Water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters the \(2.5\)-cm-internaldiameter tube of a double-pipe counter-flow heat exchanger at \(17^{\circ} \mathrm{C}\) at a rate of \(1.8 \mathrm{~kg} / \mathrm{s}\). Water is heated by steam condensing at \(120^{\circ} \mathrm{C}\left(h_{f g}=2203 \mathrm{~kJ} / \mathrm{kg}\right)\) in the shell. If the overall heat transfer coefficient of the heat exchanger is \(700 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the length of the tube required in order to heat the water to \(80^{\circ} \mathrm{C}\) using ( \(a\) ) the LMTD method and \((b)\) the \(\varepsilon-\mathrm{NTU}\) method.

Short Answer

Expert verified
The required length of the tube to effectively heat water from 17°C to 80°C using both the LMTD or ε-NTU methods is approximately 13.56 meters.

Step by step solution

01

1. Calculate the mass flow rate of water

Since the mass flow rate of water is given (\(1.8\,\text{kg/s}\)), no calculations are required for this step.
02

2. Calculate the heat transfer required to reach target temperature

We need to find out the heat transfer required to heat the water from \(17^\circ\text{C}\) to \(80^\circ\text{C}\). We can calculate this using the formula: \(Q = m \cdot c_p \cdot \Delta T\), where \(Q\) is the heat transfer, \(m\) is the mass flow rate, \(c_p\) is the specific heat capacity of the water, and \(\Delta T\) is the temperature difference. \(\Delta T = 80^\circ\text{C} - 17^\circ\text{C} = 63^\circ\text{C}\) \(Q = 1.8\,\text{kg/s} \cdot 4180\,\text{J/kg}\cdot\text{K} \cdot 63\,\text{K} = 473076\,\text{W}\) The required heat transfer is \(473076\,\text{W}\).
03

3. Find the temperature difference for LMTD method

To evaluate the LMTD, the hot and cold outlet temperatures must be estimated. The steam condenses at a constant temperature of \(120^\circ\text{C}\). Assuming the steam temperature (\(T_h\)) remains constant throughout the process, the temperature difference at the inlet (\(\Delta T_1\)) and outlet (\(\Delta T_2\)) can be calculated as follows: \(\Delta T_1 = T_h - T_{c1} = 120^\circ\text{C} - 17^\circ\text{C} = 103^\circ\text{C}\) \(\Delta T_2 = T_h - T_{c2} = 120^\circ\text{C} - 80^\circ\text{C} = 40^\circ\text{C}\)
04

4. Calculate LMTD and find the tube length using LMTD method

Now, we can find the Logarithmic Mean Temperature Difference (LMTD) using the formula: \(\mathrm{LMTD} = \frac{\Delta T_1 - \Delta T_2}{\ln \left(\frac{\Delta T_1}{\Delta T_2}\right)}\) \(\mathrm{LMTD} = \frac{103^\circ\text{C} - 40^\circ\text{C}}{\ln \left(\frac{103^\circ\text{C}}{40^\circ\text{C}}\right)} = 63.76^\circ\text{C}\) The heat transfer area \(A\) can be calculated using the formula: \(Q = U \cdot A \cdot \mathrm{LMTD}\), where \(U\) is the overall heat transfer coefficient. Rearranging the formula to calculate \(A\), we get: \(A = \frac{Q}{U \cdot \mathrm{LMTD}} = \frac{473076\,\text{W}}{700\,\text{W/m}^2\cdot\text{K} \cdot 63.76\,\text{K}} = 1.067\,\text{m}^2\) The internal diameter of the tube is given. To find the length of the tube, we use the formula for the surface area of the tube: \(A = \pi d L\), where \(d\) is the diameter, and \(L\) is the length. We can solve for \(L\): \(L = \frac{A}{\pi d} = \frac{1.067\,\text{m}^2}{\pi \cdot 0.025\,\text{m}} \approx 13.56\,\text{m}\) So, the length of the tube required using the LMTD method is approximately \(13.56\,\text{m}\).
05

5. Calculate the NTU using ε-NTU method

The number of transfer units (\(\mathrm{NTU}\)) can be calculated with the formula: \(\mathrm{NTU} = \frac{UA}{mc_p}\), where \(U\), \(A\), \(m\), and \(c_p\) are the overall heat transfer coefficient, heat transfer area, mass flow rate, and specific heat capacity of water, respectively. Using the values from the LMTD section, we get: \(\mathrm{NTU} = \frac{700\,\text{W/m}^2\cdot\text{K} \cdot 1.067\,\text{m}^2}{1.8\,\text{kg/s} \cdot 4180\,\text{J/kg}\cdot\text{K}} \approx 0.056\)
06

