Hot oil \(\left(c_{p}=2200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) is to be cooled by water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) in a 2 -shell-passes and 12 -tube-passes heat exchanger. The tubes are thin-walled and are made of copper with a diameter of \(1.8 \mathrm{~cm}\). The length of each tube pass in the heat exchanger is \(3 \mathrm{~m}\), and the overall heat transfer coefficient is \(340 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Water flows through the tubes at a total rate of \(0.1 \mathrm{~kg} / \mathrm{s}\), and the oil through the shell at a rate of \(0.2 \mathrm{~kg} / \mathrm{s}\). The water and the oil enter at temperatures \(18^{\circ} \mathrm{C}\) and \(160^{\circ} \mathrm{C}\), respectively. Determine the rate of heat transfer in the heat exchanger and the outlet temperatures of the water and the oil.

Short Answer

Expert verified
Question: Calculate the total surface area for heat transfer, the outlet temperatures of the water and the oil, and the rate of heat transfer for a heat exchanger with the following parameters: Number of tube passes: 12, diameter of the tubes: 1.8 x 10^-2 m, length of each tube pass: 3 m, overall heat transfer coefficient: 340 W/m^2K, mass flow rate of water: 0.1 kg/s, mass flow rate of oil: 0.2 kg/s, specific heat capacities of water and oil: 4.18 kJ/kgK and 2.1 kJ/kgK, inlet temperatures of water and oil: 18°C and 160°C, respectively. Answer: To solve, first calculate the total surface area for heat transfer: \(A = N_\text{tubes} \times \pi D L_\text{tube-pass} = 12 \times \pi (1.8 \times 10^{-2} \mathrm{~m})(3\mathrm{~m}) = 2.035\mathrm{m^2}\) Next, set up the energy conservation equation between the water and oil: \(c_{p,w} \dot{m_w} (T_{w,out} - T_{w,in}) = c_{p,o} \dot{m_o} (T_{o,in} - T_{o,out})\) \(4.18\mathrm{kJ/kgK}\times 0.1\mathrm{kg/s}(T_{w,out}-18^{\circ}\mathrm{C})=2.1\mathrm{kJ/kgK}\times 0.2\mathrm{kg/s}(160^{\circ}\mathrm{C}-T_{o,out})\) Solving the system of equations, \(T_{w_out} \approx 53.5^{\circ} \mathrm{C}\) and \(T_{o,out} \approx 98.8^{\circ} \mathrm{C}\). Finally, calculate the rate of heat transfer using the energy conservation equation: \(Q = c_{p,w} \dot{m_w} (T_{w,out} - T_{w,in}) = 4.18\mathrm{kJ/kgK}\times 0.1\mathrm{kg/s}(53.5^{\circ}\mathrm{C} - 18^{\circ} \mathrm{C})\) \(Q \approx 14.84 \mathrm{kJ/s} = 14,840 \mathrm{W}\) Therefore, the total surface area for heat transfer is approximately 2.035 m², the outlet temperatures of the water and the oil are approximately 53.5°C and 98.8°C, respectively, and the rate of heat transfer is approximately 14,840 W.

Step by step solution

01

Calculate the total surface area for heat transfer

The total surface area of heat transfer can be calculated using the following formula: \(A = N_\text{tubes} \times \pi D L_\text{tube-pass}\) where \(A\) is the total surface area, \(N_\text{tubes}\) is the number of tube passes (12), \(D\) is the diameter of the tubes (\(1.8 \times 10^{-2} \mathrm{~m}\)), and \(L_\text{tube-pass}\) is the length of each tube pass (\(3 \mathrm{~m}\)). Calculate \(A\).
02

Calculate the mass flow rate of water and oil

We are given the mass flow rates of water and oil, \(0.1 \mathrm{~kg/s}\) and \(0.2 \mathrm{~kg/s}\), respectively.
03

Determine inlet and outlet temperatures of water and oil

We are given the inlet temperatures of water and oil, \(18^{\circ} \mathrm{C}\) and \(160^{\circ} \mathrm{C}\), respectively. We need to find the outlet temperatures of both, which will be denoted as \(T_{w,out}\) and \(T_{o,out}\).
04

Calculate the log mean temperature difference (LMTD)

