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A single-pass heat exchanger is to be designed to heat \(100,000 \mathrm{lbm}\) of water in an hour from \(60^{\circ} \mathrm{F}\) to \(100^{\circ} \mathrm{F}\) by condensation of water vapor at \(230^{\circ} \mathrm{F}\) on the shell side. Each tube has an inner diameter of \(1.2\) in and a wall thickness of \(0.12\) in. The inner surface convection heat transfer coefficient is $480 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}$ and the outer surface convection heat transfer coefficient is $2000 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}$. If the inlet velocity of water $\left(c_{p c}=1 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right.\( and \)\left.\rho=62.3 \mathrm{lbm} / \mathrm{ft}^{3}\right)$ on the tube side is \(4 \mathrm{ft} / \mathrm{s}\), determine the required number of tubes and length of tubes. Assume the thermal resistance of the tubes is negligible.

Short Answer

Expert verified
The designed single-pass heat exchanger will require 139 tubes with a length of 91.50 ft per tube to heat the given water flow from 60°F to 100°F using condensing water vapor.

Step by step solution

01

Calculate the heat transfer needed

First, we need to calculate the heat transfer that needs to occur within the heat exchanger to achieve the desired temperature change in the water. For this, we will use the formula: $$Q = mc_p\Delta T$$ Where: - \(Q\) - Heat transfer [Btu/h] - \(m\) - Mass flow rate of water [lbm/h] - \(c_p\) - Specific heat capacity of water [Btu/lbm °F] - \(\Delta T\) - Temperature difference [°F] Given values: - Mass flow rate: \(100,000\) lbm/h - Initial temperature: \(60\) °F - Final temperature: \(100\) °F - Specific heat capacity: \(1\) Btu/lbm °F (constant) Now, we can calculate the heat transfer needed: $$Q = (100,000\, \mathrm{lbm/h})(1\, \mathrm{Btu/lbm\,°F})(100\, ^\circ\mathrm{F} - 60\,^\circ\mathrm{F}) = 4,000,000\, \mathrm{Btu/h}$$
02

Calculate the heat transfer rate per tube

Now we need to determine the heat transfer rate per tube for both the tube and shell sides. For this, we will use the formula: $$Q_\mathrm{tube}=h_\mathrm{i} A_\mathrm{i} (\Delta T_\mathrm{i})$$ \(Q_\mathrm{tube}\) is the heat transfer rate per tube [Btu/h] \(h_\mathrm{i}\) is the inner convection heat transfer coefficient [Btu/h·ft²·°F] \(A_\mathrm{i}\) is the inner heat transfer area per tube [ft²] \(\Delta T_\mathrm{i}\) is the temperature difference between the two fluids on the tube side [°F] Given values: - Inner surface convection heat transfer coefficient: \(480\, \mathrm{Btu/h\cdot ft^2\cdot °F}\) - Outer surface convection heat transfer coefficient: \(2000\, \mathrm{Btu/h\cdot ft^2\cdot °F}\) - Inlet velocity of water on the tube side: \(4\, \mathrm{ft/s}\) - \(\Delta T_\mathrm{i}\) = \(230\,^\circ\mathrm{F} - 100\,^\circ\mathrm{F} = 130\,^\circ\mathrm{F}\) The calculation for the heat transfer area per tube (A) should consider the tube inner diameter and the length of tubes. However, since the required number of tubes would be determined based on their velocities, and length is unknown yet, we don't need to calculate the actual inner tube surface area at this point. Now, we need to find the volumetric flow rate (\(\dot{V}\)) per tube: $$\dot{V}=\frac{\rho \cdot \dot{m}}{\text{Number of tubes}}$$ Also: $$A_i = \pi D_i L$$ $$\dot{V}=\frac{\pi D_i^2 v}{4}$$ $$\text{Number of tubes} = \frac{4 \cdot \dot{V} \cdot L}{\pi D_i^2v}$$ Now suppose at any time, \(n\) tubes have temperature \(T\), so heat transfer is taking place: $$Q_\mathrm{total} = Q_\mathrm{tube} \cdot \text{Number of tubes}$$ $$ \Rightarrow Q_\mathrm{tube} = \frac{Q_\mathrm{total}\cdot \pi D_i^2v}{4 \cdot \dot{V} \cdot L}$$ Finally, we can substitute the given values and solve for \(\text{Number of tubes}\) and the length \(L\) of the tubes: $$480 \cdot \frac{Q_\mathrm{total}\cdot \pi (1.2\times 10^{-1})^2(4)}{4 \cdot \dot{V} \cdot L} = 130$$ Now, \(L\) is a variable at any stage of the tube, and ultimately: $$\frac{4,000,000\cdot \pi (1.2\times 10^{-1})^2(4)}{4 \cdot \dot{V} \cdot L} = 130$$ Now we have the main equation to find the variable \(\dot{V}\) and ultimately the number of tubes and the length \(L\).
03

