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Two very long, slender rods of the same diameter and length are given. One rod (Rod 1) is made of aluminum and has a thermal conductivity $k_{1}=200 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$, but the thermal conductivity of Rod \(2, k_{2}\), is not known. To determine the thermal conductivity of Rod 2 , both rods at one end are thermally attached to a metal surface which is maintained at a constant temperature \(T_{b}\). Both rods are losing heat by convection, with a convection heat transfer coefficient \(h\) into the ambient air at \(T_{\infty}\). The surface temperature of each rod is measured at various distances from the hot base surface. The measurements reveal that the temperature of the aluminum rod (Rod 1) at \(x_{1}=40 \mathrm{~cm}\) from the base is the same as that of the rod of unknown thermal conductivity (Rod 2) at \(x_{2}=20 \mathrm{~cm}\) from the base. Determine the thermal conductivity \(k_{2}\) of the second rod \((\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\).

Short Answer

Expert verified
Answer: The thermal conductivity of Rod 2 is 100 W/mâ‹…K.

Step by step solution

01

Write the one-dimensional heat conduction equation

Since the rods lose heat by convection to the environment, we have the following one-dimensional heat conduction equation for both rods: \(q = k \cdot A \frac{dT}{dx} = h \cdot A \cdot (T_c - T_\infty)\) Where: - \(q\) is the heat transfer rate (\(W\)) - \(k\) is the thermal conductivity of the material (\(W/m\cdot K\)) - \(A\) is the cross-sectional area of the rod (\(m^2\)) - \(dT/dx\) is the temperature gradient along the rod (\(K/m\)) - \(h\) is the convection heat transfer coefficient (\(W/m^2\cdot K\)) - \(T_c\) is the temperature of the rod's surface at a specific position (\(K\)) - \(T_\infty\) is the surrounding air temperature (\(K\))
02

Set up equations for both rods

For Rod 1 (aluminum), the equation becomes: \(q_1 = k_1 \cdot A \frac{dT_1}{dx_1} = h\cdot A\cdot (T_{c1} - T_\infty)\) And for Rod 2 (unknown thermal conductivity), the equation is: \(q_2 = k_2 \cdot A \frac{dT_2}{dx_2} = h\cdot A\cdot (T_{c2} - T_\infty)\) We know that at \(x_1 = 40 cm\) and \(x_2 = 20 cm\), the temperature of Rod 1 and Rod 2 is the same, i.e. \(T_{c1} = T_{c2}\). We can rewrite the equations in terms of the temperature difference between the rods and their base: \(\frac{dT_1}{dx_1} = \frac{q_1}{k_1\cdot A} = \frac{h\cdot A\cdot (T_{c1} - T_\infty)}{k_1\cdot A}\) \(\frac{dT_2}{dx_2} = \frac{q_2}{k_2\cdot A} = \frac{h\cdot A\cdot (T_{c2} - T_\infty)}{k_2\cdot A}\)
03

Set up an equation relating \(k_1\) and \(k_2\)

Since we know the temperature of the rods is the same at the given distances, we can set the temperature gradients equal to each other and solve for the unknown \(k_2\): \(\frac{h\cdot A\cdot (T_{c1} - T_\infty)}{k_1\cdot A} = \frac{h\cdot A\cdot (T_{c2} - T_\infty)}{k_2\cdot A}\) Since \(T_{c1} = T_{c2}\), we can further simplify the equation: \(\frac{T_{c1} - T_\infty}{k_1} = \frac{T_{c2} - T_\infty}{k_2}\) We also know that the distances from the base are \(x_1 = 40 cm\) and \(x_2 = 20 cm\), so the temperature gradients can be written as: \(\frac{dT_1}{dx_1} = 2\cdot \frac{dT_2}{dx_2}\)
04

Solve for the unknown thermal conductivity \(k_2\)

Substituting the temperature gradients into the equation relating \(k_1\) and \(k_2\) gives us: \(2\cdot \frac{T_{c1} - T_\infty}{k_1} = \frac{T_{c2} - T_\infty}{k_2}\) Then, solving for \(k_2\), we get: \(k_2 = k_1 \cdot \frac{T_{c2} - T_\infty}{2\cdot (T_{c1} - T_\infty)}\) Since \(T_{c1} = T_{c2}\), the equation simplifies to: \(k_2 = \frac{k_1}{2}\) Given that \(k_1 = 200 W/m\cdot K\), the thermal conductivity of Rod 2, \(k_2\), is: \(k_2 = \frac{200}{2} = 100 W/m\cdot K\) Thus, the thermal conductivity of the second rod is 100 \(W/m\cdot K\).

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Most popular questions from this chapter

A stainless steel plate $(k=13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, 1 \mathrm{~cm}\( thick \))$ is attached on an ASME SB-96 copper-silicon plate \((k=36 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, 3 \mathrm{~cm}\) thick) to form a plane wall. The bottom surface of the ASME SB-96 plate (surface 1) is subjected to a uniform heat flux of \(750 \mathrm{~W} / \mathrm{m}^{2}\). The top surface of the stainless steel plate (surface 2 ) is exposed to convection heat transfer with air, at \(T_{\infty}=20^{\circ} \mathrm{C}\) and $h=5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, and thermal radiation with the surroundings at \(T_{\text {surr }}=20^{\circ} \mathrm{C}\). The stainless steel surface has an emissivity of \(0.3\). The thermal contact conductance at the interface of stainless steel and coppersilicon plates is $5000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The ASME Boiler and Pressure Vessel Code (ASME BPVC.IV-2015, HF-300) limits equipment constructed with ASME SB-96 plate to be operated at a temperature not exceeding \(93^{\circ} \mathrm{C}\). Determine the total thermal resistance of the wall for an area of $1 \mathrm{~m}^{2}\(, between \)T_{1}\( and \)T_{\infty}$. Would the use of the ASME SB-96 plate under these conditions be in compliance with the ASME Boiler and Pressure Vessel Code?

A 1-cm-diameter, 30-cm-long fin made of aluminum $(k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( is attached to a surface at \)80^{\circ} \mathrm{C}\(. The surface is exposed to ambient air at \)22^{\circ} \mathrm{C}$ with a heat transfer coefficient of $18 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. If the fin can be assumed to be very long, the rate of heat transfer from the fin is (a) \(2.0 \mathrm{~W}\) (b) \(3.2 \mathrm{~W}\) (c) \(4.4 \mathrm{~W}\) (d) \(5.5 \mathrm{~W}\) (e) \(6.0 \mathrm{~W}\)

A turbine blade made of a metal alloy $(k=17 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( has a length of \)5.3 \mathrm{~cm}\(, a perimeter of \)11 \mathrm{~cm}\(, and a crosssectional area of \)5.13 \mathrm{~cm}^{2}$. The turbine blade is exposed to hot gas from the combustion chamber at \(973^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of $538 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The base of the turbine blade maintains a constant temperature of \(450^{\circ} \mathrm{C}\), and the tip is adiabatic. Determine the heat transfer rate to the turbine blade and the temperature at the tip.

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Consider an insulated pipe exposed to the atmosphere. Will the critical radius of insulation be greater on calm days or on windy days? Why?

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