Air \((\operatorname{Pr}=0.7, k=0.026 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) at \(200^{\circ} \mathrm{C}\) flows across 2-cm-diameter tubes whose surface temperature is \(50^{\circ} \mathrm{C}\) with a Reynolds number of 8000 . The Churchill and Bernstein convective heat transfer correlation for the average Nusselt number in this situation is $$ \mathrm{Nu}=0.3+\frac{0.62 \mathrm{Re}^{0.5} \mathrm{Pr}^{0.33}}{\left[1+(0.4 / \mathrm{Pr})^{0.67}\right]^{0.25}} $$ (a) \(8.5 \mathrm{~kW} / \mathrm{m}^{2}\) (b) \(9.7 \mathrm{~kW} / \mathrm{m}^{2}\) (c) \(10.5 \mathrm{~kW} / \mathrm{m}^{2}\) (d) \(12.2 \mathrm{~kW} / \mathrm{m}^{2}\) (e) \(13.9 \mathrm{~kW} / \mathrm{m}^{2}\)

Short Answer

Expert verified
Question: Calculate the convective heat transfer rate between the air and the surface of the 2-cm-diameter tubes given that the temperature of the air is 50°C, the temperature of the tubes is 200°C, the properties of air are \(k = 0.026\,\mathrm{W}/\mathrm{m}\cdot\mathrm{K}\) and \(Pr = 0.7\), the Reynolds number is 8000, and the Churchill and Bernstein convective heat transfer correlation is given. Choose the correct answer from the following options: (a) 10.2 \(kW/m^2\) (b) 11.7 \(kW/m^2\) (c) 12.3 \(kW/m^2\) (d) 13.4 \(kW/m^2\) (e) 13.9 \(kW/m^2\). Answer: (e) 13.9 \(kW/m^2\)

Step by step solution

01

Calculate the average Nusselt number using the Churchill and Bernstein correlation

First, input the known values into the Churchill and Bernstein correlation for average Nusselt number given below: $$ \mathrm{Nu} = 0.3 + \frac{0.62 \cdot \mathrm{Re}^{0.5} \cdot \mathrm{Pr}^{0.33}}{\left[1 + (0.4/\mathrm{Pr})^{0.67}\right]^{0.25}} $$ Substitute \(\mathrm{Re} = 8000\) and \(\mathrm{Pr} = 0.7\): $$ \mathrm{Nu} = 0.3 + \frac{0.62 \cdot 8000^{0.5} \cdot 0.7^{0.33}}{\left[1 + (0.4/0.7)^{0.67}\right]^{0.25}} $$ Then, calculate the Nusselt number: $$ \mathrm{Nu} \approx 71.033 $$
02

Calculate the heat transfer coefficient, h

Now that we have the Nusselt number, we can find the heat transfer coefficient (\(h\)) using the following formula: $$ h = \frac{\mathrm{Nu} \cdot k}{D} $$ Substitute \(\mathrm{Nu} \approx 71.033\), \(k = 0.026 \frac{\mathrm{W}}{\mathrm{m}\cdot\mathrm{K}}\), and \(D = 0.02\,\mathrm{m}\): $$ h \approx \frac{71.033 \cdot 0.026}{0.02} \\ h \approx 92.5 \frac{\mathrm{W}}{\mathrm{m}^2\cdot\mathrm{K}} $$
03

Calculate the heat transfer rate, q"

Finally, we can find the heat transfer rate (\(q''\)) using the following formula: $$ q'' = h \cdot (\Delta T) $$ Substitute \(h \approx 92.5 \frac{\mathrm{W}}{\mathrm{m}^2\cdot\mathrm{K}}\) and \(\Delta T = 200^{\circ}\mathrm{C} - 50^{\circ}\mathrm{C} = 150^{\circ}\mathrm{C}\): $$ q'' \approx 92.5 \cdot 150 $$ Now, convert the heat transfer rate to \(\mathrm{kW}/\mathrm{m}^2\): $$ q'' \approx \frac{92.5 \cdot 150}{1000} \approx 13.875 \,\mathrm{kW}/\mathrm{m}^2 $$ Comparing the calculated heat transfer rate with the given options, we find that the closest answer is (e) \(13.9\,\mathrm{kW}/\mathrm{m}^2\).

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Most popular questions from this chapter

Air (1 atm, \(\left.5^{\circ} \mathrm{C}\right)\) with free stream velocity of \(2 \mathrm{~m} / \mathrm{s}\) flows in parallel to a stationary thin \(1 \mathrm{~m} \times 1 \mathrm{~m}\) flat plate over the top and bottom surfaces. The flat plate has a uniform surface temperature of \(35^{\circ} \mathrm{C}\). Determine \((a)\) the average friction coefficient, \((b)\) the average convection heat transfer coefficient, and \((c)\) the average convection heat transfer coefficient using the modified Reynolds analogy and compare with the result obtained in \((b)\).

A \(1.8\)-m-diameter spherical tank of negligible thickness contains iced water at \(0^{\circ} \mathrm{C}\). Air at \(25^{\circ} \mathrm{C}\) flows over the tank with a velocity of \(7 \mathrm{~m} / \mathrm{s}\). Determine the rate of heat transfer to the tank and the rate at which ice melts. The heat of fusion of water at \(0^{\circ} \mathrm{C}\) is \(333.7 \mathrm{~kJ} / \mathrm{kg}\).

What is flow separation? What causes it? What is the effect of flow separation on the drag coefficient?

Air at 1 atm is flowing in parallel over a \(3-\mathrm{m}-\) long flat plate with a velocity of \(7 \mathrm{~m} / \mathrm{s}\). The air has a free stream temperature of \(120^{\circ} \mathrm{C}\) and the surface temperature of the plate is maintained at \(20^{\circ} \mathrm{C}\). Determine the distance \(x\) from the leading edge of the plate where the critical Reynolds number \(\left(\operatorname{Re}_{c r}=5 \times 10^{5}\right)\) is reached. Then, using the EES (or other) software, evaluate the local convection heat transfer coefficient along the plate. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local convection heat transfer coefficient as a function of \(x\), and discuss the results.

Air at \(20^{\circ} \mathrm{C}\) flows over a 4-m-long and 3-m-wide surface of a plate whose temperature is \(80^{\circ} \mathrm{C}\) with a velocity of \(5 \mathrm{~m} / \mathrm{s}\). The rate of heat transfer from the laminar flow region of the surface is (a) \(950 \mathrm{~W}\) (b) \(1037 \mathrm{~W}\) (c) \(2074 \mathrm{~W}\) (d) \(2640 \mathrm{~W}\) (e) \(3075 \mathrm{~W}\) (For air, use \(k=0.02735 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7228, \nu=1.798 \times\) \(10^{-5} \mathrm{~m}^{2} / \mathrm{s}\) )

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