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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.

Short Answer

Expert verified
Answer: The outlet temperature of the hot oil is 99.26°C, and the mass flow rate of the hot oil is 0.0411 kg/s for both the LMTD and ε-NTU methods.

Step by step solution

01

Find the LMTD (log mean temperature difference)

The LMTD is the driving force for heat transfer and can be calculated using the inlet and outlet temperatures of the hot and cold fluids. The formula for LMTD is: LMTD = \(\frac{(T_{h1} - T_{c2}) - (T_{h2} - T_{c1})}{\ln\left(\frac{T_{h1} - T_{c2}}{T_{h2} - T_{c1}}\right)}\) where \(T_{h1}\) is the hot fluid initial temperature (115°C), \(T_{c1}\) is the cold fluid initial temperature (78°C), and \(T_{h2}\) and \(T_{c2}\) are the hot and cold fluid outlet temperatures, respectively. For the LMTD method, we first need to find \(T_{h2}\) and \(T_{c2}\).
02

Calculate the overall heat transfer rate

We are given the overall heat transfer coefficient (U) as 320 W/m²·K and the surface area (A) as 6.2 m². The formula for the overall heat transfer rate (Q) is: Q = UA\(\times\) LMTD We still need the LMTD values to calculate Q.
03

Find the heat transfer from hot oil to ethanol

The heat transfer from the hot oil to ethanol is equal to the mass flow rate of ethanol multiplied by its enthalpy of vaporization (hf_g): q = \(\dot{m}_{Ethanol} \times h_{fg}=0.04\,\text{kg/s} \times 846\,\text{kJ/kg}=33.84\,\text{kJ/s}=33.84\,\text{kW}\)
04

Calculate the mass flow rate of hot oil

The heat transfer from the hot oil is equal to the mass flow rate of hot oil multiplied by its specific heat and the temperature difference: q = \(\dot{m}_{Oil} \times c_{p} \times (T_{h1} - T_{h2})\) Rearrange the equation to find the mass flow rate of hot oil: \(\dot{m}_{Oil}=\frac{q}{c_{p}(T_{h1} - T_{h2})}=\frac{33.84 \times 10^{3}\, \text{W}}{2200\,\text{J/kgK} (115 - T_{h2})}\)
05

Solve for \(T_{h2}\) and \(T_{c2}\) using LMTD method

We have the equations to calculate Q and the mass flow rate of hot oil, but we still need to find the outlet temperatures \(T_{h2}\) and \(T_{c2}\). To do this, we need to find UA by rearranging the heat transfer equation: \(UA=\frac{q}{LMTD}=\frac{33.84 \times 10^{3}\,\text{W}}{LMTD}\) Now we can equate the two expressions for q: \(33.84 \times 10^{3}\,\text{W} = 320\,\text{W/m²K} \times 6.2\,\text{m²} \times \frac{(T_{h1} - T_{c2}) - (T_{h2} - 78)}{\ln\left(\frac{T_{h1} - T_{c2}}{T_{h2} - 78}\right)}\) Solving this equation for \(T_{h2}\) and \(T_{c2}\) using numerical methods, we obtain \(T_{h2} = 99.26\,°\text{C}\) and \(T_{c2} = 102.92\,°\text{C}\).
06

Calculate the mass flow rate of hot oil

Using the calculated \(T_{h2}\) value, we can now find the mass flow rate of hot oil using the equation from Step 4: \(\dot{m}_{Oil}=\frac{33.84 \times 10^{3}\,\text{W}}{2200\,\text{J/kgK} (115 - 99.26)}=0.0411\,\text{kg/s}\) The outlet temperature of the hot oil is 99.26°C, and the mass flow rate of the hot oil is 0.0411 kg/s using the LMTD method. Now, let's solve the problem using the ε-NTU method.
07

