/*! 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 21 As part of a senior project, a s... [FREE SOLUTION] | 91Ó°ÊÓ

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As part of a senior project, a student was given the assignment to design a heat exchanger that meets the following specifications: \begin{tabular}{lccc} \hline & \(\dot{m}(\mathrm{~kg} / \mathrm{s})\) & \(T_{m, i}\left({ }^{\circ} \mathrm{C}\right)\) & \(T_{m, \theta}\left({ }^{\circ} \mathrm{C}\right)\) \\ \hline Hot water & 28 & 90 & \(-\) \\ Cold water & 27 & 34 & 60 \\ \hline \end{tabular} Like many real-world situations, the customer hasn't revealed, or doesn't know, additional requirements that would allow you to proceed directly to a final configuration. At the outset, it is helpful to make a first-cut design based upon simplifying assumptions, which can be evaluated to determine what additional requirements and trade-offs should be considered by the customer. (a) Design a heat exchanger to meet the foregoing specifications. List and explain your assumptions. Hint: Begin by finding the required value for \(U A\) and using representative values of \(U\) to determine \(A\). (b) Evaluate your design by identifying what features and configurations could be explored with your customer in order to develop more complete specifications.

Short Answer

Expert verified
In the given heat exchanger problem, we first calculate the heat transfer rate, \(Q\), using mass flow rates and temperature changes of hot and cold water streams. Next, we find the required \(UA\) value for the heat exchanger using the log mean temperature difference, LMTD. Then, we determine the heat transfer area, \(A\), using a representative overall heat transfer coefficient value, \(U\). Finally, we discuss possible improvements and features to explore with the customer to develop more complete specifications, such as varying the overall heat transfer coefficient, flow arrangement, inclusion of fins, and investigating mass flow rate variations.

Step by step solution

01

Calculate the heat transfer rate

Based on the mass flow rates and the temperature changes of the hot and cold water streams, we can calculate the heat transfer rate, \(Q\). The heat transfer rate can be calculated using the formula: \[Q = \dot{m}_{h}C_{p,h}(T_{h,i} - T_{h,f}) = \dot{m}_{c}C_{p,c}(T_{c,f} - T_{c,i})\] Assuming specific heat capacities, \(C_{p,h}\) and \(C_{p,c}\), of water are constant and approximately equal to 4186 J/kg·K, the heat transfer rate can be expressed as follows: \[Q = 28 \times 4186 \times (90 - T_{h,f}) = 27 \times 4186 \times (60 - 34)\] Now, we can calculate the heat transfer rate, \(Q\), and the outlet temperature of the hot water, \(T_{h,f}\).
02

Calculate the required UA value

The heat transfer rate can be expressed as a function of the overall heat transfer coefficient, U, the heat transfer area, A, and the log mean temperature difference, LMTD. \[Q = U A \times LMTD\] LMTD can be calculated using the following formula: \[LMTD = \frac{(T_{h,i}-T_{c,f}) - (T_{h,f}-T_{c,i})}{\ln\left(\frac{T_{h,i}-T_{c,f}}{T_{h,f}-T_{c,i}}\right)}\] First, we will calculate the LMTD value, then we will find the required UA value for the heat exchanger.
03

Determine area A using representative U value

Using a representative overall heat transfer coefficient value, \(U\), we can determine the required heat transfer area, \(A\). \[A = \frac{Q}{U \times LMTD}\] Take a representative value for \(U\) = 1000 W/m²·K, then we can calculate the required area A for the heat exchanger.
04

Discuss improvements and features for specifications

Some features and configurations that could be explored with the customer to develop more complete specifications are: 1. Increasing or decreasing the overall heat transfer coefficient, which may affect the material, type and design of the heat exchanger. 2. Varying the flow arrangement, such as parallel flow, counterflow, or crossflow configurations, which can affect the heat transfer performance. 3. Inclusion of fins or extended surfaces to increase the heat transfer area, thereby improving the heat transfer rate and potentially allowing the use of more compact heat exchangers. 4. Investigating the possibility of varying the mass flow rates of the hot and cold water streams to optimize the heat exchanger. We can work with the customer and explore these features and configurations to fit their requirements better and create a more complete set of specifications.

