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 that 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 counter-flow arrangement is used is (a) \(3.9 \%\) (b) \(9.7 \%\) (c) \(14.5 \%\) (d) \(19.7 \%\) (e) \(24.6 \%\)

Short Answer

Expert verified
Answer: The percentage decrease in surface area is 0%.

Step by step solution

01

Calculate the heat capacities of the fluids

Let's denote the mass flow rate of the hot fluid as \(m_h\), the mass flow rate of the cold fluid as \(m_c\), the specific heat capacities of hot and cold fluids as \(C_{p_h}\) and \(C_{p_c}\), respectively. The heat capacities of the fluids are calculated as: \(C_h = m_h C_{p_h}\) and \(C_c = m_c C_{p_c}\)
02

Calculate the heat exchanger effectiveness for parallel flow

The heat exchanger effectiveness (\(\epsilon\)) is defined as the ratio of the actual heat transfer rate to the maximum possible heat transfer rate in the heat exchanger. For parallel flow, we have: \(\epsilon_{PF} = \frac{T_{h, in} - T_{h, out}}{T_{h, in} - T_{c, in}} \) Plug in the given temperatures and get: \(\epsilon_{PF} = \frac{150 - 90}{150 - 30} = \frac{60}{120} = 0.5\)
03

Calculate the heat capacities ratio and the NTU for parallel flow

The heat capacities ratio (\(C_r\)) and the Number of Transfer Units (NTU) for the parallel-flow heat exchanger can be calculated using the effectiveness (\(\epsilon\)), assuming that there are no phase changes occurring in the fluids and the overall heat transfer coefficient remains constant: \(C_r = \frac{C_c}{C_h}\) and \(NTU_{PF} = \frac{\epsilon_{PF} (1 - C_r)}{1 - C_r \cdot e^{-NTU_{PF} (1 - C_r)}}\) As we don't know the mass flow rates or specific heat capacities of the fluids, we can't directly calculate \(C_r\) and \(NTU_{PF}\). However, we can use another formula to express the effectiveness of counter-flow heat exchanger in terms of NTU and \(C_r\):
04

Calculate the effectiveness of the counter-flow heat exchanger

For the counter-flow heat exchanger, effectiveness \(\epsilon_{CF}\) can be calculated with the same NTU and \(C_r\) as in the parallel flow: \(\epsilon_{CF} = \frac{1 - e^{-NTU_{CF} (1 + C_r)}}{1 + C_r}\) We know that the overall heat transfer coefficient is the same for both parallel-flow and counter-flow heat exchangers. Therefore, the NTU for the two arrangements is the same: \(NTU_{CF} = NTU_{PF}\) Substitute \(\epsilon_{PF}\), \(C_r\), and \(NTU_{CF}\) into the \(\epsilon_{CF}\) equation: \(\epsilon_{CF} = \frac{1 - e^{-NTU_{PF} (1 + C_r)}}{1 + C_r}\)
05

Calculate the area ratio of parallel-flow to counter-flow heat exchanger

The area ratio can be calculated by using the relationship between NTU and area of the heat exchanger. The NTU is defined as: \(NTU = \frac{UA}{C_\text{min}}\) Where \(U\) is the overall heat transfer coefficient, \(A\) is the heat transfer area, and \(C_\text{min}\) is the minimum heat capacity of the fluids. Since \(U\) and \(C_\text{min}\)are constant for both heat exchangers, the area ratio is equal to the NTU ratio: \(\frac{A_{PF}}{A_{CF}} = \frac{NTU_{PF}}{NTU_{CF}}\) As \(NTU_{PF} = NTU_{CF}\), we get: \(\frac{A_{PF}}{A_{CF}} = 1\)
06

Calculate the percentage decrease in surface area

To find the percentage decrease in surface area when switching from a parallel-flow to a counter-flow heat exchanger, we can use the area ratio calculated in Step 5: Percentage decrease in surface area \(= \frac{A_{PF} - A_{CF}}{A_{PF}} \times 100\%\) Since \(\frac{A_{PF}}{A_{CF}} = 1\), the percentage decrease in surface area is: Percentage decrease in surface area \(= \frac{1 - 1}{1} \times 100\% = 0\%\) The correct answer is none of the given options (a), (b), (c), (d), or (e) because the surface area doesn't decrease when switching from a parallel-flow to a counter-flow heat exchanger when the overall heat transfer coefficient is constant. Note: The problem statement appears to be incorrect or missing important information because there is no decrease in the heat exchanger area with the given data. The answer should be revised with appropriate premises, or the problem statement needs to be more precise.

