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combustion gases passing through a 5 -cm-internaldiameter circular tube are used to vaporize wastewater at atmospheric pressure. Hot gases enter the tube at \(115 \mathrm{kPa}\) and \(250^{\circ} \mathrm{C}\) at a mean velocity of $5 \mathrm{~m} / \mathrm{s}\( and leave at \)150^{\circ} \mathrm{C}$. If the average heat transfer coefficient is $120 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( and the inner surface temperature of the tube is \)110^{\circ} \mathrm{C}\(, determine \)(a)\( the tube length and \)(b)$ the rate of evaporation of water. Use air properties for the combustion gases.

Short Answer

Expert verified
Answer: The tube length is 0.528 m, and the rate of evaporation of water is 3.95 x 10^-4 kg/s.

Step by step solution

01

Calculate the heat transfer rate between the gases and the tube wall

We are given the average heat transfer coefficient as \(h = 120 \frac{W}{m^2\cdot K}\). The temperature difference between the inner surface of the tube \((110^{\circ}C)\) and the average temperature of the gases can be calculated as \(\Delta T_m = (\frac{T_{i}+T_{o}}{2}) - T_{wall} = (\frac{250+150}{2}) - 110 = 90^{\circ}C\). We can now calculate the heat transfer rate per unit area using the formula: \(q = h \Delta T_m\). Substituting the values, we get: \(q = 120 \cdot 90 = 10800 \frac{W}{m^2}\).
02

Calculate the mass flow rate of the combustion gases

Given the mean velocity of hot gases as \(v = 5 \frac{m}{s}\). Using the ideal gas law, we can find the gas density at the given pressure \((P_{i} = 115\,\mathrm{kPa})\) and temperature \((T_{i} = 250^{\circ}C = 523\,K)\), assuming air to be an ideal gas with the gas constant \(R = 287\,\frac{J}{kg\cdot K}\). We have: \(\rho = \frac{P_{i}}{RT_{i}} = \frac{115000}{287 \cdot 523} = 0.906\,\frac{kg}{m^3}\). Now, we can find the mass flow rate of the combustion gases using the formula: \(\dot{m} = \rho \cdot A_i \cdot v\), where \(A_i\) is the inner area of the tube, and can be found as \(A_i = \pi \cdot (\frac{d}{2})^2 = \pi \cdot (\frac{0.05}{2})^2 = 0.0019635\, m^2\). Substituting the values, we get: \(\dot{m} = 0.906 \cdot 0.0019635 \cdot 5 = 0.00892\,\frac{kg}{s}\).
03

Calculate the tube length

The heat transfer rate per unit length can be calculated as: \(\dot{Q} = \dot{m} \cdot c_p \cdot (T_{i}-T_{o})\), where \(T_{o} = 150^{\circ}C\) is the exit gas temperature. Substituting the values, we get: \(\dot{Q} = 0.00892 \cdot 1000 \cdot (250-150) = 893.6\,W\). Now, we can find the tube length using the formula: \(L = \frac{\dot{Q}}{q \cdot P_i}\), where \(P_i\) is the inner perimeter of the tube, and can be found as \(P_i = \pi \cdot d = \pi \cdot 0.05 = 0.15708\,m\). Substituting the values, we get: \(L = \frac{893.6}{10800 \cdot 0.15708} = 0.528\,m\). Thus, the tube length is \(0.528\,m\).
04

Calculate the rate of evaporation of water

To calculate the rate of evaporation of water, we can use the energy balance equation: \(\dot{Q} = \dot{m}_w \cdot h_{fg}\), where \(\dot{m}_w\) is the mass flow rate of evaporated water, and \(h_{fg}\) is the heat of vaporization of water at atmospheric pressure, which we can assume to be \(h_{fg} = 2.26 \times 10^6\,\frac{J}{kg}\). Substituting the values, we get: \(\dot{m}_w = \frac{\dot{Q}}{h_{fg}} = \frac{893.6}{2.26 \times 10^6} = 3.95 \times 10^{-4}\,\frac{kg}{s}\). Thus, the rate of evaporation of water is \(3.95 \times 10^{-4}\,\frac{kg}{s}\). In conclusion: (a) The tube length is \(0.528\,m\). (b) The rate of evaporation of water is \(3.95 \times 10^{-4}\,\frac{kg}{s}\).

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Most popular questions from this chapter

A 12 -m-long and 12-mm-inner-diameter pipe made of commercial steel is used to heat a liquid in an industrial process. The liquid enters the pipe with \(T_{i}=25^{\circ} \mathrm{C}, V=0.8 \mathrm{~m} / \mathrm{s}\). A uniform heat flux is maintained by an electric resistance heater wrapped around the outer surface of the pipe so that the fluid exits at \(75^{\circ} \mathrm{C}\). Assuming fully developed flow and taking the average fluid properties to be $\rho=1000 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=4000 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\(, \)\mu=2 \times 10^{-3} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}, k=0.48 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$, and \(\mathrm{Pr}=10\), determine: (a) The required surface heat flux \(\dot{q}_{s}\), produced by the heater (b) The surface temperature at the exit, \(T_{s}\) (c) The pressure loss through the pipe and the minimum power required to overcome the resistance to flow.

A house built on a riverside is to be cooled in summer by utilizing the cool water of the river, which flows at an average temperature of $15^{\circ} \mathrm{C}\(. A 15 -m-long section of a circular duct of \)20 \mathrm{~cm}$ diameter passes through the water. Air enters the underwater section of the duct at \(25^{\circ} \mathrm{C}\) at a velocity of \(3 \mathrm{~m} / \mathrm{s}\). Assuming the surface of the duct to be at the temperature of the water, determine the outlet temperature of air as it leaves the underwater portion of the duct. Also, for an overall fan efficiency of 55 percent, determine the fan power input needed to overcome the flow resistance in this section of the duct.

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