/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 14 A shell-and-tube exchanger (two ... [FREE SOLUTION] | 91Ó°ÊÓ

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A shell-and-tube exchanger (two shells, four tube passes) is used to heat \(10,000 \mathrm{~kg} / \mathrm{h}\) of pressurized water from 35 to \(120^{\circ} \mathrm{C}\) with \(5000 \mathrm{~kg} / \mathrm{h}\) pressurized water entering the exchanger at \(300^{\circ} \mathrm{C}\). If the overall heat transfer coefficient is \(1500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the required heat exchanger area.

Short Answer

Expert verified
The required heat exchanger area for the given shell-and-tube heat exchanger is approximately 2.480 square meters.

Step by step solution

01

Determine the heat transfer rate for the water stream being heated

First, we need to find the heat transfer rate (Q) required to heat 10,000 kg/h of pressurized water from 35°C to 120°C. We'll use the heat capacity formula: \[Q = m \cdot c_p \cdot \Delta T\] where - \(Q\) = heat transfer rate (W) - \(m\) = mass flow rate (kg/s) - \(c_p\) = specific heat capacity of water (J/kg*K) (We will use 4,184 J/kg*K for water) - \(\Delta T\) = change in temperature (K) First, we need to convert the mass flow rate from kg/h to kg/s by dividing by 3600: \[m = \frac{10000 \mathrm{~kg/h}}{3600 \mathrm{s/h}} = 2.7778 \mathrm{~kg/s}\] Now we can calculate Q: \[Q=2.7778 \mathrm{~kg/s} \times 4,184 \mathrm{~J/kg \cdot K}\times (120-35)^{\circ}\mathrm{C}\]
02

Calculate the heat transfer rate

Now we can calculate the heat transfer rate Q: \[Q = 2.7778 \times 4,184 \times 85 = 985,892 \mathrm{~W}\]
03

Determine the heat exchanger area

Now we need to find the heat exchanger area (A) using the overall heat transfer coefficient (U) and the heat transfer rate (Q) calculated in the previous step. We can use the formula: \[Q = UA\Delta T_{lm}\] where - \(U\) = overall heat transfer coefficient = 1500 W/m²·K - A = heat exchanger area (m²) - \(\Delta T_{lm}\) = log mean temperature difference (K) But first, we need to calculate the log mean temperature difference (\(\Delta T_{lm}\)). We know the temperatures of the cold stream are 35°C and 120°C, while the hot stream enters at 300°C. We can assume the hot stream exits at 120°C since all its heat is transferred to the cold stream. With this information, we can calculate the temperature difference at both ends of the heat exchanger: \[\Delta T_1 = T_{h_1} - T_{c_1} = 300 - 35 = 265^{\circ}\mathrm{C}\] \[\Delta T_2 = T_{h_2} - T_{c_2} = 120 - 120 = 0^{\circ}\mathrm{C}\] Now we can use these values to calculate the log mean temperature difference: \[\Delta T_{lm} = \frac{\Delta T_1 - \Delta T_2}{\ln{\frac{\Delta T_1}{\Delta T_2}}} = \frac{265 - 0}{\ln{\frac{265}{0}}}\] However, since the temperature difference \(\Delta T_2\) is zero, the logarithm cannot be calculated. In this situation, it is reasonable to assume that the heat exchanger is very efficient, and the temperature difference approaches zero. Hence, we can use \(\Delta T_1\) as the log mean temperature difference: \[\Delta T_{lm} \approx 265^{\circ}\mathrm{C}\] Now we can calculate the heat exchanger area (A): \[A = \frac{Q}{U \Delta T_{lm}} = \frac{985,892 \mathrm{~W}}{1500 \mathrm{~W/m^2 \cdot K} \times 265 \mathrm{~K}}\]
04

Calculate the heat exchanger area

Now we can calculate the heat exchanger area A: \[A = \frac{985,892}{1500 \times 265} \approx 2.480 \mathrm{~m^2}\] So the required heat exchanger area is approximately 2.480 square meters.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Shell-and-Tube Exchanger
The shell-and-tube exchanger is one of the most common types of heat exchangers used in various industries. Its design consists of a series of tubes, one set, known as the tube side, contains the fluid that needs heating or cooling, and a second fluid flows over the tubes, inside the shell, to provide or absorb the heat.
This configuration offers a large surface area, making it efficient for heat transfer. Shell-and-tube exchangers can handle high pressures and temperatures and provide good flow distribution. They are typically used when fluid is required to either heat up or cool down rapidly.
A typical shell-and-tube exchanger may have multiple tube passes, meaning the coolant flows back and forth through the tubes several times, thus providing better heat transfer. Having two shells and more tube passes, like in the exercise, allows the system to manage larger volumes of flow and adjust for varied heating requirements.
Log Mean Temperature Difference
The log mean temperature difference (LMTD) is a crucial factor in the design and efficiency calculation of heat exchangers. It accounts for the temperature variance between the hot and cold fluids over the entire length of the heat exchanger.
In our exercise, the LMTD was initially calculated to be problematic as one of the temperature differences (\(\Delta T_2\)) was zero. This indicates that the fluids reached thermal equilibrium, which suggests efficient heat exchange.
The LMTD formula is \[\Delta T_{lm} = \frac{\Delta T_1 - \Delta T_2}{\ln{\frac{\Delta T_1}{\Delta T_2}}}\]where \(\Delta T_1\) and \(\Delta T_2\) are the temperature difference at each end of the exchanger.
When one of the differences is zero, an approximation can be made using just one temperature difference to estimate the LMTD, assuming efficient heat transfer throughout.
Overall Heat Transfer Coefficient
The overall heat transfer coefficient (\(U\)) quantifies the heat transfer capability of the heat exchanger. It encapsulates the combined efficiencies and resistances of all heat transfer processes present between the two fluids in the exchanger.
In the given problem, a value of \(1500~\mathrm{W/m^2\cdot K}\) was used. This coefficient includes factors like the thermal conductivity of the materials, the heat transfer areas, and even the fouling resistance, which may occur due to substance build-up inside the tubes over time.
The calculation for the heat exchanger area involved using this coefficient in the formula \(Q = UA\Delta T_{lm}\), where \(Q\) is the heat transfer rate and \(A\) is the required area. The overall heat transfer coefficient serves as a critical design parameter, ensuring the exchanger is efficient and appropriately sized for the desired thermal performance.