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Key Concepts

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

Heat Transfer Rate
Understanding the heat transfer rate is essential when designing a heat exchanger. It quantifies the amount of heat moving from the hot to the cold fluid per unit time. The heat transfer rate, denoted by \(Q\), is calculated by the formula:

\[Q = \frac{\dot{m}_h C_{p,h} (T_{h,i} - T_{h,f})}{t} = \frac{\dot{m}_c C_{p,c} (T_{c,f} - T_{c,i})}{t}\]
where \( \dot{m} \) represents mass flow rate, \(C_p\) is the specific heat capacity, and \(T\) denotes temperature, with subscripts \(i\) and \(f\) indicating the initial and final states, respectively. In thermal engineering education, this fundamental concept underpins many principles of heat exchanger performance and its efficiency. Recognizing the balance of the heat transfer rate between the hot and cold water streams is a critical step in heat exchanger design.
Overall Heat Transfer Coefficient
The overall heat transfer coefficient, symbolized by \(U\), embodies the heat exchanger's ability to conduct heat between the fluids through the materials that separate them. This coefficient is crucial in determining the necessary heat transfer area \(A\) for the given heat transfer rate \(Q\). It encompasses all modes of heat transfer including conduction, convection, and any possible radiation components. Typically, \(U\) is derived from empirical correlations or manufacturer data, reflecting how well the exchanger material transmits heat. In industries and thermal engineering education, knowing how to choose or calculate \(U\) is vital for predicting the performance of a heat exchanger.
Log Mean Temperature Difference
The log mean temperature difference (LMTD) is a crucial factor in the design of heat exchangers. It represents an average temperature difference between the hot and cold fluids, accounting for the temperature variation across the heat exchanger. The calculation for LMTD is as follows:

\[LMTD = \frac{(T_{h,i}-T_{c,f}) - (T_{h,f}-T_{c,i})}{\ln\left(\frac{T_{h,i}-T_{c,f}}{T_{h,f}-T_{c,i}}\right)}\]
Determining LMTD is necessary to calculate the required heat transfer area \(A\) once the overall heat transfer coefficient \(U\) and heat transfer rate \(Q\) are known. It is a cornerstone concept for students in thermal engineering education, as it lays the groundwork for more complex calculations involved in optimizing heat exchanger performance.
Heat Exchanger Performance
Evaluating heat exchanger performance involves assessing how effectively it transfers heat under various operating conditions. Notable variables that affect performance include the overall heat transfer coefficient \(U\), the heat transfer area \(A\), and the LMTD. These elements interplay in the fundamental heat exchanger equation \(Q = U \times A \times LMTD\). Through this, engineers can optimize the size and cost of the exchanger against its effectiveness. Enhancements such as fin modifications or flow arrangement changes can significantly affect performance. Understanding the relationship between these variables is crucial for students pursuing thermal engineering education, as it helps with designing efficient thermal systems.
Thermal Engineering Education
Thermal engineering education imparts the foundational principles and practical skills necessary for designing effective heat exchangers. Key concepts include the calculation of heat transfer rate, understanding the influence of the overall heat transfer coefficient, and the importance of LMTD in design. It also covers performance optimization and problem-solving in real-world applications. Effective education in these concepts involves not only theoretical understanding but also the application in exercises like a heat exchanger design project. The integration of theory, calculation, and practical design considerations helps students to develop into proficient thermal engineers who can address diverse industry challenges.

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Most popular questions from this chapter

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.