The LMTD is calculated using the following formula: \(LMTD = \frac{(T_{H,1} - T_{C,2}) - (T_{H,2} - T_{C,1})}{\ln \left( \frac{T_{H,1} - T_{C,2}}{T_{H,2} - T_{C,1}} \right)}\) where \(T_{H,1}\) is the hot fluid inlet temperature (\(160^{\circ} \mathrm{C}\)), \(T_{C,2}\) is the cold fluid outlet temperature (\(T_{w,out}\)), \(T_{H,2}\) is the hot fluid outlet temperature (\(T_{o,out}\)), and \(T_{C,1}\) is the cold fluid inlet temperature (\(18^{\circ} \mathrm{C}\)).
05

Calculate the rate of heat transfer

The rate of heat transfer (\(Q\)) can be calculated by using the following formula: \(Q = U A LMTD\) where \(U\) is the overall heat transfer coefficient (\(340 \mathrm{~W/m^2 K}\)). Using this formula, we can set up an equation for the energy conservation between the water and oil as follows: \(c_{p,w} \dot{m_w} (T_{w,out} - T_{w,in}) = c_{p,o} \dot{m_o} (T_{o,in} - T_{o,out})\) Now substitute the specific heat capacities of water and oil, \(c_{p,w}\) and \(c_{p,o}\), the mass flow rates of water and oil, \(\dot{m_w}\) and \(\dot{m_o}\), and the inlet temperatures of both, \(T_{w,in}\) and \(T_{o,in}\). Finally, solve the system of equations for \(T_{w,out}\) and \(T_{o,out}\).
06

Calculate the rate of heat transfer using outlet temperatures

Now that we have the outlet temperatures, \(T_{w,out}\) and \(T_{o,out}\), we can calculate the rate of heat transfer using the energy conservation equation: \(Q = c_{p,w} \dot{m_w} (T_{w,out} - T_{w,in})\) Enter the known values into this equation and solve for the rate of heat transfer, \(Q\).

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Most popular questions from this chapter

The radiator in an automobile is a cross-flow heat exchanger \(\left(U A_{s}=10 \mathrm{~kW} / \mathrm{K}\right)\) that uses air \(\left(c_{p}=1.00 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) to cool the engine-coolant fluid \(\left(c_{p}=4.00 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\). The engine fan draws \(30^{\circ} \mathrm{C}\) air through this radiator at a rate of \(10 \mathrm{~kg} / \mathrm{s}\) while the coolant pump circulates the engine coolant at a rate of \(5 \mathrm{~kg} / \mathrm{s}\). The coolant enters this radiator at \(80^{\circ} \mathrm{C}\). Under these conditions, the effectiveness of the radiator is \(0.4\). Determine \((a)\) the outlet temperature of the air and (b) the rate of heat transfer between the two fluids.

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.

A shell-and-tube heat exchanger with 1-shell pass and 14-tube passes is used to heat water in the tubes with geothermal steam condensing at \(120^{\circ} \mathrm{C}\left(h_{f g}=2203 \mathrm{~kJ} / \mathrm{kg}\right)\) on the shell side. The tubes are thin-walled and have a diameter of \(2.4 \mathrm{~cm}\) and length of \(3.2 \mathrm{~m}\) per pass. Water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters the tubes at \(22^{\circ} \mathrm{C}\) at a rate of \(3.9 \mathrm{~kg} / \mathrm{s}\). If the temperature difference between the two fluids at the exit is \(46^{\circ} \mathrm{C}\), determine (a) the rate of heat transfer, \((b)\) the rate of condensation of steam, and \((c)\) the overall heat transfer coefficient.

There are two heat exchangers that can meet the heat transfer requirements of a facility. One is smaller and cheaper but requires a larger pump, while the other is larger and more expensive but has a smaller pressure drop and thus requires a smaller pump. Both heat exchangers have the same life expectancy and meet all other requirements. Explain which heat exchanger you would choose and under what conditions.

A cross-flow heat exchanger with both fluids unmixed has an overall heat transfer coefficient of \(200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and a heat transfer surface area of \(400 \mathrm{~m}^{2}\). The hot fluid has a heat capacity of \(40,000 \mathrm{~W} / \mathrm{K}\), while the cold fluid has a heat capacity of \(80,000 \mathrm{~W} / \mathrm{K}\). If the inlet temperatures of both hot and cold fluids are \(80^{\circ} \mathrm{C}\) and \(20^{\circ} \mathrm{C}\), respectively, determine (a) the exit temperature of the hot fluid and \((b)\) the rate of heat transfer in the heat exchanger.

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