Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

A shell-and-tube heat exchanger is used for heating $14 \mathrm{~kg} / \mathrm{s}\( of oil \)\left(c_{p}=2.0 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\( from \)20^{\circ} \mathrm{C}\( to \)46^{\circ} \mathrm{C}$. The heat exchanger has one shell pass and six tube passes. Water enters the shell side at \(80^{\circ} \mathrm{C}\) and leaves at \(60^{\circ} \mathrm{C}\). The overall heat transfer coefficient is estimated to be $1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Calculate the rate of heat transfer and the heat transfer area.

Short Answer

Expert verified
Question: Calculate the heat transfer rate and the heat transfer area of a shell-and-tube heat exchanger given the following information: the mass flow rate of oil is 14 kg/s, the specific heat capacity of oil is 2.0 kJ/kg·K, the initial and final temperatures of the oil are 20°C and 46°C, the overall heat transfer coefficient is 1000 W/m²·K, and the initial and final temperatures of the water in the shell side are 80°C and 60°C. Answer: The heat transfer rate of the shell-and-tube heat exchanger is 728,000 W, and the heat transfer area is 15.83 m².

Step by step solution

01

Calculate the rate of heat transfer using the oil data

We know that the mass flow rate of oil is \(14\,\mathrm{kg/s}\), the specific heat capacity is \(2.0\,\mathrm{kJ/kg\cdot K}\) and the initial and final temperatures are \(T_{1} = 20^{\circ}\mathrm{C}\) and \(T_{2} = 46^{\circ}\mathrm{C}\) respectively. We can now calculate the rate of heat transfer using the oil data: \(Q = mc_p(T_2-T_1) = 14\,\mathrm{kg/s} \cdot 2.0\,\mathrm{kJ/kg\cdot K} \cdot (46^{\circ}\mathrm{C} - 20^{\circ}\mathrm{C})\) Convert the specific heat capacity to \(\mathrm{W/kg\cdot K}\): \(2.0\,\mathrm{kJ/kg\cdot K} \cdot \frac{1000\,\mathrm{W}}{1\,\mathrm{kJ}} = 2000\,\mathrm{W/kg\cdot K}\) Now, plug in the converted specific heat capacity: \(Q = 14\,\mathrm{kg/s} \cdot 2000\,\mathrm{W/kg\cdot K} \cdot (46^{\circ}\mathrm{C} - 20^{\circ}\mathrm{C}) = 14\,\mathrm{kg/s} \cdot 2000\,\mathrm{W/kg\cdot K} \cdot 26\,\mathrm{K} = 728,000\,\mathrm{W}\) The rate of heat transfer using the oil data is \(728,000\,\mathrm{W}\).
02

Calculate the temperature difference across the heat exchanger

We are given the initial and final temperatures of the water entering and leaving the shell side of the heat exchanger as \(80^{\circ}\mathrm{C}\) and \(60^{\circ}\mathrm{C}\). The temperature difference across the heat exchanger (minimum temperature change) can be calculated as follows: \(\Delta T = T_{\mathrm{water}} - T_{\mathrm{oil}} = (80^{\circ}\mathrm{C} - 20^{\circ}\mathrm{C}) - (60^{\circ}\mathrm{C} - 46^{\circ}\mathrm{C}) = 60^{\circ}\mathrm{C} - 14^{\circ}\mathrm{C} = 46\,\mathrm{K}\) The temperature difference across the heat exchanger is \(46\,\mathrm{K}\).
03

Calculate the heat transfer area using the overall heat transfer coefficient and the rate of heat transfer

We are given the overall heat transfer coefficient as \(1000\,\mathrm{W/m^2\cdot K}\). Now we can calculate the heat transfer area using the previously calculated rate of heat transfer \(Q = 728,000\,\mathrm{W}\) and the temperature difference \(\Delta T = 46\,\mathrm{K}\): \(A = \frac{Q}{U\Delta T} = \frac{728,000\,\mathrm{W}}{1000\,\mathrm{W/m^2\cdot K} \cdot 46\,\mathrm{K}} = 15.83\,\mathrm{m^2}\) The heat transfer area of the shell-and-tube heat exchanger is \(15.83\,\mathrm{m^2}\).

