/*! 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

91Ó°ÊÓ

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.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with 91Ó°ÊÓ!

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.

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

An automobile radiator may be viewed as a cross-flow heat exchanger with both fluids unmixed. Water, which has a flow rate of \(0.05 \mathrm{~kg} / \mathrm{s}\), enters the radiator at \(400 \mathrm{~K}\) and is to leave at \(330 \mathrm{~K}\). The water is cooled by air that enters at \(0.75 \mathrm{~kg} / \mathrm{s}\) and \(300 \mathrm{~K}\). (a) If the overall heat transfer coefficient is \(200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), what is the required heat transfer surface area? (b) A manufacturing engineer claims ridges can be stamped on the finned surface of the exchanger, which could greatly increase the overall heat transfer coefficient. With all other conditions remaining the same and the heat transfer surface area determined from part (a), generate a plot of the air and water outlet temperatures as a function of \(U\) for \(200 \leq U \leq 400 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). What benefits result from increasing the overall convection coefficient for this application?

A liquefied natural gas (LNG) regasification facility utilizes a vertical heat exchanger or vaporizer that consists of a shell with a single-pass tube bundle used to convert the fuel to its vapor form for subsequent delivery through a land-based pipeline. Pressurized LNG is off-loaded from an oceangoing tanker to the bottom of the vaporizer at \(T_{c, i}=-155^{\circ} \mathrm{C}\) and \(\dot{m}_{\mathrm{LNG}}=150 \mathrm{~kg} / \mathrm{s}\) and flows through the shell. The pressurized LNG has a vaporization temperature of \(T_{f}=-75^{\circ} \mathrm{C}\) and specific heat \(c_{p l}=4200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\). The specific heat of the vaporized natural gas is \(c_{p, v}=2210 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\) while the gas has a latent heat of vaporization of \(h_{f g}=575 \mathrm{~kJ} / \mathrm{kg}\). The LNG is heated with seawater flowing through the tubes, also introduced at the bottom of the vaporizer, that is available at \(T_{h, i}=20^{\circ} \mathrm{C}\) with a specific heat of \(c_{\mu \mathrm{Sw}}=3985 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\). If the gas is to leave the vaporizer at \(T_{c o}=8^{\circ} \mathrm{C}\) and the seawater is to exit the device at \(T_{\text {hot }}=10^{\circ} \mathrm{C}\), determine the required vaporizer heat transfer area. Hint: Divide the vaporizer into three sections, as shown in the schematic, with \(U_{\mathrm{A}}=150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), \(U_{\mathrm{B}}=260 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and \(U_{\mathrm{C}}=40 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\).

Saturated process steam at 1 atm is condensed in a shell-and-tube heat exchanger (one shell, two tube passes). Cooling water enters the tubes at \(15^{\circ} \mathrm{C}\) with an average velocity of \(3.5 \mathrm{~m} / \mathrm{s}\). The tubes are thin walled and made of copper with a diameter of \(14 \mathrm{~mm}\) and length of \(0.5 \mathrm{~m}\). The convective heat transfer coefficient for condensation on the outer surface of the tubes is \(21,800 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) Find the number of tubes/pass required to condense \(2.3 \mathrm{~kg} / \mathrm{s}\) of steam. (b) Find the outlet water temperature. (c) Find the maximum possible condensation rate that could be achieved with this heat exchanger using the same water flow rate and inlet temperature. (d) Using the heat transfer surface area found in part (a), plot the water outlet temperature and steam condensation rate for water mean velocities in the range from 1 to \(5 \mathrm{~m} / \mathrm{s}\). Assume that the shell-side convection coefficient remains unchanged.

A shell-and-tube heat exchanger consisting of one shell pass and two tube passes is used to transfer heat from an ethylene glycol-water solution (shell side) supplied from a rooftop solar collector to pure water (tube side) used for household purposes. The tubes are of inner and outer diameters \(D_{i}=3.6 \mathrm{~mm}\) and \(D_{o}=3.8 \mathrm{~mm}\), respectively. Each of the 100 tubes is \(0.8 \mathrm{~m}\) long ( \(0.4 \mathrm{~m}\) per pass), and the heat transfer coefficient associated with the ethylene glycol-water mixture is \(h_{o}=11,000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) For pure copper tubes, calculate the heat transfer rate from the ethylene glycol-water solution \(\left(\dot{m}=2.5 \mathrm{~kg} / \mathrm{s}, T_{h, i}=80^{\circ} \mathrm{C}\right)\) to the pure water \((\dot{m}=\) \(2.5 \mathrm{~kg} / \mathrm{s}, T_{c, i}=20^{\circ} \mathrm{C}\) ). Determine the outlet temperatures of both streams of fluid. The density and specific heat of the ethylene glycol-water mixture are \(1040 \mathrm{~kg} / \mathrm{m}^{3}\) and \(3660 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively. (b) It is proposed to replace the copper tube bundle with a bundle composed of high-temperature nylon tubes of the same diameter and tube wall thickness. The nylon is characterized by a thermal conductivity of \(k_{n}=0.31 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). Determine the tube length required to transfer the same amount of energy as in part (a).

A recuperator is a heat exchanger that heats the air used in a combustion process by extracting energy from the products of combustion (the flue gas). Consider using a single-pass, cross-flow heat exchanger as a recuperator. Eighty \((80)\) silicon carbide ceramic tubes \((k=20\) \(\mathrm{W} / \mathrm{m} \cdot \mathrm{K})\) of inner and outer diameters equal to 55 and \(80 \mathrm{~mm}\), respectively, and of length \(L=1.4 \mathrm{~m}\) are arranged as an aligned tube bank of longitudinal and transverse pitches \(S_{L}=100 \mathrm{~mm}\) and \(S_{T}=120 \mathrm{~mm}\), respectively. Cold air is in cross flow over the tube bank with upstream conditions of \(V=1 \mathrm{~m} / \mathrm{s}\) and \(T_{c i}=300 \mathrm{~K}\), while hot flue gases of inlet temperature \(T_{\mathrm{h}, \mathrm{I}}=1400 \mathrm{~K}\) pass through the tubes. The tube outer surface is clean, while the inner surface is characterized by a fouling factor of \(R_{f}^{N \prime}=2 \times 10^{-4} \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\). The air and flue gas flow rates are \(\dot{m}_{c}=1.0 \mathrm{~kg} / \mathrm{s}\) and \(m_{\mathrm{h}}=1.05 \mathrm{~kg} / \mathrm{s}\), respectively. As first approximations, (1) evaluate all required air properties at \(1 \mathrm{~atm}\) and \(300 \mathrm{~K},(2)\) assume the flue gas to have the properties of air at \(1 \mathrm{~atm}\) and \(1400 \mathrm{~K}\), and (3) assume the tube wall temperature to be at \(800 \mathrm{~K}\) for the purpose of treating the effect of variable properties on convection heat transfer. (a) If there is a \(1 \%\) fuel savings associated with each \(10^{\circ} \mathrm{C}\) increase in the temperature of the combustion air \(\left(T_{c o}\right)\) above \(300 \mathrm{~K}\), what is the percentage fuel savings for the prescribed conditions? (b) The performance of the recuperator is strongly influenced by the product of the overall heat transfer coefficient and the total surface area, UA. Compute and plot \(T_{c, \infty}\) and the percentage fuel savings as a function of UA for \(300 \leq U A \leq 600 \mathrm{~W} / \mathrm{K}\). Without changing the flow rates, what measures may be taken to increase \(U A^{*}\) ?

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.