/*! 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 39 A cross-flow heat exchanger used... [FREE SOLUTION] | 91Ó°ÊÓ

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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.

Short Answer

Expert verified
The heat transfer rate for the exchanger is \(36688.4 \text{ W}\). The water flow rate is approximately \(11.078 \mathrm{~L} / \mathrm{min}\). The surface area of the heat exchanger is approximately \(2.094 \text{ m}^2\). For the blood and water outlet temperatures as a function of the water flow rate, we would need to use software like MATLAB or Python to calculate and plot the results. However, we can expect that an increase in water flow rate would lower the blood outlet temperature and bring the water outlet temperature closer to the blood outlet temperature, allowing better temperature control and potentially a more efficient heat exchange.

Step by step solution

01

a) Determine the heat transfer rate for the exchanger

First, we need to find the mass flow rate of the blood. To do this, we can use the following formula: Mass flow rate = Density × Flow rate The flow rate of blood is given as 5 L/min which needs to be converted to m³/s: \(5 \frac{\text{L}}{\text{min}} \cdot \frac{1 \text{ m}^3}{1000 \text{ L}} \cdot \frac{1 \text{min}}{60 \text{s}} = 8.33 × 10^{-5} \frac{\text{m}^3}{\text{s}}\) Now we can find the mass flow rate of blood: \(m_{blood} = \rho_{blood} \cdot Q_{blood} = 1050 \frac{\text{kg}}{\text{m}^3} \cdot 8.33 × 10^{-5} \frac{\text{m}^3}{\text{s}} = 0.08745 \frac{\text{kg}}{\text{s}}\) Next, we can use the specific heat and the temperature difference to find the heat transfer rate for the exchanger: \[q = m_{blood} \cdot c_{p,blood} \cdot (T_{in,blood} - T_{out,blood})\] Plugging the values in the above equation, we get: \(q = 0.08745 \frac{\text{kg}}{\text{s}} \cdot 3740 \frac{\text{J}}{\text{kg⋅K}} \cdot (37^\circ\text{C} - 25^\circ\text{C}) = 36688.4 \text{ W}\) So, the heat transfer rate for the exchanger is \(36688.4 \text{ W}\).
02

b) Calculate the water flow rate

In order to find the water flow rate, we first need to determine the mass flow rate of water. We can use the energy balance equation: \(q = m_{water} \cdot c_{p,water} \cdot (T_{out,water} - T_{in,water})\) where \(c_{p,water} = 4186 \frac{\text{J}}{\text{kg⋅K}}\) (average specific heat of water in the given temperature range) Rearranging the equation to solve for the mass flow rate of water: \(m_{water} = \frac{q}{c_{p,water} \cdot (T_{out,water} - T_{in,water})} = \frac{36688.4 \text{ W}}{4186 \frac{\text{J}}{\text{kg⋅K}} \cdot (15^\circ\text{C} - 0^\circ\text{C})} = 0.1846 \frac{\text{kg}}{\text{s}}\) Now, we can convert the mass flow rate of water back to a volumetric flow rate using the density of water (assume \(1000 \frac{\text{kg}}{\text{m}^3}\) at these temperatures): \(Q_{water} = \frac{m_{water}}{\rho_{water}} = \frac{0.1846 \frac{\text{kg}}{\text{s}}}{1000 \frac{\text{kg}}{\text{m}^3}} = 1.846 × 10^{-4} \frac{\text{m}^3}{\text{s}}\) Converting to L/min, we get: \(1.846 × 10^{-4} \frac{\text{m}^3}{\text{s}} \cdot \frac{1000 \text{ L}}{1 \text{ m}^3} \cdot \frac{60 \text{s}}{1 \text{min}} = 11.078 \frac{\text{L}}{\text{min}}\) So, the water flow rate is approximately \(11.078 \mathrm{~L} / \mathrm{min}\).
03

