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Water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) is to be heated by solarheated hot air $\left(c_{p}=1010 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)$ in a double-pipe counterflow heat exchanger. Air enters the heat exchanger at \(90^{\circ} \mathrm{C}\) at a rate of \(0.3 \mathrm{~kg} / \mathrm{s}\), while water enters at $22^{\circ} \mathrm{C}\( at a rate of \)0.1 \mathrm{~kg} / \mathrm{s}$. The overall heat transfer coefficient based on the inner side of the tube is given to be $80 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. The length of the tube is \)12 \mathrm{~m}\(, and the internal diameter of the tube is \)1.2 \mathrm{~cm}$. Determine the outlet temperatures of the water and the air.

Short Answer

Expert verified
Based on the given information and calculations, the outlet temperatures of water and air in the double-pipe counterflow heat exchanger are: - Water outlet temperature: \(27.774^{\circ}\mathrm{C}\) - Air outlet temperature: \(82.039^{\circ}\mathrm{C}\)

Step by step solution

01

Calculate the heat capacity rates for water and air

Calculate the heat capacity rates (C) for both water and air using the formula: \(C = m \times c_p\), where \(m\) is the mass flow rate and \(c_p\) is the specific heat capacity. For water: \(C_w = m_w \times c_{p_{w}} = 0.1 \textrm{ kg/s} \times 4180 \textrm{ J/kgK} = 418 \textrm{ W/K}\) For air: \(C_a = m_a \times c_{p_{a}} = 0.3 \textrm{ kg/s} \times 1010 \textrm{ J/kgK} = 303 \textrm{ W/K}\)
02

Determine the minimum heat capacity rate and the heat capacity rate ratio

Identify the fluid with the minimum heat capacity rate (C_min) and calculate the heat capacity rate ratio (R) using the formula: \(R = \frac{C_{min}}{C_{max}}\) In this case, \(C_w < C_a\), so fluid with the minimum heat capacity rate is water. \(C_{min} = C_w = 418 \mathrm{~W/K}\) Now, calculate R: \(R = \frac{C_{w}}{C_{a}} = \frac{418}{303} = 1.3792\)
03

Calculate the heat transfer area

Calculate the heat transfer area (A) using the length and internal diameter of the tube. The formula for the heat transfer area of a tube is \(A = \pi d L\), where \(d\) is the internal diameter and \(L\) is the length of the tube. \(A = \pi(0.012 \mathrm{~m})(12 \mathrm{~m}) = 0.453 \mathrm{~m^2}\)
04

Calculate the NTU value

Calculate the Number of Transfer Units (NTU) using the formula: \(NTU = \frac{UA}{C_{min}}\), where U is the overall heat transfer coefficient, and A is the heat transfer area. \(NTU = \frac{80 \mathrm{~W/m^2K} \times 0.453 \mathrm{~m^2}}{418 \mathrm{~W/K}} = 0.0864\)
05

Determine the effectiveness

For a double-pipe counterflow heat exchanger, we can use the formula for calculating effectiveness: \(\epsilon = \frac{1 - e^{-NTU(1-R)}}{1 - R e^{-NTU(1-R)}}\) Substitute the values we obtained in the previous steps: \(\epsilon = \frac{1 - e^{-0.0864(1-1.3792)}}{1 - 1.3792 e^{-0.0864(1-1.3792)}} = 0.0844\)
06

Calculate the heat transfer

Calculate the heat transfer rate (Q) using the formula: \(Q = \epsilon \times C_{min} \times (\Delta T)_{max}\) In this case, the maximum possible temperature change is the difference in inlet temperatures of air and water: \((\Delta T)_{max} = T_{inlet_{air}} - T_{inlet_{water}} = 90^{\circ}C - 22^{\circ}C = 68 \mathrm{~K}\) \(Q = 0.0844 \times 418 \mathrm{~W/K} \times 68 \mathrm{~K} = 2412.312 \mathrm{~W}\)
07

Determine the outlet temperatures

Calculate the outlet temperature of water (T_outlet_water) using the formula: \(T_{outlet_{water}} = T_{inlet_{water}} + \frac{Q}{C_w}\) \(T_{outlet_{water}} = 22^{\circ}C + \frac{2412.312 \mathrm{~W}}{418 \mathrm{~W/K}} = 22^{\circ}C + 5.774 \mathrm{~K} = 27.774^{\circ}\mathrm{C}\) Calculate the outlet temperature of air (T_outlet_air) using the formula: \(T_{outlet_{air}} = T_{inlet_{air}} - \frac{Q}{C_a}\) \(T_{outlet_{air}} = 90^{\circ}C - \frac{2412.312 \mathrm{~W}}{303 \mathrm{~W/K}} = 90^{\circ}C - 7.961 \mathrm{~K} = 82.039^{\circ}\mathrm{C}\) The outlet temperatures of water and air are \(27.774^{\circ}\mathrm{C}\) and \(82.039^{\circ}\mathrm{C}\), respectively.

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Most popular questions from this chapter

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 \(\mu=0.002 \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\). The coolant stream is water \(c_{p}=4.18\) \(\mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K}\) 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 \(4.0 \mathrm{~kW} / \mathrm{m}^{2} . \mathrm{K}\). Calculate the tube length if the heat exchanger has \((a)\) one shell pass and one tube pass and \((b)\) one shell pass and four tube passes.

Oil in an engine is being cooled by air in a crossflow heat exchanger, where both fluids are unmixed. Oil $\left(c_{p l}=2047 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( flowing with a flow rate of \)0.026 \mathrm{~kg} / \mathrm{s}\( enters the tube side at \)75^{\circ} \mathrm{C}$, while air \(\left(c_{p c}=1007 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters the shell side at \(30^{\circ} \mathrm{C}\) with a flow rate of $0.21 \mathrm{~kg} / \mathrm{s}$. The overall heat transfer coefficient of the heat exchanger is \(53 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\), and the total surface area is \(1 \mathrm{~m}^{2}\). If the correction factor is \(F=0.96\), determine the outlet temperatures of the oil and air.

In a parallel-flow, water-to-water heat exchanger, the hot water enters at \(75^{\circ} \mathrm{C}\) at a rate of \(1.2 \mathrm{~kg} / \mathrm{s}\) and cold water enters at \(20^{\circ} \mathrm{C}\) at a rate of $0.9 \mathrm{~kg} / \mathrm{s}$. The overall heat transfer coefficient and the surface area for this heat exchanger are \(750 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(6.4 \mathrm{~m}^{2}\), respectively. The specific heat for both the hot and cold fluids may be taken to be $4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}$. For the same overall heat transfer coefficient and the surface area, the increase in the effectiveness of this heat exchanger if counterflow arrangement is used is (a) \(0.09\) (b) \(0.11\) (c) \(0.14\) (d) \(0.17\) (e) \(0.19\)

Consider a heat exchanger that has an NTU of \(0.1\). Someone proposes to triple the size of the heat exchanger and thus triple the NTU to \(0.3\) in order to increase the effectiveness of the heat exchanger and thus save energy. Would you support this proposal?

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. Answer: $8.31 \mathrm{~kW} / \mathrm{m}^{2} \mathrm{~K}$

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