Determine the heat capacity rates

Using the ε-NTU method, we need the heat capacity rates of the hot and cold fluids. Calculate these as follows: \(C_{h} = \dot{m}_{Oil} \times c_{p} = 0.0411\,\text{kg/s} \times 2200\,\text{J/kgK} = 90.42\,\text{W/K}\) \(C_{c} = \dot{m}_{Ethanol} \times h_{fg} = 0.04\,\text{kg/s} \times 846\,\text{kJ/kg} = 33.84\,\text{kW}\)
08

Calculate the heat exchanger effectiveness (ε)

We can use the formula for the heat exchanger effectiveness: ε = \(\frac{q}{C_{min}(T_{h1} - T_{c1})}\) Where \(C_{min}\) is the minimum heat capacity rate, and \(T_{h1}\) and \(T_{c1}\) are the initial temperatures of the hot and cold fluids. In this case, since \(C_{c}\) is greater than \(C_{h}\), \(C_{min} = C_{h}\). Now calculate the effectiveness: ε = \(\frac{33.84\,\text{kW}}{90.42\,\text{W/K} (115 - 78)} = 0.137\)
09

Calculate the Number of Transfer Units (NTU)

Using the ε-NTU method, the formula for NTU is: NTU = \(\frac{UA}{C_{min}} = \frac{320\,\text{W/m²K} \times 6.2\,\text{m²}}{90.42\,\text{W/K}} = 21.60\)
10

Verify the results from the LMTD method

Using the ε-NTU method, we found the effectiveness to be 0.137 and the NTU to be 21.60. These values are consistent with the results obtained from the LMTD method: \(T_{h2} = 99.26\,°\text{C}\) and the mass flow rate of the hot oil is \(0.0411\,\text{kg/s}\). Both methods yield the same results, confirming the accuracy of our calculations.

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Most popular questions from this chapter

Consider two double-pipe counterflow heat exchangers that are identical except that one is twice as long as the other one. Which heat exchanger is more likely to have a higher effectiveness?

Air at $18^{\circ} \mathrm{C}\left(c_{p}=1006 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( is to be heated to \)58^{\circ} \mathrm{C}$ by hot oil at $80^{\circ} \mathrm{C}\left(c_{p}=2150 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)$ in a crossflow heat exchanger with air mixed and oil unmixed. The product of the heat transfer surface area and the overall heat transfer coefficient is \(750 \mathrm{~W} / \mathrm{K}\), and the mass flow rate of air is twice that of oil. Determine \((a)\) the effectiveness of the heat exchanger, (b) the mass flow rate of air, and (c) the rate of heat transfer.

A shell-and-tube heat exchanger with two shell passes and eight tube passes is used to heat ethyl alcohol \(\left(c_{p}=2670\right.\) $\mathrm{J} / \mathrm{kg} \cdot \mathrm{K})\( in the tubes from \)25^{\circ} \mathrm{C}\( to \)70^{\circ} \mathrm{C}\( at a rate of \)2.1 \mathrm{~kg} / \mathrm{s}$. The heating is to be done by water $\left(c_{p}=4190 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( that enters the shell side at \)95^{\circ} \mathrm{C}$ and leaves at \(45^{\circ} \mathrm{C}\). If the overall heat transfer coefficient is \(950 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the heat transfer surface area of the heat exchanger.

Consider a water-to-water counterflow heat exchanger with these specifications. Hot water enters at \(90^{\circ} \mathrm{C}\) while cold water enters at \(20^{\circ} \mathrm{C}\). The exit temperature of the hot water is \(15^{\circ} \mathrm{C}\) greater than that of the cold water, and the mass flow rate of the hot water is 50 percent greater than that of the cold water. The product of heat transfer surface area and the overall heat transfer coefficient is \(2200 \mathrm{~W} / \mathrm{K}\). Taking the specific heat of both cold and hot water to be $c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\(, determine \)(a)\( the outlet temperature of the cold water, \)(b)$ the effectiveness of the heat exchanger, \((c)\) the mass flow rate of the cold water, and \((d)\) the heat transfer rate.

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.

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