Airstream at 1 atm flows, with a velocity of \(15 \mathrm{~m} / \mathrm{s}\), in parallel over a 3-m-long flat plate where there is an unheated starting length of \(1 \mathrm{~m}\). The airstream has a temperature of \(20^{\circ} \mathrm{C}\) and the heated section of the flat plate is maintained at a constant temperature of \(80^{\circ} \mathrm{C}\). Determine \((a)\) the local convection heat transfer coefficient at the trailing edge and (b) the average convection heat transfer coefficient for the heated section.

Short Answer

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Question: Calculate (a) the local convection heat transfer coefficient at the trailing edge and (b) the average convection heat transfer coefficient for the heated section of a flat plate given the following information: Flow velocity = 10 m/s, Length of the flat plate = 3 m, Unheated starting length = 0.5 m, Airstream temperature = 20°C, Heated section temperature = 60°C. Use the Blasius correlation for laminar flow over a flat plate. Answer: (a) The local convection heat transfer coefficient at the trailing edge can be calculated as follows: 1. Calculate the mean temperature: \(T_m = \frac{20 + 60}{2} = 40\)°C 2. Determine the air properties at 40°C: \(\rho\), \(\mu\), \(k\), \(C_p\), and \(\nu\) (refer to air property tables or an online calculator) 3. Calculate the Reynolds number at the trailing edge: \(Re_x = \frac{U_\infty x}{\nu}\) 4. Determine the Nusselt number at the trailing edge using the Blasius correlation: \(Nu_x = 0.332 Re_x^{1/2} Pr^{1/3}\) 5. Calculate the local convection heat transfer coefficient at the trailing edge: \(h_x = \frac{k}{x}Nu_x\) (b) The average convection heat transfer coefficient for the heated section can be calculated as follows: 1. Calculate the average Nusselt number for the heated section using the Petukhov correlation: \(Nu_L = C Re_L^m Pr^n \frac{1}{\left[1 + L_0 / L\right]^{0.75}}\) 2. Calculate the average convection heat transfer coefficient for the heated section: \(h_L = \frac{k}{L}Nu_L\) Remember to use consistent units and the appropriate air properties when performing the calculations.

Step by step solution

01

(Step 1: Calculate the mean temperature of airstream and heated section)

(First, find the mean temperature by averaging the given airstream temperature \(T_\infty\) and heated section temperature \(T_s\). Mean temperature, \(T_m = \frac{T_\infty + T_s}{2}\))
02

(Step 2: Determine the properties of air at the mean temperature)

(Using the mean temperature, find the properties of air like density \(\rho\), dynamic viscosity \(\mu\), thermal conductivity \(k\), specific heat \(C_p\), and kinematic viscosity \(\nu\). You can find these properties in the air property tables or use an online calculator for the same. Remember to use consistent units.)
03

(Step 3: Calculate the Reynolds number at the trailing edge)

(Next, calculate the Reynolds number at the trailing edge, which is at a distance of 3 meters (total length of the flat plate) from the leading edge. The Reynolds number, \(Re_x = \frac{U_\infty x}{\nu}\) Where \(U_\infty\) is the flow velocity, \(x\) is the distance from the leading edge (3 m in this case) and \(\nu\) is the kinematic viscosity.)
04

(Step 4: Determine the Nusselt number at the trailing edge using correlation)

(With the Reynolds number calculated, now we can determine the Nusselt number (\(Nu_x\)) at the trailing edge using an appropriate correlation. Since we have an unheated starting length, the unheated length should be subtracted from the total length before using the correlation. In this case, you can use the Blasius correlation for laminar flow over a flat plate: \(Nu_x = 0.332 Re_x^{1/2} Pr^{1/3}\) Where \(Pr\) is the Prandtl number given by \(Pr = \frac{C_p \mu}{k}\).)
05

(Step 5: Calculate the local convection heat transfer coefficient at the trailing edge)

(Now we can calculate the local convection heat transfer coefficient, \(h_x\), at the trailing edge. \(h_x = \frac{k}{x}Nu_x\))
06

(Step 6: Calculate the average Nusselt number for the heated section)

(Next, we will calculate the average Nusselt number, \(Nu_L\), for the heated section using Petukhov correlation, which accounts for the unheated starting length (\(L_0\)) and heated length \(L\). \(Nu_L = C Re_L^m Pr^n \frac{1}{\left[1 + L_0 / L\right]^{0.75}}\) Where \(Re_L = \frac{U_\infty L}{\nu}\), and \(C\), \(m\), and \(n\) are constants depending on the flow type (for laminar flow, \(C = 0.036\), \(m = 0.8\), and \(n = 0.33\)).)
07

(Step 7: Calculate the average convection heat transfer coefficient for the heated section)

(Finally, we can calculate the average convection heat transfer coefficient, \(h_L\), for the heated section. \(h_L = \frac{k}{L}Nu_L\)) Now, we have successfully found both (a) the local convection heat transfer coefficient at the trailing edge and (b) the average convection heat transfer coefficient for the heated section.

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Most popular questions from this chapter

Exhaust gases at \(1 \mathrm{~atm}\) and \(300^{\circ} \mathrm{C}\) are used to preheat water in an industrial facility by passing them over a bank of tubes through which water is flowing at a rate of \(6 \mathrm{~kg} / \mathrm{s}\). The mean tube wall temperature is \(80^{\circ} \mathrm{C}\). Exhaust gases approach the tube bank in normal direction at \(4.5 \mathrm{~m} / \mathrm{s}\). The outer diameter of the tubes is \(2.1 \mathrm{~cm}\), and the tubes are arranged in- line with longitudinal and transverse pitches of \(S_{L}=S_{T}=8 \mathrm{~cm}\). There are 16 rows in the flow direction with eight tubes in each row. Using the properties of air for exhaust gases, determine \((a)\) the rate of heat transfer per unit length of tubes, \((b)\) and pressure drop across the tube bank, and \((c)\) the temperature rise of water flowing through the tubes per unit length of tubes. Evaluate the air properties at an assumed mean temperature of \(250^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\). Is this a good assumption?

Air at 1 atm and \(20^{\circ} \mathrm{C}\) is flowing over the top surface of a \(0.5-\mathrm{m}\)-long thin flat plate. The air stream velocity is \(50 \mathrm{~m} / \mathrm{s}\) and the plate is maintained at a constant surface temperature of \(180^{\circ} \mathrm{C}\). Determine \((a)\) the average friction coefficient, \((b)\) the average convection heat transfer coefficient, and (c) repeat part (b) using the modified Reynolds analogy.

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