c) Calculate the surface area of the heat exchanger

We can use the following equation to find the surface area of the heat exchanger: \(q = U \cdot A \cdot \Delta T_{lm}\) where \(U = 750 \frac{\text{W}}{\text{m}^2\cdot\text{K}}\) is the overall heat transfer coefficient, \(A\) is the surface area and \(\Delta T_{lm}\) is the log mean temperature difference. The log mean temperature difference can be calculated as follows: \(\Delta T_{lm} = \frac{(\Delta T_1 - \Delta T_2)}{\ln{(\frac{\Delta T_1}{\Delta T_2})}}\) where \(\Delta T_1 = T_{in,blood} - T_{out,water} = 37^\circ\text{C} - 15^\circ\text{C}\) \(\Delta T_2 = T_{out,blood} - T_{in,water} = 25^\circ\text{C} - 0^\circ\text{C}\) Calculating the log mean temperature difference, we get: \(\Delta T_{lm} = \frac{(22^\circ\text{C} - 25^\circ\text{C})}{\ln{(\frac{22^\circ\text{C}}{25^\circ\text{C}})}} = 23.47^\circ\text{C}\) Now, we rearrange the equation for the surface area of the heat exchanger: \(A = \frac{q}{U \cdot \Delta T_{lm}} = \frac{36688.4\text{ W}}{750 \frac{\text{W}}{\text{m}^2\cdot\text{K}} \cdot 23.47^\circ\text{C}} = 2.094 \text{ m}^2\) So, the surface area of the heat exchanger is approximately \(2.094 \text{ m}^2\).
04

d) Calculate and plot the blood and water outlet temperatures as a function of the water flow rate

To solve this part of the problem, we would need to use the governing equations for the heat exchanger and create a mathematical model. We suggest doing this with the help of software like MATLAB or Python, which would allow you to calculate the blood and water outlet temperatures over the given range of water flow rates (2 to 4 L/min). Once the calculations are done and the results are plotted, one could comment on how the changes in the outlet temperatures are affected by changes in the water flow rate. It is expected that an increase in water flow rate would lower the blood outlet temperature, and possibly bring the water outlet temperature closer to the blood outlet temperature. This would be advantageous in the cardiopulmonary bypass procedure, as it would allow better temperature control and potentially a more efficient heat exchange.

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Key Concepts

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

Cardiopulmonary Bypass Procedure
The cardiopulmonary bypass procedure is a critical medical technique applied during heart surgeries. This procedure temporarily takes over the function of both the heart and the lungs, maintaining circulation and oxygenation of the patient's blood. One key aspect of the procedure involves heat exchange to control the patient's temperature.
In many cases, inducing hypothermia is beneficial because it reduces metabolic rates and lowers oxygen demands, giving surgeons more time to operate without risking tissue damage.
  • Reducing the patient's body temperature slows cellular processes and provides protection against potential ischemic injury during prolonged surgeries.
  • Heat exchangers play a crucial role in this process by allowing precise control over blood temperature.
  • This controlled temperature management aids in reducing complications and improving patient outcomes.
Cross-Flow Heat Exchanger
A cross-flow heat exchanger is a type of heat exchanger where two fluids flow in perpendicular directions to each other. In the context of a cardiopulmonary bypass, this design is essential for efficient temperature regulation of the blood.
The unmixed flow design maximizes the temperature differential between the incoming blood and coolant, facilitating effective heat exchange.
  • This type of exchanger often allows for compact design, optimizing space use in medical devices.
  • It increases contact surface area between the blood and the cooling medium, enhancing the overall heat transfer rate.
  • Cross-flow exchangers are relatively simple, making them reliable and easy to maintain during critical medical procedures.
Heat Transfer Rate Calculation
Calculating the heat transfer rate is vital in understanding and optimizing the efficiency of a heat exchanger in a medical device. In this context, it measures how effectively the exchanger can cool the blood to the desired temperature.
The heat transfer rate, denoted by the symbol \( q \), can be computed using the formula: \[ q = \dot{m} \cdot c_p \cdot (T_{in} - T_{out}) \] where:
  • \( \dot{m} \) is the mass flow rate of the fluid, which is determined by multiplying the fluid's density by its volumetric flow rate.
  • \( c_p \) represents the specific heat capacity of the fluid, which indicates the energy required to change the fluid’s temperature.
  • \( T_{in} \) and \( T_{out} \) are the inlet and outlet temperatures, respectively.
This calculation helps assess whether the heat exchanger is meeting the necessary requirements to achieve the therapeutic goals of the procedure.
Overall Heat Transfer Coefficient
The overall heat transfer coefficient, symbolized as \( U \), is crucial for evaluating how well a heat exchanger performs. It considers all modes of heat transfer—conduction, convection, and radiation—between the fluids and the surfaces of the exchanger.
In practice, this coefficient helps determine the size and efficiency of a heat exchanger required for a specific application. A higher \( U \) value indicates more efficient heat transfer across the exchanger interface.
  • The \( U \) value combines material properties and surface conditions, impacting the design and operation of the exchanger.
  • Factors such as fluid velocities, material thermal conductivities, and exchanger geometry all contribute to this coefficient.
  • In medical procedures, understanding \( U \) helps engineers tailor heat exchangers to maintain patient safety and achieve precise temperature control.
Mathematically, it is used in the heat exchanger equation: \[ q = U \cdot A \cdot \Delta T_{lm} \] where \( A \) is the heat exchange surface area and \( \Delta T_{lm} \) is the log mean temperature difference, allowing precise calculation of the necessary surface area for effective operation.

