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 \(k=6 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

Short Answer

Expert verified
Answer: The temperature at a distance of 3.5 mm from the center of the wire is 178.86°C.

Step by step solution

01

The heat generated in the wire due to electric current

The rate at which heat is generated in the wire is given as \(q_g = 5\times 10^7~\text{W}/\text{m}^3\). This heat must be conducted outward through the wire radially.
02

Heat conduction in a radial direction

For radial heat conduction, the equation is given by: \(\frac{d}{dr}(r k \frac{dT}{dr}) + q_g = 0.\) Here, \(r\) is the distance from the center of the wire, \(T\) is the temperature, and \(k\) is the thermal conductivity of the wire.
03

Solving the differential equation

Substitute the value of \(q_g\) and \(k\) into the equation and solve for \(\frac{dT}{dr}\): \(\frac{d}{dr}(r k \frac{dT}{dr}) + 5\times 10^7 = 0\) Integration yields: \(r \frac{dT}{dr} = -\frac{5\times 10^7}{6}{r^2} + C_1\) Next, integrate with respect to \(r\): \(T(r) = -\frac{5\times 10^7}{12}{r^3} + C_1 \ln r +C_2\) Now, we need to apply boundary conditions to get the values of \(C_1\) and \(C_2\).
04

Boundary conditions

At the outer radius (\(r=r_o = 5 \text{ mm} = 5\times 10^{-3}~\text{m}\)), the temperature is \(180^\circ\text{C}\): \(T(r_o) = T(5\times 10^{-3})= 180^\circ\text{C} = 453.15\text{K}\) (converting Celsius to Kelvin) Substitute values into the equation: \(453.15 = -\frac{5\times 10^7}{12}(5\times 10^{-3})^3 + C_1 \ln (5\times 10^{-3}) +C_2\) There is no source of heat at the center of the wire (since it is homogenous). Hence, as \(r \rightarrow 0,\) \(\frac{dT}{dr} \rightarrow 0\): \(0 = -\frac{5\times 10^7}{6}(0)^2 + C_1\) This means \(C_1 = 0\). So we can rewrite temperature equation as: \(T(r) = -\frac{5\times 10^7}{12}{r^3} + C_2\) Now substitute the values again to get \(C_2\): \(453.15 = -\frac{5\times 10^7}{12}(5\times 10^{-3})^3 + C_2\) Solving for \(C_2\), we get \(C_2 = 453.15 + \frac{5\times 10^7}{12}(5\times 10^{-3})^3 = 453.9247\) The temperature equation can now be written as: \(T(r) = -\frac{5\times 10^7}{12}{r^3} + 453.9247\)
05

Calculate temperature at r = 3.5 mm

We are asked to find the temperature at \(r = 3.5\text{~mm} = 3.5\times10^{-3}~\text{m}\). Substitute this value into the temperature equation: \(T(3.5\times10^{-3}) = -\frac{5\times 10^7}{12}(3.5\times 10^{-3})^3 + 453.9247\) Evaluating the expression, we get the temperature in Kelvin: \(T(3.5\times10^{-3}) = 452.009\text{K}\) Now convert the temperature back to Celsius: \(T = 452.009\text{K} - 273.15 = 178.86^\circ\text{C}\) So, the temperature at a radius of \(3.5\text{~mm}\) from the center of the wire is \(178.86^\circ\text{C}\).

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Most popular questions from this chapter

The heat conduction equation in a medium is given in its simplest form as $$ \frac{1}{r} \frac{d}{d r}\left(r k \frac{d T}{d r}\right)+\dot{e}_{\text {gen }}=0 $$ Select the wrong statement below. (a) The medium is of cylindrical shape. (b) The thermal conductivity of the medium is constant. (c) Heat transfer through the medium is steady. (d) There is heat generation within the medium. (e) Heat conduction through the medium is one-dimensional.

The variation of temperature in a plane wall is determined to be \(T(x)=110-60 x\) where \(x\) is in \(\mathrm{m}\) and \(T\) is in \({ }^{\circ} \mathrm{C}\). If the thickness of the wall is \(0.75 \mathrm{~m}\), the temperature difference between the inner and outer surfaces of the wall is (a) \(30^{\circ} \mathrm{C}\) (b) \(45^{\circ} \mathrm{C}\) (c) \(60^{\circ} \mathrm{C}\) (d) \(75^{\circ} \mathrm{C}\) (e) \(84^{\circ} \mathrm{C}\)

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 \(T_{\infty 2}=8^{\circ} \mathrm{C}\) 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.

A plane wall of thickness \(L\) is subjected to convection at both surfaces with ambient temperature \(T_{\infty 1}\) and heat transfer coefficient \(h_{1}\) at inner surface, and corresponding \(T_{\infty 2}\) and \(h_{2}\) values at the outer surface. Taking the positive direction of \(x\) to be from the inner surface to the outer surface, the correct expression for the convection boundary condition is (a) \(\left.k \frac{d T(0)}{d x}=h_{1}\left[T(0)-T_{\mathrm{o} 1}\right)\right]\) (b) \(\left.k \frac{d T(L)}{d x}=h_{2}\left[T(L)-T_{\infty 2}\right)\right]\) (c) \(\left.-k \frac{d T(0)}{d x}=h_{1}\left[T_{\infty 1}-T_{\infty 2}\right)\right]\) (d) \(\left.-k \frac{d T(L)}{d x}=h_{2}\left[T_{\infty 1}-T_{\infty 22}\right)\right]\) (e) None of them

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