Hot air for a large-scale drying operation is to be produced by routing the air over a tube bank (unmixed), while products of combustion are routed through the tubes. The surface area of the cross-flow heat exchanger is \(A=25 \mathrm{~m}^{2}\), and for the proposed operating conditions, the manufacturer specifies an overall heat transfer coefficient of \(U=35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The air and the combustion gases may each be assumed to have a specific heat of \(c_{p}=1040 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\). Consider conditions for which combustion gases flowing at \(1 \mathrm{~kg} / \mathrm{s}\) enter the heat exchanger at \(800 \mathrm{~K}\), while air at \(5 \mathrm{~kg} / \mathrm{s}\) has an inlet temperature of \(300 \mathrm{~K}\). (a) What are the air and gas outlet temperatures? (b) After extended operation, deposits on the inner tube surfaces are expected to provide a fouling resistance of \(R_{f}^{N}=0.004 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\). Should operation be suspended in order to clean the tubes? (c) The heat exchanger performance may be improved by increasing the surface area and/or the overall heat transfer coefficient. Explore the effect of such changes on the air outlet temperature for \(500 \leq U A \leq 2500 \mathrm{~W} / \mathrm{K}\).

An energy storage system is proposed to absorb thermal energy collected during the day with a solar collector and release thermal energy at night to heat a building. The key component of the system is a shelland-tube heat exchanger with the shell side filled with \(n\)-octadecane (see Problem 8.47). (a) Warm water from the solar collector is delivered to the heat exchanger at \(T_{h, i}=40^{\circ} \mathrm{C}\) and \(\dot{m}=2 \mathrm{~kg} / \mathrm{s}\) through the tube bundle consisting of 50 tubes, two tube passes, and a tube length per pass of \(L_{l}=2 \mathrm{~m}\). The thin-walled, metal tubes are of diameter \(D=25 \mathrm{~mm}\). Free convection exists within the molten \(n\)-octadecane, providing an average heat transfer coefficient of \(h_{o}=25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) on the outside of each tube. Determine the volume of \(n\) octadecane that is melted over a 12 -h period. If the total volume of \(n\)-octadecane is to be \(50 \%\) greater than the volume melted over \(12 \mathrm{~h}\), determine the diameter of the \(L_{j}=2.2\)-m-long shell. (b) At night, water at \(T_{c, i}=15^{\circ} \mathrm{C}\) is supplied to the heat exchanger, increasing the water temperature and solidifying the \(n\)-octadecane. Do you expect the heat transfer rate to be the same, greater than, or less than the heat transfer rate in part (a)? Explain your reasoning.

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.

Hot water for an industrial washing operation is produced by recovering heat from the flue gases of a furnace. A cross-flow heat exchanger is used, with the gases passing over the tubes and the water making a single pass through the tubes. The steel tubes \((k=60 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) have inner and outer diameters of \(D_{i}=15 \mathrm{~mm}\) and \(D_{o}=20 \mathrm{~mm}\), while the staggered tube array has longitudinal and transverse pitches of \(S_{T}=S_{L}=40 \mathrm{~mm}\). The plenum in which the array is installed has a width (corresponding to the tube length) of \(W=2 \mathrm{~m}\) and a height (normal to the tube axis) of \(H=1.2 \mathrm{~m}\). The number of tubes in the transverse plane is therefore \(N_{T} \approx H / S_{T}=30\). The gas properties may be approximated as those of atmospheric air, and the convection coefficient associated with water flow in the tubes may be approximated as \(3000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) If \(50 \mathrm{~kg} / \mathrm{s}\) of water are to be heated from 290 to \(350 \mathrm{~K}\) by \(40 \mathrm{~kg} / \mathrm{s}\) of flue gases entering the exchanger at \(700 \mathrm{~K}\), what is the gas outlet temperature and how many tube rows \(N_{L}\) are required? (b) The water outlet temperature may be controlled by varying the gas flow rate and/or inlet temperature. For the value of \(N_{L}\) determined in part (a) and the prescribed values of \(H, W, S_{T}, h_{c}\), and \(T_{c, l}\), compute and plot \(T_{c \rho}\) as a function of \(\dot{m}_{h}\) over the range \(20 \leq \dot{m}_{h} \leq 40 \mathrm{~kg} / \mathrm{s}\) for values of \(T_{h u}=500\), 600 , and \(700 \mathrm{~K}\). Also plot the corresponding variations of \(T_{h \rho}\). If \(T_{h, \rho}\) must not drop below \(400 \mathrm{~K}\) to prevent condensation of corrosive vapors on the heat exchanger surfaces, are there any constraints on \(\dot{m}_{\mathrm{h}}\) and \(T_{h i}\) ?

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