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Most popular questions from this chapter

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?

Thin-walled aluminum tubes of diameter \(D=10 \mathrm{~mm}\) are used in the condenser of an air conditioner. Under normal operating conditions, a convection coefficient of \(h_{i}=5000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) is associated with condensation on the inner surface of the tubes, while a coefficient of \(h_{o}=100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) is maintained by airflow over the tubes. (a) What is the overall heat transfer coefficient if the tubes are unfinned? (b) What is the overall heat transfer coefficient based on the inner surface, \(U_{i}\), if aluminum annular fins of thickness \(t=1.5 \mathrm{~mm}\), outer diameter \(D_{o}=20 \mathrm{~mm}\), and pitch \(S=3.5 \mathrm{~mm}\) are added to the outer surface? Base your calculations on a 1-m-long section of tube. Subject to the requirements that \(t \geq 1 \mathrm{~mm}\) and \((S-t) \geq 1.5 \mathrm{~mm}\), explore the effect of variations in \(t\) and \(S\) on \(U_{i}\). What combination of \(t\) and \(S\) would yield the best heat transfer performance?

Cooling of outdoor electronic equipment such as in telecommunications towers is difficult due to seasonal and diurnal variations of the air temperature, and potential fouling of heat exchange surfaces due to dust accumulation or insect nesting. A concept to provide a nearly constant sink temperature in a hermetically sealed environment is shown below. The cool surface is maintained at nearly constant groundwater temperature \(\left(T_{1}=5^{\circ} \mathrm{C}\right)\) while the hot surface is subjected to a constant heat load from the electronic equipment \(\left(q_{2}=50 \mathrm{~W}, T_{2}\right)\). Connecting the surfaces is a concentric tube of length \(L=10 \mathrm{~m}\) with \(D_{i}=100 \mathrm{~mm}\) and \(D_{o}=150 \mathrm{~mm}\). A fan moves air at a mass flow rate of \(m=0.0325 \mathrm{~kg} / \mathrm{s}\) and dissipates \(P=10 \mathrm{~W}\) of thermal energy. Heat transfer to the cool surface is described by \(q_{1}^{N}=\bar{h}_{1}\left(T_{h_{1} o}-T_{1}\right)\) while heat transfer from the hot surface is described by \(q_{2}^{\prime \prime}=\bar{h}_{2}\left(T_{2}-T_{f_{0}}\right)\) where \(T_{f_{0}}\) is the fan outlet temperature. The values of \(\bar{h}_{1}\) and \(h_{2}\) are 40 and \(60 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), respectively. To isolate the electronics from ambient temperature variations, the entire device is insulated at its outer surfaces. The design engineer is concerned that conduction through the wall of the inner tube may adversely affect the device performance. Determine the value of \(T_{2}\) for the limiting cases of (i) no conduction resistance in the inner tube wall and (ii) infinite conduction resistance in the inner tube wall. Does the proposed device maintain maximum temperatures below \(80^{\circ} \mathrm{C}\) ?

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 \(T_{h i}\) ?

Consider a Rankine cycle with saturated steam leaving the boiler at a pressure of \(2 \mathrm{MPa}\) and a condenser pressure of \(10 \mathrm{kPa}\). (a) Calculate the thermal efficiency of the ideal Rankine cycle for these operating conditions. (b) If the net reversible work for the cycle is \(0.5 \mathrm{MW}\), calculate the required flow rate of cooling water supplied to the condenser at \(15^{\circ} \mathrm{C}\) with an allowable temperature rise of \(10^{\circ} \mathrm{C}\). (c) Design a shell-and-tube heat exchanger (one-shell, multiple-tube passes) that will meet the heat rate and temperature conditions required of the condenser. Your design should specify the number of tubes and their diameter and length.

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