In a gas-fired boiler, water is being boiled at \(120^{\circ} \mathrm{C}\) by hot air flowing through a 5 -m-long, 5 -cm-diameter tube submerged in water. Hot air enters the tube at 1 atm and \(300^{\circ} \mathrm{C}\) at a mean velocity of \(7 \mathrm{~m} / \mathrm{s}\), and leaves at \(150^{\circ} \mathrm{C}\). If the surface temperature of the tube is \(120^{\circ} \mathrm{C}\), determine the average convection heat transfer coefficient of the air and the rate of water evaporation, in \(\mathrm{kg} / \mathrm{h}\).

Short Answer

Expert verified
Based on the given conditions and calculations for a gas-fired boiler, the average convection heat transfer coefficient of the air is 6465.8 W/m^2.K, and the rate of water evaporation is 2440.4 kg/h.

Step by step solution

01

Calculate the heat capacity rate of air

Find the heat capacity rate of the air, given by \(C_{p,a} = \dot{m}_a \, c_{p,a}\), where \(\dot{m}_a\) is the mass flow rate of air and \(c_{p,a}\) is the specific heat of air at constant pressure (can be taken as 1005 J/kg.K). Firstly, we need to assume air behaves as an ideal gas (which is reasonable at these conditions). Using the ideal gas law at the inlet and outlet, and the mass flow rate continuity equation, we can relate the mass flow rate to the given mean velocity: $$\dot{m}_a = \rho_a A v = \frac{P}{RT_a}A v$$ where \(\rho_a\) is the air density, \(A\) is the tube cross-sectional area, \(v\) is the air velocity, \(P\) is the air pressure, \(R\) is the ideal gas constant for air (287 J/kg.K), and \(T_a\) is the air temperature (300°C = 573.15 K). Now plug in the values: $$\dot{m}_a = \frac{101325}{286.9 \times 573.15} \left(\pi \frac{(0.05)^{2}}{4}\right) 7 = 10.14 \,\text{kg/s}$$ Now, we can find the heat capacity rate of air: $$ C_{p,a} = 10.14 * 1005 = 10204.1 \,\text{W/K} $$
02

Calculate overall heat transfer

Using the given inlet and outlet temperature of the air, we can find the overall heat transfer \(Q\) with the following formula: $$ Q = C_{p,a}(T_{inlet} - T_{outlet}) = 10204.1(573.15 - 423.15) = 1530480 \,\text{W} $$
03

Calculate average convection heat transfer coefficient

Now the heat transfer rate can be related to the temperature difference between the tube's surface temperature and the bulk fluid along with the heat transfer area as follows: $$ Q = h A \Delta T $$ where \(h\) is the average convection heat transfer coefficient, \(A\) is the heat transfer area, and \(\Delta T\) is the temperature difference. $$ h = \frac{Q}{A \Delta T} $$ Here, \(A = \pi d L\) where \(d\) is the diameter, and \(L\) is the length of the tube. Also, \(\Delta T = T_{surface} - T_{outlet} = 120 - 150 = -30^\circ \mathrm{C}\) (note that a negative sign indicates heat transfer from the air to the tube, which is expected). Now plug in the values: $$ h = \frac{1530480}{\pi (0.05) (5) \times -30 } = 6465.8 \,\text{W/m^2.K} $$
04

Calculate the rate of water evaporation

Given the heat transfer rate and the latent heat of vaporization for water \(L_v = 2257\,\text{kJ/kg}\), we can calculate the evaporation rate as: $$ \dot{m}_{water}=\frac{Q}{L_v} $$ $$ \dot{m}_{water}=\frac{1530480}{2257 \times 1000} = 0.6779 \,\text{kg/s} $$ To get the evaporation rate in \(\text{kg/h}\), convert from seconds to hours: $$ \dot{m}_{water} = 0.6779 \times 3600 = 2440.4 \,\text{kg/h} $$ The average convection heat transfer coefficient of the air is \(h = 6465.8 \,\text{W/m^2.K}\) and the rate of water evaporation is 2440.4 kg/h.

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Most popular questions from this chapter

Water at \(10^{\circ} \mathrm{C}\left(\rho=999.7 \mathrm{~kg} / \mathrm{m}^{3}\right.\) and \(\mu=1.307 \times\) \(10^{-3} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\) ) is flowing in a \(0.20\)-cm-diameter 15 -m-long pipe steadily at an average velocity of \(1.2 \mathrm{~m} / \mathrm{s}\). Determine \((a)\) the pressure drop and (b) the pumping power requirement to overcome this pressure drop. Assume flow is fully developed. Is this a good assumption? Answers: (a) \(188 \mathrm{kPa}\), (b) \(0.71 \mathrm{~W}\)

Consider fully developed flow in a circular pipe with negligible entrance effects. If the length of the pipe is doubled, the pressure drop will \((a\) ) double, \((b)\) more than double, \((c)\) less than double, \((d)\) reduce by half, or \((e)\) remain constant.

A metal pipe \(\left(k_{\text {pipe }}=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, D_{i, \text { pipe }}=\right.\) \(5 \mathrm{~cm}, D_{o \text {,pipe }}=6 \mathrm{~cm}\), and \(\left.L=10 \mathrm{~m}\right)\) situated in an engine room is used for transporting hot saturated water vapor at a flow rate of \(0.03 \mathrm{~kg} / \mathrm{s}\). The water vapor enters and exits the pipe at \(325^{\circ} \mathrm{C}\) and \(290^{\circ} \mathrm{C}\), respectively. Oil leakage can occur in the engine room, and when leaked oil comes in contact with hot spots above the oil's autoignition temperature, it can ignite spontaneously. To prevent any fire hazard caused by oil leakage on the hot surface of the pipe, determine the needed insulation \(\left(k_{\text {ins }}=0.95 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\) layer thickness over the pipe for keeping the outer surface temperature below \(180^{\circ} \mathrm{C}\).

Consider a fluid with a Prandtl number of 7 flowing through a smooth circular tube. Using the Colburn, Petukhov, and Gnielinski equations, determine the Nusselt numbers for Reynolds numbers at \(3500,10^{4}\), and \(5 \times 10^{5}\). Compare and discuss the results.

Consider laminar flow in a circular tube. Will the friction factor be higher near the inlet of the tube or near the exit? Why? What would your response be if the flow were turbulent?

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