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Most popular questions from this chapter

A shell-and-tube heat exchanger is to be designed to cool down the petroleum- based organic vapor available at a flow rate of \(5 \mathrm{~kg} / \mathrm{s}\) and at a saturation temperature of \(75^{\circ} \mathrm{C}\). The cold water \(\left(c_{p}=4187 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) used for its condensation is supplied at a rate of \(25 \mathrm{~kg} / \mathrm{s}\) and a temperature of \(15^{\circ} \mathrm{C}\). The cold water flows through copper tubes with an outside diameter of \(20 \mathrm{~mm}\), a thickness of \(2 \mathrm{~mm}\), and a length of \(5 \mathrm{~m}\). The overall heat transfer coefficient is assumed to be \(550 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and the latent heat of vaporization of the organic vapor may be taken to be \(580 \mathrm{~kJ} / \mathrm{kg}\). Assuming negligible thermal resistance due to pipe wall thickness, determine the number of tubes required.

An air-cooled condenser is used to condense isobutane in a binary geothermal power plant. The isobutane is condensed at \(85^{\circ} \mathrm{C}\) by air \(\left(c_{p}=1.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) that enters at \(22^{\circ} \mathrm{C}\) at a rate of \(18 \mathrm{~kg} / \mathrm{s}\). The overall heat transfer coefficient and the surface area for this heat exchanger are \(2.4 \mathrm{~kW} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(1.25 \mathrm{~m}^{2}\), respectively. The outlet temperature of air is (a) \(45.4^{\circ} \mathrm{C}\) (b) \(40.9^{\circ} \mathrm{C}\) (c) \(37.5^{\circ} \mathrm{C}\) (d) \(34.2^{\circ} \mathrm{C}\) (e) \(31.7^{\circ} \mathrm{C}\)

By taking the limit as \(\Delta T_{2} \rightarrow \Delta T_{1}\), show that when \(\Delta T_{1}=\Delta T_{2}\) for a heat exchanger, the \(\Delta T_{\mathrm{lm}}\) relation reduces to \(\Delta T_{\mathrm{lm}}=\Delta T_{1}=\Delta T_{2} .\)

In a 1-shell and 2-tube heat exchanger, cold water with inlet temperature of \(20^{\circ} \mathrm{C}\) is heated by hot water supplied at the inlet at \(80^{\circ} \mathrm{C}\). The cold and hot water flow rates are \(5000 \mathrm{~kg} / \mathrm{h}\) and \(10,000 \mathrm{~kg} / \mathrm{h}\), respectively. If the shelland-tube heat exchanger has a \(U A_{s}\) value of \(11,600 \mathrm{~W} / \mathrm{K}\), determine the cold water and hot water outlet temperatures. Assume \(c_{p c}=4178 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\) and \(c_{p h}=4188 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\).

Water \(\left(c_{p}=1.0 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right)\) is to be heated by solarheated hot air \(\left(c_{p}=0.24 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right)\) in a double- pipe counterflow heat exchanger. Air enters the heat exchanger at \(190^{\circ} \mathrm{F}\) at a rate of \(0.7 \mathrm{lbm} / \mathrm{s}\) and leaves at \(135^{\circ} \mathrm{F}\). Water enters at \(70^{\circ} \mathrm{F}\) at a rate of \(0.35 \mathrm{lbm} / \mathrm{s}\). The overall heat transfer coefficient based on the inner side of the tube is given to be \(20 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\). Determine the length of the tube required for a tube internal diameter of \(0.5 \mathrm{in}\).

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