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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.

Short Answer

Expert verified
Answer: Approximately 46 tube passes are required per shell pass.

Step by step solution

01

Determine the mass flow rate of water

Given that the mass flow rate of the water is \(0.5\,\mathrm{kg/s}\).
02

Calculate the heat transfer in the water

Given that the specific heat capacity of water is \(4200\,\mathrm{J/kg\cdot K}\). The temperature of water increases from \(20^{\circ}\mathrm{C}\) to \(86^{\circ}\mathrm{C}\). The equation for heat transfer, \(Q\), can be written as follows: \(Q = (\dot m\,c_p\Delta T)_{water}\) \(Q = 0.5\,\mathrm{kg/s} \times 4200\,\mathrm{J/kg \cdot K} \times (86 - 20)\) \(Q = 138600\,\mathrm{W}\)
03

Calculate the overall heat transfer coefficient

The overall heat transfer coefficient, \(U\), is given by: \(1 / U = 1 / h_{i} + 1 / h_{o} + R_{f}\) where \(h_i\) and \(h_o\) are the convection heat transfer coefficients on the inner and outer surfaces of the tube, and \(R_f\) is the fouling factor. \(1 / U = 1 / 2700 + 1 / 450 + 0.0002\) Solving for \(U\), we get: \(U = 399.6\,\mathrm{W/m^2 \cdot K}\)
04

Calculate the Log Mean Temperature Difference (LMTD)

As this is a two-shell pass heat exchanger, we need to consider the temperature changes happening within the shell. The temperatures are given as: - Hot fluid inlet temp: \(T_{Hi} = 98^\circ\mathrm{C}\) - Hot fluid outlet temp: \(T_{Ho} = 90^\circ\mathrm{C}\) - Cold fluid inlet temp: \(T_{Ci} = 20^\circ\mathrm{C}\) - Cold fluid outlet temp: \(T_{Co} = 86^\circ\mathrm{C}\) LMTD = \(\frac{(ΔT_{1ab}-ΔT_{2ab})}{\ln(\frac{ΔT_{1ab}}{ΔT_{2ab}})}\) \(\Delta T_{1ab} = T_{Hi} - T_{Co}\) \(\Delta T_{1ab} = 98 - 86 = 12\,\mathrm{K}\) \(\Delta T_{2ab} = T_{Ho} - T_{Ci}\) \(\Delta T_{2ab} = 90 - 20 = 70\,\mathrm{K}\) Substituting the values in the LMTD equation: LMTD = \(\frac{(12-70)}{\ln(\frac{12}{70})}\) LMTD = \(24.399\,\mathrm{K}\)
05

Calculate the required heat transfer area

Using the heat transfer equation \(Q = UA\Delta T\), we can calculate the required heat transfer area \(A\): \(A = \frac{Q}{U \cdot \text{LMTD}}\) \(A = \frac{138600}{399.6 \times 24.399}\) \(A = 14.352\,\mathrm{m^2}\)
06

Calculate the heat transfer area per tube pass

Using the tube diameter and length information given, we can calculate the heat transfer area per tube pass: \(A_t = \pi D L = \pi \times 0.025 \times 4\) \(A_t = 0.314\,\mathrm{m^2}\) per tube pass
07

Calculate the number of tube passes required per shell pass

Finally, we can determine the number of tube passes required per shell pass by dividing the total heat transfer area by the heat transfer area per tube pass: Number of tube passes per shell pass = \(\frac{A}{A_t}\) Number of tube passes per shell pass = \(\frac{14.352}{0.314}\) Number of tube passes per shell pass = \(45.71\) Since it's not possible to have a fraction of a tube pass, we can round up to the nearest whole number: The number of tube passes required per shell pass is approximately 46.

