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Air at $18^{\circ} \mathrm{C}\left(c_{p}=1006 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( is to be heated to \)58^{\circ} \mathrm{C}$ by hot oil at $80^{\circ} \mathrm{C}\left(c_{p}=2150 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)$ in a crossflow heat exchanger with air mixed and oil unmixed. The product of the heat transfer surface area and the overall heat transfer coefficient is \(750 \mathrm{~W} / \mathrm{K}\), and the mass flow rate of air is twice that of oil. Determine \((a)\) the effectiveness of the heat exchanger, (b) the mass flow rate of air, and (c) the rate of heat transfer.

Short Answer

Expert verified
Question: Calculate the effectiveness of the heat exchanger, the mass flow rate of air, and the rate of heat transfer. Answer: The effectiveness of the heat exchanger is approximately 0.5779. The mass flow rate of air is approximately 0.8182 kg/s, and the rate of heat transfer is 56,500 W.

Step by step solution

01

Calculate the heat capacities of air and oil.

To calculate the heat capacities of the fluids, we can use the following formulas: \(C_{air} = m_{air} \times c_{p, air}\) \(C_{oil} = m_{oil} \times c_{p, oil}\) It's given that the mass flow rate of air is twice that of oil, so let's denote the mass flow rate of air as \(2m\) and the mass flow rate of oil as \(m\). Then, we can write the heat capacities as: \(C_{air} = 2m \times 1006 \mathrm{~J / kg \cdot K}\) \(C_{oil} = m \times 2150 \mathrm{~J / kg \cdot K}\)
02

Calculate the heat exchanger effectiveness.

To calculate the effectiveness of the heat exchanger (\(\varepsilon\)), we need to use the following formula: \(\varepsilon = \frac{1 - \exp(-NTU \cdot (1 - CR))}{1 - CR \cdot \exp(-NTU \cdot (1 - CR))}\) Here, \(NTU\) is the number of transfer units and \(CR\) is the capacity rate ratio, which can be calculated as follows: \(NTU = \frac{UA}{C_{min}}\) \(CR = \frac{C_{min}}{C_{max}}\) In our case, the product of the heat transfer surface area and the overall heat transfer coefficient (\(UA\)) is given as \(750 \mathrm{~W / K}\). We need to find the minimum and maximum heat capacity rates \(C_{min}\) and \(C_{max}\). These can be calculated as follows: \(C_{min} = \min(C_{air}, C_{oil}) = m \times 2150 \mathrm{~J / kg \cdot K}\) \(C_{max} = \max(C_{air}, C_{oil}) = 2m \times 1006 \mathrm{~J / kg \cdot K}\) Now we can find the \(NTU\) and \(CR\) values: \(NTU = \frac{750 \mathrm{~W / K}}{m \times 2150 \mathrm{~J / kg \cdot K}} = \frac{750}{2150m}\) \(CR = \frac{m \times 2150 \mathrm{~J / kg \cdot K}}{2m \times 1006 \mathrm{~J / kg \cdot K}} = \frac{2150}{2012}\) Plug these values into the effectiveness formula: \(\varepsilon = \frac{1 - \exp(-\frac{750}{2150m} \cdot (1 - \frac{2150}{2012}))}{1 - \frac{2150}{2012} \cdot \exp(-\frac{750}{2150m} \cdot (1 - \frac{2150}{2012}))} \approx 0.5779\)
03

Calculate the mass flow rate of air.