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 shell-and-tube heat exchanger is used for cooling $47 \mathrm{~kg} / \mathrm{s}\( of a process stream flowing through the tubes from \)160^{\circ} \mathrm{C}\( to \)100^{\circ} \mathrm{C}$. This heat exchanger has a total of 100 identical tubes, each with an inside diameter of \(2.5 \mathrm{~cm}\) and negligible wall thickness. The average properties of the process stream are: $\rho=950 \mathrm{~kg} / \mathrm{m}^{3}, k=0.50 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, c_{p}=3.5 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}$, and \(\mu=0.002 \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\). The coolant stream is water \(c_{p}=4.18\) \(\mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K}\) at a flow rate of \(66 \mathrm{~kg} / \mathrm{s}\) and an inlet temperature of $10^{\circ} \mathrm{C}$, which yields an average shell-side heat transfer coefficient of \(4.0 \mathrm{~kW} / \mathrm{m}^{2} . \mathrm{K}\). Calculate the tube length if the heat exchanger has \((a)\) one shell pass and one tube pass and \((b)\) one shell pass and four tube passes.

Oil in an engine is being cooled by air in a crossflow heat exchanger, where both fluids are unmixed. Oil $\left(c_{p k}=2047 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( flowing with a flow rate of \)0.026 \mathrm{~kg} / \mathrm{s}\( enters the heat exchanger at \)75^{\circ} \mathrm{C}$, while air \(\left(c_{p c}=1007 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters at \(30^{\circ} \mathrm{C}\) with a flow rate of $0.21 \mathrm{~kg} / \mathrm{s}$. The overall heat transfer coefficient of the heat exchanger is \(53 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\) and the total surface area is \(1 \mathrm{~m}^{2}\). Determine \((a)\) the heat transfer effectiveness and \((b)\) the outlet temperature of the oil.

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.

Hot oil \(\left(c_{p}=2.1 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\right)\) at \(110^{\circ} \mathrm{C}\) and \(12 \mathrm{~kg} / \mathrm{s}\) is to be cooled in a heat exchanger by cold water \(\left(c_{p}=4.18\right.\) $\mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K})\( entering at \)10^{\circ} \mathrm{C}$ and at a rate of \(2 \mathrm{~kg} / \mathrm{s}\). The lowest temperature that oil can be cooled in this heat exchanger is (a) \(10^{\circ} \mathrm{C}\) (b) \(24^{\circ} \mathrm{C}\) (c) \(47^{\circ} \mathrm{C}\) (d) \(61^{\circ} \mathrm{C}\) (e) \(77^{\circ} \mathrm{C}\)

A pipe system is mainly constructed with ASTM F441 CPVC pipes. The ASME Code for Process Piping (ASME B31.3-2014, Table B-1) recommends that the maximum temperature limit for CPVC pipes be \(93.3^{\circ} \mathrm{C}\). A double-pipe heat exchanger is located upstream of the pipe system to reduce the hot water temperature before it flows into the CPVC pipes. The inner tube of the heat exchanger has a negligible wall thickness, and its length and diameter are $5 \mathrm{~m}\( and \)25 \mathrm{~mm}$, respectively. The convection heat transfer coefficients inside and outside of the heat exchanger inner tube are $3600 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( and \)4500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. The hot fluid enters the heat exchanger at \(105^{\circ} \mathrm{C}\) with a flow rate of $0.75 \mathrm{~kg} / \mathrm{s}$. In the cold fluid stream, water enters the heat exchanger at \(10^{\circ} \mathrm{C}\) and exits at \(80^{\circ} \mathrm{C}\). Determine whether this double-pipe heat exchanger should employ the parallel flow or the counterflow configuration to ensure that the hot water exiting the heat exchanger is \(93.3^{\circ} \mathrm{C}\) or lower.

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