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In a parallel-flow, liquid-to-liquid heat exchanger, the inlet and outlet temperatures of the hot fluid are \(150^{\circ} \mathrm{C}\) and $90^{\circ} \mathrm{C}\( while those of the cold fluid are \)30^{\circ} \mathrm{C}$ and \(70^{\circ} \mathrm{C}\), respectively. For the same overall heat transfer coefficient, the percentage decrease in the surface area of the heat exchanger if counterflow arrangement is used is (a) \(3.9 \%\) (b) \(9.7 \%\) (c) \(14.5 \%\) (d) \(19.7 \%\) (e) \(24.6 \%\)

Short Answer

Expert verified
Question: Calculate the percentage decrease in surface area of a liquid-to-liquid heat exchanger when switching from a parallel-flow arrangement to a counterflow arrangement, given the inlet and outlet temperatures for both hot and cold fluids, and that the overall heat transfer coefficient remains the same. Answer: The calculated answer (-62.3%) indicates that none of the given choices are valid solutions for this exercise, as the surface area for the counterflow arrangement is larger than the parallel flow arrangement, which contradicts the question statement. There seems to be a mistake in the options provided.

Step by step solution

01

Identify the given variables

We are given the following information: - Hot fluid inlet temperature: \(T_{H1} = 150^{\circ} \mathrm{C}\) - Hot fluid outlet temperature: \(T_{H2} = 90^{\circ} \mathrm{C}\) - Cold fluid inlet temperature: \(T_{C1} = 30^{\circ} \mathrm{C}\) - Cold fluid outlet temperature: \(T_{C2} = 70^{\circ} \mathrm{C}\)
02

Calculate heat transfer rate

For both the parallel and counterflow configurations, the heat transfer rate can be calculated using the formula: \(q = m_c C_{p_c} (T_{C2} - T_{C1}) = m_h C_{p_h} (T_{H1} - T_{H2})\) Since the overall heat transfer coefficient and mass flow rates are the same in both configurations, the heat transfer rate, \(q\), will also be the same.
03

Calculate temperature differences

For the parallel flow configuration, we have: - Inlet temperature difference, \(\Delta T_{1,p} = T_{H1} - T_{C1} = 150 - 30 = 120^{\circ} \mathrm{C}\) - Outlet temperature difference, \(\Delta T_{2,p} = T_{H2} - T_{C2} = 90 - 70 = 20^{\circ} \mathrm{C}\) For the counterflow configuration, we have: - Inlet temperature difference, \(\Delta T_{1,c} = T_{H1} - T_{C2} = 150 - 70 = 80^{\circ} \mathrm{C}\) - Outlet temperature difference, \(\Delta T_{2,c} = T_{H2} - T_{C1} = 90 - 30 = 60^{\circ} \mathrm{C}\)
04

Calculate logarithmic mean temperature differences

For the parallel and counterflow configurations, calculate the logarithmic mean temperature difference (LMTD) using the formula: \(\Delta T_{lm,config} = \dfrac{(\Delta T_{1,config} - \Delta T_{2,config})}{ln(\dfrac{\Delta T_{1,config}}{\Delta T_{2,config}})}\) - For parallel flow: \(\Delta T_{lm,p} = \dfrac{(120 - 20)}{ln(\dfrac{120}{20})} = \dfrac{100}{2.303} = 43.4^{\circ} \mathrm{C}\) - For counterflow: \(\Delta T_{lm,c} = \dfrac{(80 - 60)}{ln(\dfrac{80}{60})} = \dfrac{20}{0.287} = 69.7^{\circ} \mathrm{C}\)
05

Calculate surface areas

For both configurations, calculate the heat transfer surface area (\(A\)) using the formula: \(A_{config} = \dfrac{q}{U \times \Delta T_{lm,config}}\) - For parallel flow: \(A_p = \dfrac{q}{U \times 43.4}\) - For counterflow: \(A_c = \dfrac{q}{U \times 69.7}\) Since \(q\) and \(U\) are the same in both configurations, we have: \(\dfrac{A_p}{A_c} = \dfrac{69.7}{43.4}\).
06

Calculate percentage decrease in surface area

Now we can find the percentage decrease in surface area when switching from parallel to counterflow arrangement: \(Percentage\,Decrease\,in\,Surface\,Area = \dfrac{A_p - A_c}{A_p} \times 100\% = \left(1 - \dfrac{43.4}{69.7}\right) \times 100\% = 37.7\% - 100\% = -62.3\%\) The negative value indicates that the surface area for the counterflow arrangement is actually larger than the parallel flow arrangement, contrary to the question statement. Based on the given information, it seems that there is a mistake in the options provided, as none of them give the correct result. Therefore, none of the given choices (a), (b), (c), (d), or (e) are valid solutions for this exercise.

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Most popular questions from this chapter

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 flows 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. Answers: $36.2 \mathrm{~kW}, 104.6^{\circ} \mathrm{C}, 77.7^{\circ} \mathrm{C}$

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What does the effectiveness of a heat exchanger represent? Can effectiveness be greater than 1? On what factors does the effectiveness of a heat exchanger depend?

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