/*! 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 60 A recuperator is a heat exchange... [FREE SOLUTION] | 91Ó°ÊÓ

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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 \(U A^{*}\) ?

Short Answer

Expert verified
The percentage fuel savings for the prescribed conditions can be calculated using the outlet temperature of the cold air, which is obtained through the energy balance equation. By calculating the overall heat transfer coefficient (U) and the total surface area (A), temperatures and percentage fuel savings can be plotted as a function of UA. To increase UA without changing the flow rates, some measures include increasing the number of tubes or heat transfer surface area, using a material with higher thermal conductivity, minimizing fouling through maintenance, and improving the convective heat transfer coefficient with inserts or flow channel modifications.

Step by step solution

01

The convective heat transfer coefficient, h (W / m² · K), can be determined using the following correlation for cross-flow over a cylinder: \[ h = 0.36 * (k / L) * Re_L^{0.6}\] In this correlation, k is the thermal conductivity of the fluid (W/m·K), and Re_L is the Reynolds number, which is given by: \[ Re_L = (\rho * V * L ) / \mu \] where \( \rho \) is the fluid density (kg/m³), V is the fluid velocity (m/s), L is the cylinder length (m), and \( \mu \) is the fluid dynamic viscosity (kg/m·s). #Step 2: Calculate overall heat transfer coefficient, U#

Using the formula for overall heat transfer coefficient, U (W/m²·K), in conjunction with the given fouling factor, R': \[ U = 1 / (1/h + R') \] #Step 3: Calculate total surface area, A#
02

The total surface area A (m²) of the silicon carbide tubes can be calculated using the formula: \[ A = N_t * (pi*D*L) \] where N_t is the number of tubes, D is the diameter of the tube, and L is the length of the tube. #Step 4: Calculate the Log Mean Temperature Difference (LMTD) #

For a cross-flow heat exchanger, the LMTD is given by: \[ LMTD = \frac{(T_{h,i} - T_{c,o}) - (T_{h,o} - T_{c,i})}{ln\left((T_{h,i}-T_{c,o})/(T_{h,o}-T_{c,i})\right) }\] where, \(T_{h,i}\) is the inlet temperature of the hot flue gases \(T_{h,o}\) is the outlet temperature of the hot flue gases \(T_{c,i}\) is the inlet temperature of the cold air \(T_{c,o}\) is the outlet temperature of the cold air #Step 5: Calculate energy balance and find T_c_o #
03

Using the energy balance, we can find the outlet temperature of the cold air: \[ \dot{Q} = \dot{m}_c * c_p_c * (T_{c,o} - T_{c,i}) = \dot{m}_h * c_p_h * (T_{h,i} - T_{h,o}) = U*A*LMTD\] #Step 6: Calculate percentage fuel savings for prescribed conditions#

Using the given relationship, we can find the percentage of fuel savings based on the increase in the combustion air temperature: \[ \frac{\Delta T_{c}}"10^{\circ}C" * 1\% = \% \text{fuel savings}\] #Step 7: Calculate the values of T_c_o and percentage fuel savings as a function of UA #
04

Create a range of UA values and compute the following quantities: T_c_o, \% fuel savings, and plot these against UA using the calculated results. #Step 8: Recommend measures for increasing UA#

To increase the value of UA without changing the flow rates, consider the following options: 1. Increase the number of tubes. 2. Increase the heat transfer surface area by making tubes longer or by increasing the number of fins. 3. Use a material with higher thermal conductivity for tubes to reduce the resistance to heat transfer. 4. Minimize fouling by periodic maintenance to keep the fouling factor as low as possible. 5. Improve the convective heat transfer coefficient by using inserts or modifying the flow channels.

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Key Concepts

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

Overall Heat Transfer Coefficient
The overall heat transfer coefficient, often represented by the symbol U, is a measure that demonstrates the ability of a heat exchanger to conduct heat from the hot side to the cold side. It encompasses the resistance to heat transfer in every component part of the heat exchanger system, such as the walls of the tubes, and any fouling that may occur on these surfaces. The formula for calculating this coefficient is:

\[\begin{equation}U = \frac{1}{\frac{1}{h} + R_f}\end{equation}\]
where h is the heat transfer coefficient for convection and Rf is the fouling factor. The latter is a correction factor that accounts for the degradation of performance over time due to the accumulation of unwanted materials on the heat transfer surfaces. Optimizing the overall heat transfer coefficient is crucial because it directly correlates to the heat exchanger’s efficiency. In the given problem, one can increase the value of U by using materials with higher thermal conductivity for the tubes, thus minimizing the resistance.To explore the impact on performance, changes in the U value could be graphed against the outlet temperature of the cold air and the percentage fuel savings. Thus, a practitioner can assess how different materials or designs affect the efficiency of heat exchange in practical scenarios.
Log Mean Temperature Difference (LMTD)
The Log Mean Temperature Difference, abbreviated as LMTD, is integral to the design and analysis of heat exchangers. It represents the driving force behind the heat exchange process and is used to calculate the total heat transfer when the overall heat transfer coefficient is known. The formula for LMTD in a cross-flow heat exchanger with unmixed streams is:

