{3} \) 2. At r = r2: \( -kr_{2}^2 \frac{dT}{dr}\Big|_{r=r2} = h (T_{\infty} - T)\Big|_{r=r2} \) \( -30 (\frac{2.1^3}{3}C_1 - \frac{2^3}{3}C_1) = 18 (25 - (\frac{2.1^3}{3}C_1 - \frac{2^3}{3}C_1)) \) Solving for \(C_1\), we get \(C_1 = -66.75\) and \(C_2 = 267\) Now, we have the temperature variation relation: \( T(r) = -66.75 \frac{r^3}{3} + 267 \)
03

(c) Heat gain rate

To evaluate the rate of heat gain to the iced water, we need to consider the rate of heat transfer through the container at the inner surface (r = r1). We can use the following formula for heat transfer: \( q = -k\frac{dT}{dr}\Big|_{r=r1} \) Now, calculating the heat transfer rate at r1: \( q = -30 \times -66.75 \times \frac{2^2}{3}\, \frac{1}{2} \) \( q = 1335 \,\mathrm{~W} \) Therefore, the rate of heat gain to the iced water is 1335 W.

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Most popular questions from this chapter

Consider a 20-cm-thick large concrete plane wall $(k=0.77 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})$ subjected to convection on both sides with \(T_{\infty 1}=22^{\circ} \mathrm{C}\) and $h_{1}=8 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( on the inside and \)T_{\infty 22}=8^{\circ} \mathrm{C}$ and \(h_{2}=12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) on the outside. Assuming constant thermal conductivity with no heat generation and negligible radiation, \((a)\) express the differential equations 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.

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.

What is the difference between the degree and the order of a derivative?

Consider a long solid cylinder of radius \(r_{o}=4 \mathrm{~cm}\) and thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). Heat is generated in the cylinder uniformly at a rate of $\dot{e}_{\mathrm{gen}}=35 \mathrm{~W} / \mathrm{cm}^{3}$. The side surface of the cylinder is maintained at a constant temperature of \(T_{s}=80^{\circ} \mathrm{C}\). The variation of temperature in the cylinder is given by $$ T(r)=\frac{e_{\mathrm{gen}} r_{o}^{2}}{k}\left[1-\left(\frac{r}{r_{o}}\right)^{2}\right]+T_{s} $$ Based on this relation, determine \((a)\) if the heat conduction is steady or transient, \((b)\) if it is one-, two-, or threedimensional, and \((c)\) the value of heat flux on the side surface of the cylinder at \(r=r_{a r}\)

A long homogeneous resistance wire of radius \(r_{o}=5 \mathrm{~mm}\) is being used to heat the air in a room by the passage of electric current. Heat is generated in the wire uniformly at a rate of $5 \times 10^{7} \mathrm{~W} / \mathrm{m}^{3}$ as a result of resistance heating. If the temperature of the outer surface of the wire remains at \(180^{\circ} \mathrm{C}\), determine the temperature at \(r=3.5 \mathrm{~mm}\) after steady operation conditions are reached. Take the thermal conductivity of the wire to be $k=8 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(. Answer: \)200^{\circ} \mathrm{C}$

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