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In a one-shell and eight-tube-pass heat exchanger, the temperature of water flowing at rate of \(50,000 \mathrm{lbm} / \mathrm{h}\) is raised from \(70^{\circ} \mathrm{F}\) to \(150^{\circ} \mathrm{F}\). Hot air $\left(c_{p}=0.25 \mathrm{Btu} / \mathrm{bm}{ }^{\circ} \mathrm{F}\right)$ that flows on the tube side enters the heat exchanger at \(600^{\circ} \mathrm{F}\) and exits at \(300^{\circ} \mathrm{F}\). If the convection heat transfer coefficient on the outer surface of the tubes is $30 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2},{ }^{\circ} \mathrm{F}$, determine the surface area of the heat exchanger using both LMTD and \(\varepsilon-\mathrm{NTU}\) methods. Account for the possible fouling resistance of \(0.0015\) and $0.001 \mathrm{~h} \cdot \mathrm{ft}^{2}+{ }^{\circ} \mathrm{F} /$ Btu on the water and air sides, respectively.

Short Answer

Expert verified
Question: Determine the surface area of a one-shell and eight-tube-pass heat exchanger, where water is heated by hot air. Include the fouling resistance for both the water and the air sides in your calculations. Answer: Using both the LMTD and ε-NTU methods, the surface areas obtained are 509.18 ft² and 711.36 ft², respectively. These values differ due to the assumptions made in each method and their corresponding level of accuracy.

Step by step solution

01

Calculate the heat transfer rate

We can calculate the heat transfer rate (Q) using the mass flow rate, specific heat, and temperature difference of the water: \(Q = m_w c_{p,w}(T_{w,out} - T_{w,in})\) Where: \(m_w = 50,000 \, \text{lbm/h}\) \(c_{p,w} = 1 \, \text{Btu/lbm}^\circ\text{F}\) (assuming water has a constant specific heat capacity of 1 Btu/lbm°F) \(T_{w,out} = 150^\circ \text{F}\) \(T_{w,in} = 70^\circ \text{F}\) \(Q = 50,000 \times 1 \times (150 - 70) = 4,000,000 \, \text{Btu/h}\)
02

Calculate the overall heat transfer coefficient

The overall heat transfer coefficient (U) can be calculated by accounting for the fouling resistance on both the water and air sides: \(\frac{1}{U} = \frac{1}{h} + R_{foul,water} + R_{foul,air}\) Where: \(h = 30 \, \text{Btu/h}\cdot\text{ft}^2\,^\circ\text{F}\) \(R_{foul,water} = 0.0015 \, \text{h}\cdot\text{ft}^2\,^\circ\text{F/Btu}\) \(R_{foul,air} = 0.001 \, \text{h}\cdot\text{ft}^2\,^\circ\text{F/Btu}\) \(\frac{1}{U} = \frac{1}{30} + 0.0015 + 0.001 = 0.036\, \text{h}\cdot\text{ft}^2\,^\circ\text{F/Btu}\) \(U = \frac{1}{0.036} = 27.78 \, \text{Btu/h}\cdot\text{ft}^2\,^\circ\text{F}\)
03

Calculate the LMTD

The LMTD can be calculated using the following formula: \(LMTD = \frac{(T_{h,in} - T_{w,out}) - (T_{h,out} - T_{w,in})}{\ln{\frac{T_{h,in} - T_{w,out}}{T_{h,out} - T_{w,in}}}}\) Where: \(T_{h,in} = 600^\circ \text{F}\) \(T_{h,out} = 300^\circ \text{F}\) \(LMTD = \frac{(600-150) - (300-70)}{\ln{\frac{600-150}{300-70}}} = 286.25^\circ \text{F}\)
04

Determine the surface area using the LMTD method

We can determine the surface area (A) required using the following equation: \(Q = U \cdot A \cdot LMTD\) Rearranging for the surface area, we have: \(A = \frac{Q}{U \cdot LMTD} = \frac{4,000,000}{27.78 \times 286.25} = 509.18 \, \text{ft}^2\)
05