Calculate the volumetric flow rate

Given the inlet velocity of water (\(v = 4\, \mathrm{ft/s}\)) and the known tube side density of water (\(\rho=62.3\, \mathrm{lbm/ft^3}\)), we can calculate the volumetric flow rate (\(\dot{V}\)) for water on the tube side: $$\dot{V} = \frac{\dot{m}}{\rho} = \frac{100,000\, \mathrm{lbm/h}}{62.3\, \mathrm{lbm/ft^3}} = 1,\!605.47\, \mathrm{ft^3/h}=0.44624\, \mathrm{ft^3/min}$$
04

Determine the required number of tubes and length of tubes

Now that we have the volumetric flow rate, we will revisit the main equation and determine the required number of tubes and the length of the tubes: $$\frac{4,000,000\, \pi (1.2\times 10^{-1})^2(4)}{4 \cdot 0.44624 \cdot L} = 130$$ We can now solve the equation for \(L\): $$L = \frac{4,000,000\, \pi (1.2\times 10^{-1})^2(4)}{4 \cdot 0.44624 \cdot 130} = 91.503\, \mathrm{ft}$$ As the length \(L\) is given only for four digits of precision, we'll round it up to \(91.50\, \mathrm{ft}\) for the final answer. Now, we can find the number of tubes needed using the L and volumetric flow rate: $$\text{Number of tubes} = \frac{4 \cdot \dot{V} \cdot L}{\pi D_i^2v} = \frac{4 \cdot 0.44624\cdot 91.5}{\pi (1.2\times 10^{-1})^2(4)}$$ The result is: $$\text{Number of tubes} = 138.87$$ Since we cannot have partial tubes, we round up the number of tubes to 139. #Final Answers# The required number of tubes for the heat exchanger design is 139, and the length of each tube is 91.50 ft.

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Most popular questions from this chapter

Write an interactive computer program that will give the effectiveness of a heat exchanger and the outlet temperatures of both the hot and cold fluids when the types of fluids, the inlet temperatures, the mass flow rates, the heat transfer surface area, the overall heat transfer coefficient, and the type of heat exchanger are specified. The program should allow the user to select from the fluids water, engine oil, glycerin, ethyl alcohol, and ammonia. Assume constant specific heats at about room temperature.

Cold water $\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( enters a counterflow heat exchanger at \)18^{\circ} \mathrm{C}\( at a rate of \)0.7 \mathrm{~kg} / \mathrm{s}$ where it is heated by hot air \(\left(c_{p}=1.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) that enters the heat exchanger at \(50^{\circ} \mathrm{C}\) at a rate of $1.6 \mathrm{~kg} / \mathrm{s}\( and leaves at \)25^{\circ} \mathrm{C}$. The maximum possible outlet temperature of the cold water is (a) \(25.0^{\circ} \mathrm{C}\) (b) \(32.0^{\circ} \mathrm{C}\) (c) \(35.5^{\circ} \mathrm{C}\) (d) \(39.7^{\circ} \mathrm{C}\) (e) \(50.0^{\circ} \mathrm{C}\)

Consider a recuperative crossflow heat exchanger (both fluids unmixed) used in a gas turbine system that carries the exhaust gases at a flow rate of $7.5 \mathrm{~kg} / \mathrm{s}\( and a temperature of \)500^{\circ} \mathrm{C}$. The air initially at \(30^{\circ} \mathrm{C}\) and flowing at a rate of $15 \mathrm{~kg} / \mathrm{s}$ is to be heated in the recuperator. The convective heat transfer coefficients on the exhaust gas and air sides are $750 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( and \)300 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$, respectively. Due to long-term use of the gas turbine, the recuperative heat exchanger is subject to fouling on both gas and air sides that offers a resistance of \(0.0004\) \(\mathrm{m}^{2}\). $/ \mathrm{W}$ each. Take the properties of exhaust gas to be the same as that of air \(\left(c_{p}=1069 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\). If the exit temperature of the exhaust gas is \(320^{\circ} \mathrm{C}\), determine \((a)\) if the air could be heated to a temperature of \(150^{\circ} \mathrm{C}\) and \((b)\) the area of the heat exchanger. (c) If the answer to part \((a)\) is no, then determine what should be the air mass flow rate in order to attain the desired exit temperature of \(150^{\circ} \mathrm{C}\) and \((d)\) plot the variation of the exit air temperature over a range of \(75^{\circ} \mathrm{C}\) to \(300^{\circ} \mathrm{C}\) with the air mass flow rate, assuming all the other conditions remain the same.

Consider a heat exchanger in which both fluids have the same specific heats but different mass flow rates. Which fluid will experience a larger temperature change: the one with the lower or higher mass flow rate?

Explain how you can evaluate the outlet temperatures of the cold and hot fluids in a heat exchanger after its effectiveness is determined.

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