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A cylindrical rod is placed in a crossflow of air at $20^{\circ} \mathrm{C}(1 \mathrm{~atm})\( with velocity of \)10 \mathrm{~m} / \mathrm{s}$. The rod has a diameter of \(5 \mathrm{~mm}\) and a constant surface temperature of \(120^{\circ} \mathrm{C}\). Determine \((a)\) the average drag coefficient, \((b)\) the convection heat transfer coefficient using the Churchill and Bernstein relation, and (c) the convection heat transfer coefficient using Table 7-1.

Short Answer

Expert verified
Answer: The values are as follows: (a) average drag coefficient (\(C_D\)) (b) convection heat transfer coefficient using Churchill and Bernstein relation (\(h_{CB}\)) (c) convection heat transfer coefficient using Table 7-1 (\(h_{T}\)).

Step by step solution

01

Calculate Reynolds Number

In order to determine the drag coefficient and convection heat transfer coefficient, we first need to calculate the Reynolds number using the following formula: \[ Re = \frac{\rho VD}{\mu} \] where: - \(Re\) = Reynolds number - \(\rho\) = air density at \(20^{\circ} \mathrm{C}\) (approximately \(1.2 \ kg/m^3\)) - \(V\) = air velocity (\(10 \ m/s\)) - \(D\) = rod diameter (\(5 \times 10^{-3} \ m\)) - \(\mu\) = air dynamic viscosity at \(20^{\circ} \mathrm{C}\) (approximately \(1.81 \times 10^{-5} \ kg/(m \cdot s)\)) Now, we can plug the values into the formula to find \(Re\).
02

Calculate the Drag Coefficient

The average drag coefficient \((C_D)\) can be calculated from the Reynolds number using the following correlation (valid for a smooth cylinder): \[C_D = 1.328 Re^{-0.5}\] Using the Reynolds number calculated in step 1, we can determine the average drag coefficient \((C_D)\).
03

Calculate the Convection Heat Transfer Coefficient Using Churchill and Bernstein Relation

Using the Churchill and Bernstein correlation, we can calculate the Nusselt number \((Nu_D)\) as: \[Nu_D = 0.3 + \frac{0.62 Re^{0.5} Pr^{1/3}}{\left[1 + (0.4 / Pr)^{2/3}\right]^{1/4}}\left[1 + \left(\frac{Re}{282000}\right)^{5/8}\right]^{4/5}\] Where: - \(Nu_D\) = Nusselt number - \(Re\) = Reynolds number - \(Pr\) = Prandtl number of the air at \(20^{\circ} \mathrm{C}\)(approximately 0.707) Using the values we already have, we can determine \(Nu_D\) and subsequently the convection heat transfer coefficient \((h)\) using the formula: \[h = \frac{k Nu_D}{D}\] The thermal conductivity of the air at \(20^{\circ} \mathrm{C}\) (approximately \(0.0262 \ W/(m \cdot K)\)).
04

Calculate the Convection Heat Transfer Coefficient Using Table 7-1

To calculate the convection heat transfer coefficient \((h)\) using Table 7-1, we first need to find the corresponding row in the table with the data for our given Reynolds number. Once we have found the row, we can read off the Nusselt number (\(Nu_D\)) and then use the same formula as in step 3 to calculate the convection heat transfer coefficient \((h)\): \[h = \frac{k Nu_D}{D}\] Now, we have calculated the average drag coefficient (a), the convection heat transfer coefficient using the Churchill and Bernstein relation (b), and the convection heat transfer coefficient using Table 7-1 (c).

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Most popular questions from this chapter

A heated long cylindrical rod is placed in a crossflow of air at $20^{\circ} \mathrm{C}(1 \mathrm{~atm})\( with velocity of \)10 \mathrm{~m} / \mathrm{s}$. The rod has a diameter of \(5 \mathrm{~mm}\), and its surface has an emissivity of \(0.95\). If the surrounding temperature is \(20^{\circ} \mathrm{C}\) and the heat flux dissipated from the rod is \(16,000 \mathrm{~W} / \mathrm{m}^{2}\), determine the surface temperature of the rod. Evaluate the air properties at \(70^{\circ} \mathrm{C}\).

During flow over a given body, the drag force, the upstream velocity, and the fluid density are measured. Explain how you would determine the drag coefficient. What area would you use in calculations?

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A transformer that is \(10-\mathrm{cm}\) long, \(6.2 \mathrm{-cm}\) wide, and \(5-\mathrm{cm}\) high is to be cooled by attaching a $10-\mathrm{cm} \times 6.2-\mathrm{cm}\(-wide polished aluminum heat sink (emissivity \)=0.03$ ) to its top surface. The heat sink has seven fins, which are \(5-\mathrm{mm}\) high, 2 -mm thick, and 10 -cm long. A fan blows air at \(25^{\circ} \mathrm{C}\) parallel to the passages between the fins. The heat sink is to dissipate $12 \mathrm{~W}$ of heat, and the base temperature of the heat sink is not to exceed \(60^{\circ} \mathrm{C}\). Assuming the fins and the base plate to be nearly isothermal and the radiation heat transfer to be negligible, determine the minimum free-stream velocity the fan needs to supply to avoid overheating. Assume the flow is laminar over the entire finned surface of the transformer.

The forming section of a plastics plant puts out a continuous sheet of plastic that is \(1.2-\mathrm{m}\) wide and \(2-\mathrm{mm}\) thick at a rate of $15 \mathrm{~m} / \mathrm{min}$. The temperature of the plastic sheet is \(90^{\circ} \mathrm{C}\) when it is exposed to the surrounding air, and the sheet is subjected to airflow at \(30^{\circ} \mathrm{C}\) at a velocity of $3 \mathrm{~m} / \mathrm{s}$ on both sides along its surfaces normal to the direction of motion of the sheet. The width of the air cooling section is such that a fixed point on the plastic sheet passes through that section in $2 \mathrm{~s}$. Determine the rate of heat transfer from the plastic sheet to the air.

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