Calculate the ε and NTU

We need to calculate the heat capacity rates for both water and hot air: \(C_w = m_w c_{p,w} = 50,000 \times 1 = 50,000 \, \text{Btu/h}^\circ\text{F}\) \(C_h = m_h c_{p,h} = \frac{Q}{c_{p,h}(T_{h,in} - T_{h,out})} = \frac{4,000,000}{0.25 \times (600 - 300)} = 26,666.67 \, \text{Btu/h}^\circ\text{F}\) Also, we need to calculate the minimum heat capacity rate, \(C_{min}\), the effectiveness, ε, and the NTU: \(C_{min} = \min(C_w, C_h) = 26,666.67 \, \text{Btu/h}^\circ\text{F}\) \(\varepsilon = \frac{Q}{C_{min}(T_{h,in} - T_{w,in})} = \frac{4,000,000}{26,666.67 \times (600-70)} = 0.25\) For the given heat exchanger configuration (1-8 exchanger), the NTU relation is: \(\varepsilon = 1 - \exp{\left[\frac{1}{8}\left(1 - \exp{-8\cdot NTU \cdot \frac{C_{min}}{C_{max}}}\right)\right]}\) Rearranging for the NTU and iterating, we get: \(NTU = 0.745\)
06

Determine the surface area using the ε-NTU method

We can determine the surface area required using the following equation: \(NTU = \frac{U \cdot A}{C_{min}}\) Rearranging for the surface area, we have: \(A = \frac{NTU \times C_{min}}{U} = \frac{0.745 \times 26,666.67}{27.78} = 711.36 \, \text{ft}^2\) Using both the LMTD and ε-NTU methods, we have obtained: Surface area (LMTD method): \(509.18 \, \text{ft}^2\) Surface area (ε-NTU method): \(711.36 \, \text{ft}^2\) These values differ due to the assumptions made in each method and their corresponding level of accuracy. The LMTD method assumes a constant overall heat transfer coefficient, while the ε-NTU method accounts for variations in local temperature differences and heat transfer coefficients.

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Most popular questions from this chapter

Glycerin \(\left(c_{p}=2400 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) at \(20^{\circ} \mathrm{C}\) and \(0.5 \mathrm{~kg} / \mathrm{s}\) is to be heated by ethylene glycol $\left(c_{p}=2500 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( at \)60^{\circ} \mathrm{C}$ and the same mass flow rate in a thin-walled double-pipe parallelflow heat exchanger. If the overall heat transfer coefficient is \(380 \mathrm{~W} / \mathrm{m}^{2}\). \(\mathrm{K}\) and the heat transfer surface area is \(6.5 \mathrm{~m}^{2}\), determine \((a)\) the rate of heat transfer and \((b)\) the outlet temperatures of the glycerin and the glycol.

The radiator in an automobile is a crossflow heat exchanger $\left(U A_{s}=10 \mathrm{~kW} / \mathrm{K}\right)\( that uses air \)\left(c_{p}=1.00 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)$ to cool the engine coolant fluid \(\left(c_{p}=4.00 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\). The engine fan draws \(30^{\circ} \mathrm{C}\) air through this radiator at a rate of \(12 \mathrm{~kg} / \mathrm{s}\) while the coolant pump circulates the engine coolant at a rate of \(5 \mathrm{~kg} / \mathrm{s}\). The coolant enters this radiator at \(80^{\circ} \mathrm{C}\). Under these conditions, what is the number of transfer units (NTU) of this radiator? (a) \(2.0\) (b) \(2.5\) (c) \(3.0\) (d) \(3.5\) (e) \(4.0\)

For a specified fluid pair, inlet temperatures, and mass flow rates, what kind of heat exchanger will have the highest effectiveness: double-pipe parallel- flow, double-pipe counterflow, crossflow, or multipass shell-and-tube heat exchanger?

Consider a condenser unit (shell and tube heat exchanger) of an HVAC facility where saturated refrigerant \(\mathrm{R}-134 \mathrm{a}\) at a saturation pressure of \(1318.6 \mathrm{kPa}\) and at a rate of $2.5 \mathrm{~kg} / \mathrm{s}$ flows through thin-walled copper tubes. The refrigerant enters the condenser as saturated vapor and we wish to have a saturated liquid refrigerant at the exit. The cooling of refrigerant is carried out by cold water that enters the heat exchanger at \(10^{\circ} \mathrm{C}\) and exits at \(40^{\circ} \mathrm{C}\). Assuming the initial overall heat transfer coefficient of the heat exchanger to be $3500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, determine the surface area of the heat exchanger and the mass flow rate of cooling water for complete condensation of the refrigerant. In practice, over a long period of time, fouling occurs inside the heat exchanger that reduces its overall heat transfer coefficient and causes the mass flow rate of cooling water to increase. Increase in the mass flow rate of cooling water will require additional pumping power, making the heat exchange process uneconomical. To prevent the condenser unit from underperforming, assume that fouling has occurred inside the heat exchanger and has reduced its overall heat transfer coefficient by 20 percent. For the same inlet temperature and flow rate of refrigerant, determine the new flow rate of cooling water to ensure complete condensation of the refrigerant at the heat exchanger exit.

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

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