6. Calculate the effectiveness and find the tube length using ε-NTU method

The effectiveness (\(\varepsilon\)) can be calculated using the formula: \(\varepsilon = \frac{Q_{actual}}{Q_{max}}\), where \(Q_{actual}\) and \(Q_{max}\) are the actual and maximum possible heat transfers, respectively. Since the outlet coolant temperature is given, we can calculate the actual heat transfer: \(Q_{actual} = m c_p (T_{c2} - T_{c1}) = 1.8\,\text{kg/s} \cdot 4180\,\text{J/kg}\cdot\text{K} \cdot (80^\circ\text{C} - 17^\circ\text{C})= 473076\,\text{W}\) The maximum possible heat transfer occurs when the coolant reaches the temperature of steam: \(Q_{max} = m c_p (T_h - T_{c1}) = 1.8\,\text{kg/s} \cdot 4180\,\text{J/kg}\cdot\text{K} \cdot (120^\circ\text{C} - 17^\circ\text{C})= 627096\,\text{W}\) \(\varepsilon = \frac{473076\,\text{W}}{627096\,\text{W}} \approx 0.754\) We can use the effectiveness-NTU relation to check the NTU value: \(\varepsilon = 1 - \exp\left(-\frac{1}{c} \cdot \left(1 - \exp(-c\,\mathrm{NTU})\right)\right)\), where \(c = \frac{mc_p}{U\cdot A}\) Using the given values, \(c = \frac{1.8\,\text{kg/s}\cdot 4180\,\text{J/kg}\cdot\text{K}}{700\,\text{W/m}^2\cdot\text{K} \cdot 1.067\,\text{m}^2} \approx 17.77\) Solving for NTU, we obtain \(\mathrm{NTU} \approx 0.056\), which agrees with the value we calculated earlier. Now, we can calculate the heat transfer area using the NTU and ε values: \(A = \frac{m c_p}{U \cdot \mathrm{NTU}} = \frac{1.8\,\text{kg/s} \cdot 4180\,\text{J/kg}\cdot\text{K}}{700\,\text{W/m}^2\cdot\text{K} \cdot 0.056} \approx 1.067\,\text{m}^2\) Finally, the tube length can be found using the same formula as in the LMTD method: \(L = \frac{A}{\pi d} = \frac{1.067\,\text{m}^2}{\pi \cdot 0.025\,\text{m}} \approx 13.56\,\text{m}\) So, the length of the tube required using the ε-NTU method is approximately \(13.56\,\text{m}\).

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

A counter-flow heat exchanger is used to cool oil \(\left(c_{p}=\right.\) \(2.20 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K})\) from \(110^{\circ} \mathrm{C}\) to \(85^{\circ} \mathrm{C}\) at a rate of \(0.75 \mathrm{~kg} / \mathrm{s}\) by cold water \(\left(c_{p}=4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) that enters the heat exchanger at \(20^{\circ} \mathrm{C}\) at a rate of \(0.6 \mathrm{~kg} / \mathrm{s}\). If the overall heat transfer coefficient is \(800 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), the heat transfer area of the heat exchanger is (a) \(0.745 \mathrm{~m}^{2}\) (b) \(0.760 \mathrm{~m}^{2}\) (c) \(0.775 \mathrm{~m}^{2}\) (d) \(0.790 \mathrm{~m}^{2}\) (e) \(0.805 \mathrm{~m}^{2}\)

Can the temperature of the cold fluid rise above the inlet temperature of the hot 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 \(18^{\circ} \mathrm{C}\) at a rate of \(0.7 \mathrm{~kg} / \mathrm{s}\) 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 \(1.6 \mathrm{~kg} / \mathrm{s}\) and leaves at \(25^{\circ} \mathrm{C}\). The maximum possible outlet temperature of the cold water is (a) \(25.0^{\circ} \mathrm{C}\) (b) \(32.0^{\circ} \mathrm{C}\) (c) \(35.5^{\circ} \mathrm{C}\) (d) \(39.7^{\circ} \mathrm{C}\) (e) \(50.0^{\circ} \mathrm{C}\)

A shell-and-tube heat exchanger with 2-shell passes and 4-tube passes is used for cooling oil \(\left(c_{p}=2.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) from \(125^{\circ} \mathrm{C}\) to \(55^{\circ} \mathrm{C}\). The coolant is water, which enters the shell side at \(25^{\circ} \mathrm{C}\) and leaves at \(46^{\circ} \mathrm{C}\). The overall heat transfer coefficient is \(900 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). For an oil flow rate of \(10 \mathrm{~kg} / \mathrm{s}\), calculate the cooling water flow rate and the heat transfer area.

A 1-shell-pass and 8-tube-passes heat exchanger is used to heat glycerin \(\left(c_{p}=0.60 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right)\) from \(65^{\circ} \mathrm{F}\) to \(140^{\circ} \mathrm{F}\) by hot water \(\left(c_{p}=1.0 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right)\) that enters the thinwalled \(0.5\)-in-diameter tubes at \(175^{\circ} \mathrm{F}\) and leaves at \(120^{\circ} \mathrm{F}\). The total length of the tubes in the heat exchanger is \(500 \mathrm{ft}\). The convection heat transfer coefficient is \(4 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\) on the glycerin (shell) side and \(50 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\) on the water (tube) side. Determine the rate of heat transfer in the heat exchanger \((a)\) before any fouling occurs and \((b)\) after fouling with a fouling factor of \(0.002 \mathrm{~h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F} /\) Btu on the outer surfaces of the tubes.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free