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A pipe system is mainly constructed with ASTM F441 CPVC pipes. The ASME Code for Process Piping (ASME B31.3-2014, Table B-1) recommends that the maximum temperature limit for CPVC pipes be \(93.3^{\circ} \mathrm{C}\). A double-pipe heat exchanger is located upstream of the pipe system to reduce the hot water temperature before it flows into the CPVC pipes. The inner tube of the heat exchanger has a negligible wall thickness, and its length and diameter are $5 \mathrm{~m}\( and \)25 \mathrm{~mm}$, respectively. The convection heat transfer coefficients inside and outside of the heat exchanger inner tube are $3600 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( and \)4500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. The hot fluid enters the heat exchanger at \(105^{\circ} \mathrm{C}\) with a flow rate of $0.75 \mathrm{~kg} / \mathrm{s}$. In the cold fluid stream, water enters the heat exchanger at \(10^{\circ} \mathrm{C}\) and exits at \(80^{\circ} \mathrm{C}\). Determine whether this double-pipe heat exchanger should employ the parallel flow or the counterflow configuration to ensure that the hot water exiting the heat exchanger is \(93.3^{\circ} \mathrm{C}\) or lower.

Short Answer

Expert verified
Answer: Parallel flow configuration should be employed to ensure that the hot water exiting the heat exchanger is at most \(93.3^{\circ} \mathrm{C}\).

Step by step solution

01

Determine the heat transfer area, A

Calculate the heat transfer area using the length and diameter of the inner tube: \(A = \pi d L\), where \(d = 25 \times 10^{-3}\) meters and \(L = 5\) meters \(A = \pi (25 \times 10^{-3})(5) = 0.3927~ \mathrm{m}^2\).
02

Calculate the overall heat transfer coefficient, U

To find the overall heat transfer coefficient, U, use the given convection heat transfer coefficients inside and outside of the heat exchanger inner tube: \(\frac{1}{U} = \frac{1}{h_{i}} + \frac{1}{h_{o}}\), where \(h_{i} = 3600~ \mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(h_{o} = 4500~ \mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) \(U = \frac{1}{\frac{1}{3600}+\frac{1}{4500}} = 2083.33~ \mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\).
03

Determine the heat transfer rate, q

The hot fluid enters the heat exchanger at \(T_{h1} = 105^{\circ} \mathrm{C}\) and leaves at \(T_{h2}=93.3^{\circ} \mathrm{C}\). The cold fluid enters at \(T_{c1} = 10^{\circ} \mathrm{C}\) and leaves at \(T_{c2} = 80^{\circ} \mathrm{C}\). The flow rate, \(\dot{m_{h}} = 0.75~\mathrm{kg}/\mathrm{s}\), and the specific heat, \(c_{p} = 4.18~\mathrm{kJ}/\mathrm{kg}\cdot\mathrm{K}\). Calculate the heat transfer rate using the hot fluid values: \(q = \dot{m_{h}}c_{p}(T_{h1}-T_{h2})\) \(q = (0.75~\mathrm{kg}/\mathrm{s})(4.18~\mathrm{kJ}/\mathrm{kg}\cdot\mathrm{K})(105-93.3)\) \(q = 36.6~\mathrm{kW} = 36600~\mathrm{W}\).
04

Determine the temperature difference between the hot and cold fluids in the parallel-flow configuration

In parallel flow configuration, the cold fluid temperature difference is: \(\Delta T_{c}^{\mathrm{parallel}} = T_{c2} - T_{c1} = 80^{\circ} \mathrm{C} - 10^{\circ} \mathrm{C} = 70^{\circ} \mathrm{C}\).
05

Determine the heat transfer rate in the parallel-flow configuration, q_parallel

Calculate the heat transfer rate for this temperature difference using the overall heat transfer coefficient and the heat transfer area found in Steps 1 and 2: \(q_{\mathrm{parallel}} = U A \Delta T_{c}^{\mathrm{parallel}}\) \(q_{\mathrm{parallel}} = (2083.33~\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K})(0.3927~\mathrm{m}^{2})(70~\mathrm{K})\) \(q_{\mathrm{parallel}} = 57577.3~\mathrm{W}\).
06

Determine the effectiveness of parallel flow configuration

Check if \(q_{\mathrm{parallel}} > q\) to see whether the parallel flow configuration will be effective in maintaining hot water exit temperature at \(93.3^{\circ} \mathrm{C}\) or lower: \(57577.3~\mathrm{W} > 36600~\mathrm{W}\). The parallel flow configuration is effective, and the hot fluid exit temperature will be \(\leq 93.3^{\circ} \mathrm{C}\).
07

Conclusion

The parallel flow configuration for the double-pipe heat exchanger should be employed to ensure that the hot water exiting the heat exchanger is at most \(93.3^{\circ} \mathrm{C}\).

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Most popular questions from this chapter

Can the temperature of the hot fluid drop below the inlet temperature of the cold fluid at any location in a heat exchanger? Explain.

Cold water $\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( enters a counterflow heat exchanger at \)10^{\circ} \mathrm{C}\( at a rate of \)0.35 \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 \(1.9 \mathrm{~kg} / \mathrm{s}\) and leaves at $25^{\circ} \mathrm{C}$. The effectiveness of this heat exchanger is (a) \(0.50\) (b) \(0.63\) (c) \(0.72\) (d) \(0.81\) (e) \(0.89\)

A crossflow 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.

Consider a recuperative crossflow heat exchanger (both fluids unmixed) used in a gas turbine system that carries the exhaust gases at a flow rate of $7.5 \mathrm{~kg} / \mathrm{s}\( and a temperature of \)500^{\circ} \mathrm{C}$. The air initially at \(30^{\circ} \mathrm{C}\) and flowing at a rate of $15 \mathrm{~kg} / \mathrm{s}$ is to be heated in the recuperator. The convective heat transfer coefficients on the exhaust gas and air sides are $750 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( and \)300 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$, respectively. Due to long-term use of the gas turbine, the recuperative heat exchanger is subject to fouling on both gas and air sides that offers a resistance of \(0.0004\) \(\mathrm{m}^{2}\). $/ \mathrm{W}$ each. Take the properties of exhaust gas to be the same as that of air \(\left(c_{p}=1069 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\). If the exit temperature of the exhaust gas is \(320^{\circ} \mathrm{C}\), determine \((a)\) if the air could be heated to a temperature of \(150^{\circ} \mathrm{C}\) and \((b)\) the area of the heat exchanger. (c) If the answer to part \((a)\) is no, then determine what should be the air mass flow rate in order to attain the desired exit temperature of \(150^{\circ} \mathrm{C}\) and \((d)\) plot the variation of the exit air temperature over a range of \(75^{\circ} \mathrm{C}\) to \(300^{\circ} \mathrm{C}\) with the air mass flow rate, assuming all the other conditions remain the same.

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