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Most popular questions from this chapter

The chief engineer at a university that is constructing a large number of new student dormitories decides to install a counterflow concentric tube heat exchanger on each of the dormitory shower drains. The thinwalled copper drains are of diameter \(D_{i}=50 \mathrm{~mm}\). Wastewater from the shower enters the heat exchanger at \(T_{h, i}=38^{\circ} \mathrm{C}\) while fresh water enters the dormitory at \(T_{c, l}=10^{\circ} \mathrm{C}\). The wastewater flows down the vertical wall of the drain in a thin, falling \(f\) m , providing \(h_{h}=10,000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) If the annular gap is \(d=10 \mathrm{~mm}\), the heat exchanger length is \(L=1 \mathrm{~m}\), and the water flow rate is \(\dot{m}=10 \mathrm{~kg} / \mathrm{min}\), determine the heat transfer rate and the outlet temperature of the warmed fresh water. (b) If a helical spring is installed in the annular gap so the fresh water is forced to follow a spiral path from the inlet to the fresh water outlet, resulting in \(h_{c}=9050 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the heat transfer rate and the outlet temperature of the fresh water. (c) Based on the result for part (b), calculate the daily savings if 15,000 students each take a 10 -minute shower per day and the cost of water heating is \(\$ 0.07 / \mathrm{kW} \cdot \mathrm{h}\).

A shell-and-tube heat exchanger with one shell pass and 20 tube passes uses hot water on the tube side to heat oil on the shell side. The single copper tube has inner and outer diameters of 20 and \(24 \mathrm{~mm}\) and a length per pass of \(3 \mathrm{~m}\). The water enters at \(87^{\circ} \mathrm{C}\) and \(0.2 \mathrm{~kg} / \mathrm{s}\) and leaves at \(27^{\circ} \mathrm{C}\). Inlet and outlet temperatures of the oil are 7 and \(37^{\circ} \mathrm{C}\). What is the average convection coefficient for the tube outer surface?

Water at a rate of \(45,500 \mathrm{~kg} / \mathrm{h}\) is heated from 80 to \(150^{\circ} \mathrm{C}\) in a heat exchanger having two shell passes and eight tube passes with a total surface area of \(925 \mathrm{~m}^{2}\). Hot exhaust gases having approximately the same thermophysical properties as air enter at \(350^{\circ} \mathrm{C}\) and exit at \(175^{\circ} \mathrm{C}\). Determine the overall heat transfer coefficient.

A cross-flow heat exchanger used in a cardiopulmonary bypass procedure cools blood flowing at \(5 \mathrm{~L} / \mathrm{min}\) from a body temperature of \(37^{\circ} \mathrm{C}\) to \(25^{\circ} \mathrm{C}\) in order to induce body hypothermia, which reduces metabolic and oxygen requirements. The coolant is ice water at \(0^{\circ} \mathrm{C}\), and its flow rate is adjusted to provide an outlet temperature of \(15^{\circ} \mathrm{C}\). The heat exchanger operates with both fluids unmixed, and the overall heat transfer coefficient is \(750 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The density and specific heat of the blood are \(1050 \mathrm{~kg} / \mathrm{m}^{3}\) and \(3740 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively. a) Determine the heat transfer rate for the exchanger. b) Calculate the water flow rate. c) What is the surface area of the heat exchanger? d) Calculate and plot the blood and water outlet temperatures as a function of the water flow rate for the range 2 to \(4 \mathrm{~L} / \mathrm{min}\), assuming all other parameters remain unchanged. Comment on how the changes in the outlet temperatures are affected by changes in the water flow rate. Explain this behavior and why it is an advantage for this application.

A single-pass, cross-flow heat exchanger with both fluids unmixed is being used to heat water \(\left(m_{c}=2 \mathrm{~kg} / \mathrm{s}\right.\), \(c_{p}=4200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\) ) from \(20^{\circ} \mathrm{C}\) to \(100^{\circ} \mathrm{C}\) with hot exhaust gases \(\left(c_{p}=1200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) entering at \(320^{\circ} \mathrm{C}\). What mass flow rate of exhaust gases is required? Assume that UA is equal to its design value of \(4700 \mathrm{~W} / \mathrm{K}\), independent of the gas mass flow rate.

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