\[\begin{equation}LMTD = \frac{(T_{h,i} - T_{c,o}) - (T_{h,o} - T_{c,i})}{\ln\left(\frac{T_{h,i}-T_{c,o}}{T_{h,o}-T_{c,i}}\right)}\end{equation}\]
Here, Th,i and Th,o are the inlet and outlet temperatures of the hot fluid, respectively, while Tc,i and Tc,o are the inlet and outlet temperatures of the cold fluid, respectively.The significance of LMTD is that it provides a means to address the varying temperature difference along the length of the heat exchanger. In reality, this temperature difference is not constant due to the heat exchange process; thus, the LMTD serves to average the gradient to help estimate the total heat transfer. For students aiming to improve their understanding, concepts like LMTD are critical to grasp, as it directly determines the efficiency of a heat exchanger.
Fouling Factor
Fouling within a heat exchanger is a common issue that can severely impede the system's performance over time. Fouling happens when impurities, such as minerals, biological matter, or corrosion products, accumulate on the heat transfer surfaces. The fouling factor, denoted by Rf, quantifies the thermal resistance introduced by this layer of fouling material. It is essential to consider the fouling factor in the calculation of overall heat transfer coefficient by the equation:\[\begin{equation}U = \frac{1}{\frac{1}{h} + R_f}\end{equation}\]The fouling factor is pivotal when designing the heat exchanger as well as during maintenance planning. By anticipating the fouling factor, designers can ensure that a sufficient surface area is provided to permit effective heat exchange even as fouling develops. Additionally, maintenance procedures can be scheduled to clean and restore surfaces, hence keeping the fouling factor at a manageable level. Incorporating methods such as periodic cleaning or using anti-fouling coatings can help maintain the heat exchanger's efficiency close to its initial capabilities. Therefore, understanding and managing the fouling factor is crucial for sustaining the performance of heat exchanges in practical applications.

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Most popular questions from this chapter

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 \(T_{h i}\) ?

In a dairy operation, milk at a flow rate of \(250 \mathrm{~L} / \mathrm{h}\) and a cow-body temperature of \(38.6^{\circ} \mathrm{C}\) must be chilled to a safe-to-store temperature of \(13^{\circ} \mathrm{C}\) or less. Ground water at \(10^{\circ} \mathrm{C}\) is available at a flow rate of \(0.72 \mathrm{~m}^{3} / \mathrm{h}\). The density and specific heat of milk are \(1030 \mathrm{~kg} / \mathrm{m}^{3}\) and \(3860 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively. (a) Determine the UA product of a counterflow heat exchanger required for the chilling process. Determine the length of the exchanger if the inner pipe has a 50 -mm diameter and the overall heat transfer coefficient is \(U=1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (b) Determine the outlet temperature of the water. (c) Using the value of \(U A\) found in part (a), determine the milk outlet temperature if the water flow rate is doubled. What is the outlet temperature if the flow rate is halved?

A shell-and-tube heat exchanger must be designed to heat \(2.5 \mathrm{~kg} / \mathrm{s}\) of water from 15 to \(85^{\circ} \mathrm{C}\). The heating is to be accomplished by passing hot engine oil, which is available at \(160^{\circ} \mathrm{C}\), through the shell side of the exchanger. The oil is known to provide an average convection coefficient of \(h_{o}=400 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) on the outside of the tubes. Ten tubes pass the water through the shell. Each tube is thin walled, of diameter \(D=25 \mathrm{~mm}\), and makes eight passes through the shell. If the oil leaves the exchanger at \(100^{\circ} \mathrm{C}\), what is its flow rate? How long must the tubes be to accomplish the desired heating?

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.

The oil in an engine is cooled by air in a cross-flow heat exchanger where both fluids are unmixed. Atmospheric air enters at \(30^{\circ} \mathrm{C}\) and \(0.53 \mathrm{~kg} / \mathrm{s}\). Oil at \(0.026 \mathrm{~kg} / \mathrm{s}\) enters at \(75^{\circ} \mathrm{C}\) and flows through a tube of 10-mm diameter. Assuming fully developed flow and constant wall heat flux, estimate the oil- side heat transfer coefficient. If the overall convection coefficient is \(53 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and the total heat transfer area is \(1 \mathrm{~m}^{2}\), determine the effectiveness. What is the exit temperature of the oil?

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