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Most popular questions from this chapter

Saturated water vapor at \(40^{\circ} \mathrm{C}\) is to be condensed as it flows through the tubes of an air-cooled condenser at a rate of $0.2 \mathrm{~kg} / \mathrm{s}$. The condensate leaves the tubes as a saturated liquid at \(40^{\circ} \mathrm{C}\). The rate of heat transfer to air is (a) \(34 \mathrm{~kJ} / \mathrm{s}\) (b) \(268 \mathrm{~kJ} / \mathrm{s}\) (c) \(453 \mathrm{~kJ} / \mathrm{s}\) (d) \(481 \mathrm{~kJ} / \mathrm{s}\) (e) \(515 \mathrm{~kJ} / \mathrm{s}\)

Ethanol is vaporized at $78^{\circ} \mathrm{C}\left(h_{f \mathrm{~g}}=846 \mathrm{~kJ} / \mathrm{kg}\right)$ in a double-pipe parallel-flow heat exchanger at a rate of \(0.04 \mathrm{~kg} / \mathrm{s}\) by hot oil \(\left(c_{p}=2200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) that enters at \(115^{\circ} \mathrm{C}\). If the heat transfer surface area and the overall heat transfer coefficients are \(6.2 \mathrm{~m}^{2}\) and $320 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively, determine the outlet temperature and the mass flow rate of oil using \((a)\) the LMTD method and \((b)\) the \(\varepsilon-\mathrm{NTU}\) method.

A double-pipe heat exchanger is used to cool a hot fluid before it flows into a system of pipes. The inner surface of the pipes is primarily coated with polypropylene lining. The maximum use temperature for polypropylene lining is $107^{\circ} \mathrm{C}$ (ASME Code for Process Piping, ASME B31.32014, Table A323.4.3). The double-pipe heat exchanger has a thin-walled inner tube, with convection heat transfer coefficients inside and outside of the inner tube estimated to be \(1400 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and $1100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. The heat exchanger has a heat transfer surface area of \(2.5 \mathrm{~m}^{2}\), and the estimated fouling factor caused by the accumulation of deposit on the surface is \(0.0002\) \(\mathrm{m}^{2} \cdot \mathrm{K} / \mathrm{W}\). The hot fluid \(\left(c_{p}=3800 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters the heat exchanger at \(200^{\circ} \mathrm{C}\) with a flow rate of $0.4 \mathrm{~kg} / \mathrm{s}\(. In the cold side, cooling fluid \)\left(c_{p}=4200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)$ enters the heat exchanger at \(10^{\circ} \mathrm{C}\) with a mass flow rate of $0.5 \mathrm{~kg} / \mathrm{s}$.

Consider a double-pipe heat exchanger with a tube diameter of $10 \mathrm{~cm}$ and negligible tube thickness. The total thermal resistance of the heat exchanger was calculated to be \(0.025 \mathrm{k} / \mathrm{W}\) when it was first constructed. After some prolonged use, fouling occurs at both the inner and outer surfaces with the fouling factors $0.00045 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}\( and \)0.00015 \mathrm{~m}^{2} \cdot \mathrm{K} / \mathrm{W}$, respectively. The percentage decrease in the rate of heat transfer in this heat exchanger due to fouling is (a) \(2.3 \%\) (b) \(6.8 \%\) (c) \(7.1 \%\) (d) \(7.6 \%\) (e) \(8.5 \%\)

Cold water $\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( enters a heat exchanger at \)15^{\circ} \mathrm{C}$ at a rate of \(0.5 \mathrm{~kg} / \mathrm{s}\), where it is heated by hot air \(\left(c_{p}=1.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) that enters the heat exchanger at \(50^{\circ} \mathrm{C}\) at a rate of $1.8 \mathrm{~kg} / \mathrm{s}$. The maximum possible heat transfer rate in this heat exchanger is (a) \(51.1 \mathrm{~kW}\) (b) \(63.0 \mathrm{~kW}\) (c) \(66.8 \mathrm{~kW}\) (d) \(73.2 \mathrm{~kW}\) (e) \(80.0 \mathrm{~kW}\)

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