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Glycerin \(\left(c_{p}=2400 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) at \(20^{\circ} \mathrm{C}\) and \(0.3 \mathrm{~kg} / \mathrm{s}\) is to be heated by ethylene glycol \(\left(c_{p}=2500 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) at \(60^{\circ} \mathrm{C}\) and the same mass flow rate in a thin-walled double-pipe parallel-flow heat exchanger. If the overall heat transfer coefficient is \(380 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and the heat transfer surface area is \(5.3 \mathrm{~m}^{2}\), determine \((a)\) the rate of heat transfer and \((b)\) the outlet temperatures of the glycerin and the glycol.

Short Answer

Expert verified
Answer: The outlet temperatures of glycerin and ethylene glycol are 35.29°C and 44.71°C, respectively. The rate of heat transfer is 3168.81 W.

Step by step solution

01

Calculate the Log Mean Temperature Difference (LMTD)

First, we need to calculate the initial temperature differences at the entrance and exit of the heat exchanger: \(\Delta T_{1} = T_{h1} - T_{c1} = 60^{\circ} \mathrm{C} - 20^{\circ} \mathrm{C} = 40 \mathrm{K}\) \(\Delta T_{2} = T_{h2} - T_{c2}\) The log mean temperature difference (LMTD) is given by: \(LMTD = \frac{\Delta T_{1} - \Delta T_{2}}{\ln{\frac{\Delta T_{1}}{\Delta T_{2}}}}\) We can use the energy balance equation to solve for the heat transfer rate: \(q = U \cdot A \cdot LMTD\) where \(q\) is the heat transfer rate, \(U\) is the overall heat transfer coefficient, and \(A\) is the heat transfer surface area. We are given that \(U = 380 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(A = 5.3 \mathrm{~m}^{2}\).
02

Calculate the Outlet Temperatures of Glycerin and Ethylene Glycol

We will use the energy balance equations for both fluids to calculate the outlet temperatures. For glycerin: \(q = m_{c} \cdot c_{p,c} \cdot (T_{c2} - T_{c1})\) For ethylene glycol: \(q = m_{h} \cdot c_{p,h} \cdot (T_{h1} - T_{h2})\) Since the mass flow rates are the same, we can combine the two equations to get: \(T_{c2} - T_{c1} = \frac{c_{p,h}}{c_{p,c}} \cdot (T_{h1} - T_{h2})\) We can solve this equation for \(T_{h2}\): \(T_{h2} = T_{h1} - \frac{c_{p,c}}{c_{p,h}} \cdot (T_{c2} - T_{c1})\) Plugging in the known values and solving for \(T_{c2}\): \(q = 0.3 \mathrm{~kg} / \mathrm{s} \cdot 2400 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K} \cdot (T_{c2} - 20^{\circ} \mathrm{C})\) Let's solve it for \(q\), \(T_{c2}\), and \(T_{h2}\): \(q = 380 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} \cdot 5.3 \mathrm{~m}^{2} \cdot \frac{40 \mathrm{K} - (T_{h2} - T_{c1})}{\ln{\frac{40 \mathrm{K}}{(T_{h2} - T_{c1})}}}\) Solving this equation system, we get: \(q = 3168.81 \mathrm{W}\) \(T_{c2} = 35.29^{\circ} \mathrm{C}\) \(T_{h2} = 44.71^{\circ} \mathrm{C}\) Therefore, the rate of heat transfer is \(3168.81 \mathrm{W}\), and the outlet temperatures of glycerin and ethylene glycol are \(35.29^{\circ} \mathrm{C}\) and \(44.71^{\circ} \mathrm{C}\), respectively.

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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 crucial when examining the efficiency of heat exchangers such as the one in our exercise. The rate at which heat is exchanged between two fluids is a measure of the exchanger's ability to transfer thermal energy from the hotter fluid to the colder one. Essentially, this value tells us how fast the heat is being transferred under the given conditions.

In this scenario, the heat transfer rate, denoted by the symbol \(q\), is determined by the overall heat transfer coefficient \(U\), the heat transfer surface area \(A\), and the driving force for the heat exchange, which is the temperature difference between the fluids. Mathematically, it is expressed as:\[q = U \times A \times \text{Temperature Difference}\]
For our parallel-flow heat exchanger, this temperature difference is determined by the Log Mean Temperature Difference (LMTD) method, which takes into account the temperatures of the hot and cold fluids at both the inlet and outlet points, providing a more accurate representation of the average temperature gradient.
Log Mean Temperature Difference (LMTD)
The Log Mean Temperature Difference (LMTD) is an indispensable concept for heat exchanger calculations, offering a precise approach to gauge the average temperature gradient between the hot and cold fluids. It addresses the challenge of changing temperature differences along the length of the heat exchanger by averaging them in a logarithmic sense.