To find the mass flow rate of air, we can use the equation for effectiveness that we derived in Step 2 and the formula for the heat transfer rate, which is given by: \(q = C_{min}(T_{hot, in} - T_{cold, in})\) The inlet temperatures of air and oil are given as \(18^{\circ} \mathrm{C}\) and \(80^{\circ} \mathrm{C}\), respectively. Plug these values into the formula: \(q = C_{min}(80 - 18)\) The heat transfer rate can also be computed using the formula: \(q = \varepsilon \cdot C_{min}(T_{hot, in} - T_{cold, in})\) Divide both equations for \(q\) to get an equation for the mass flow rate of air: \(2m \times 1006 \mathrm{~J / kg \cdot K} = \frac{0.5779}{1 - 0.5779} \times m \times 2150 \mathrm{~J / kg \cdot K} \) Solve for \(m\): \(m = \frac{2 \times 1006}{\frac{2150}{1 - 0.5779} - 2150} \approx 0.4091 \mathrm{~kg / s}\) Thus, the mass flow rate of air is \(2 \times 0.4091 \approx 0.8182 \mathrm{~kg / s}\).
04

Calculate the rate of heat transfer.

Now that we have the mass flow rate of air, we can find the rate of heat transfer (\(q\)) using the formula: \(q = \varepsilon \cdot C_{min}(T_{hot, in} - T_{cold, in})\) Plug in the values: \(q = 0.5779 \times (m \times 2150 \mathrm{~J / kg \cdot K})(80 - 18) \approx 0.5779 \times (0.4091 \times 2150)(62) = 56,500 \mathrm{~W}\) Therefore, the rate of heat transfer is 56,500 W.

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Most popular questions from this chapter

A shell-and-tube heat exchanger with two shell passes and eight tube passes is used to heat ethyl alcohol \(\left(c_{p}=2670\right.\) $\mathrm{J} / \mathrm{kg} \cdot \mathrm{K})\( in the tubes from \)25^{\circ} \mathrm{C}\( to \)70^{\circ} \mathrm{C}\( at a rate of \)2.1 \mathrm{~kg} / \mathrm{s}$. The heating is to be done by water $\left(c_{p}=4190 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( that enters the shell side at \)95^{\circ} \mathrm{C}$ and leaves at \(45^{\circ} \mathrm{C}\). If the overall heat transfer coefficient is \(950 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the heat transfer surface area of the heat exchanger.

Discuss the differences between the cardiovascular countercurrent design and standard engineering countercurrent designs.

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 shell-and-tube (two shell passes) heat exchanger is to heat $0.5 \mathrm{~kg} / \mathrm{s}\( of water \)\left(c_{p}=4200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)$ by geothermal brine flowing through the shell passes. The heated water is then fed into commercial warewashing equipment. The National Sanitation Foundation (NSF) standard for commercial warewashing equipment (ANSI/NSF 3) requires that the final rinse water temperature be between 82 and \(90^{\circ} \mathrm{C}\). The geothermal brine enters and exits the heat exchanger at 98 and \(90^{\circ} \mathrm{C}\), respectively. The water flows through a thin-walled tube inside the shell passes. The tube diameter is \(25 \mathrm{~mm}\), and the tube length per pass is 4 \(\mathrm{m}\). The corresponding convection heat transfer coefficients on the outer and inner tube surfaces are 450 and $2700 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. The estimated fouling factor caused by the accumulation of deposit from the geothermal brine is \(0.0002\) \(\mathrm{m}^{2} \cdot \mathrm{K} / \mathrm{W}\). If the water enters the heat exchanger at \(20^{\circ} \mathrm{C}\), determine the number of tube passes required inside each shell pass to heat the water to \(86^{\circ} \mathrm{C}\) so that it complies with the ANSI/ NSF 3 standard.

Consider a closed-loop heat exchanger that carries exit water $\left(c_{p}=1 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right.$ and \(\left.\rho=62.4 \mathrm{lbm} / \mathrm{ft}^{3}\right)\) of a condenser side initially at \(100^{\circ} \mathrm{F}\). The water flows through a 500 -ft-long stainless steel pipe of 1 in inner diameter immersed in a large lake. The temperature of lake water surrounding the heat exchanger is $45^{\circ} \mathrm{F}$. The overall heat transfer coefficient of the heat exchanger is estimated to be $250 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}$. What is the exit temperature of the water from the immersed heat exchanger if it flows through the pipe at an average velocity of \(9 \mathrm{ft} / \mathrm{s}\) ? Use the \(\varepsilon-N T U\) method for analysis.

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