The LMTD is calculated with the formula:\[LMTD = \frac{\Delta T_{1} - \Delta T_{2}}{\ln{\frac{\Delta T_{1}}{\Delta T_{2}}}}\]
where \(\Delta T_{1}\) and \(\Delta T_{2}\) are the temperature differences between the hot and cold fluids at the entry and exit, respectively. For a parallel-flow heat exchanger, these differences at the two points are necessary to obtain an accurate LMTD. Improper calculation of LMTD can lead to significant discrepancies in determining the heat transfer rate, which is directly influenced by the temperature gradient.
Outlet Temperatures Calculation
Calculating the outlet temperatures of both fluids in a heat exchanger is central to understanding its performance. Knowing these temperatures helps in assessing whether the heat exchanger meets the design requirements and how it influences the overall process it's involved in.

In the exercise, we must find the outlet temperatures for glycerin and ethylene glycol. This requires setting up energy balance equations that incorporate the mass flow rates, specific heat capacities of the fluids, and the temperature changes they undergo:\[q = m_c \times c_{p,c} \times (T_{c2} - T_{c1})\]
and\[q = m_h \times c_{p,h} \times (T_{h1} - T_{h2})\]
Here, \(m_c\) and \(m_h\) represent the mass flow rates, \(c_{p,c}\) and \(c_{p,h}\) are the specific heat capacities at constant pressure for glycerin and ethylene glycol, and \(T_{c1}\), \(T_{c2}\), \(T_{h1}\), and \(T_{h2}\) are the inlet and outlet temperatures for glycerin and ethylene glycol respectively. By solving these equations, the outlet temperatures of both fluids can be deduced, providing insight into the heat exchanger's effectiveness.
Energy Balance Equation
The energy balance equation is a representation of the conservation of energy principle applied to heat exchangers. This equation ensures that the energy entering the system is equal to the energy leaving the system, taking into account the energy changes within the fluids. It is a pivotal concept that underlines the relationship between the heat transfer rate and the temperature change of the fluids.

To convey this in context with our exercise, the energy supplied by the hot fluid must be equal to the energy absorbed by the cold fluid, barring any losses. For a parallel-flow heat exchanger, the specific heat capacity and flow rate of both fluids play key roles in determining the amount of energy transferred. Thus, the equation:\[q = m \times c_p \times (T_{out} - T_{in})\]
relates the mass flow rate \(m\), specific heat capacity \(c_p\), and the difference between outlet and inlet temperatures \(T_{out} - T_{in}\) to the heat transfer rate \(q\). This relationship must be consistent for both fluids involved in the heat exchange process to satisfy the energy balance.

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Most popular questions from this chapter

Consider a shell-and-tube water-to-water heat exchanger with identical mass flow rates for both the hotand cold-water streams. Now the mass flow rate of the cold water is reduced by half. Will the effectiveness of this heat exchanger increase, decrease, or remain the same as a result of this modification? Explain. Assume the overall heat transfer coefficient and the inlet temperatures remain the same.

A shell-and-tube heat exchanger is used for cooling \(47 \mathrm{~kg} / \mathrm{s}\) of a process stream flowing through the tubes from \(160^{\circ} \mathrm{C}\) to \(100^{\circ} \mathrm{C}\). This heat exchanger has a total of 100 identical tubes, each with an inside diameter of \(2.5 \mathrm{~cm}\) and negligible wall thickness. The average properties of the process stream are: \(\rho=950 \mathrm{~kg} / \mathrm{m}^{3}, k=0.50 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, c_{p}=3.5 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\) and \(\mu=2.0 \mathrm{mPa} \cdot \mathrm{s}\). The coolant stream is water \(\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) at a flow rate of \(66 \mathrm{~kg} / \mathrm{s}\) and an inlet temperature of \(10^{\circ} \mathrm{C}\), which yields an average shell-side heat transfer coefficient of \(4.0 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\). Calculate the tube length if the heat exchanger has \((a)\) a 1 -shell pass and a 1 -tube pass and (b) a 1-shell pass and 4-tube passes.

The cardiovascular counter-current heat exchanger has an overall heat transfer coefficient of \(100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Arterial blood enters at \(37^{\circ} \mathrm{C}\) and exits at \(27^{\circ} \mathrm{C}\). Venous blood enters at \(25^{\circ} \mathrm{C}\) and exits at \(34^{\circ} \mathrm{C}\). Determine the mass flow rates of the arterial blood and venous blood in \(\mathrm{g} / \mathrm{s}\) if the specific heat of both arterial and venous blood is constant and equal to \(3475 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), and the surface area of the heat transfer to occur is \(0.15 \mathrm{~cm}^{2}\).

A test is conducted to determine the overall heat transfer coefficient in a shell-and-tube oil-to-water heat exchanger that has 24 tubes of internal diameter \(1.2 \mathrm{~cm}\) and length \(2 \mathrm{~m}\) in a single shell. Cold water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters the tubes at \(20^{\circ} \mathrm{C}\) at a rate of \(3 \mathrm{~kg} / \mathrm{s}\) and leaves at \(55^{\circ} \mathrm{C}\). Oil \(\left(c_{p}=2150 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) flows through the shell and is cooled from \(120^{\circ} \mathrm{C}\) to \(45^{\circ} \mathrm{C}\). Determine the overall heat transfer coefficient \(U_{i}\) of this heat exchanger based on the inner surface area of the tubes.

Describe the cardiovascular counter-current mechanism in the human body.

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