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Liquid water flows in a thin-walled circular tube, where the pumping power required to overcome the turbulent flow pressure loss in the tube is $100 \mathrm{~W}\(. The water enters the tube at \)10^{\circ} \mathrm{C}$, where it is heated at a rate of \(3.6 \mathrm{~kW}\). The average convection heat transfer coefficient for the internal flow is $120 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. The tube is \)3 \mathrm{~m}$ long and has an inner diameter of \(12.5 \mathrm{~mm}\). The tube surface is maintained at a constant temperature. At the tube exit, an ethylene propylene diene (EPDM) rubber o-ring is attached to the tube's outer surface. The maximum temperature permitted for the o-ring is \(150^{\circ} \mathrm{C}\) (ASME Boiler and Pressure Vessel Code, BPVC. IV-2015, HG-360). Is the EPDM o-ring suitable for this operation? Evaluate the fluid properties at \(10^{\circ} \mathrm{C}\). Is this an appropriate temperature at which to evaluate the fluid properties?

Short Answer

Expert verified
Answer: Yes, the EPDM o-ring is suitable for this operation since the calculated temperature at the tube exit (138.72°C) is less than the maximum allowable temperature for the o-ring (150°C).

Step by step solution

01

Calculate the thermal energy supplied to the water

The rate at which heat is supplied to the water is given as 3.6 kW. Convert this to watts: Thermal energy supplied = 3.6 kW × 1000 = 3600 W
02

Calculate the water flow rate

The power required to overcome the turbulent flow pressure loss is given as 100 W. The water flow rate can be calculated using the relation: \(\dot{m} = \frac{P}{C_p(T_f - T_i)}\) where \(\dot{m}\) is the mass flow rate, \(P\) is the pumping power, \(C_p\) is the specific heat of water (approximately 4186 J/kg·K at 10°C), \(T_f\) is the final temperature of the water, and \(T_i\) is the initial temperature of the water (10°C). We will solve for the mass flow rate: \(\dot{m} = \frac{100}{4186(T_f - 10)}\)
03

Determine the heat transfer rate from convection

The heat transfer rate due to convection can be calculated as: \(Q = hA_s\Delta T\) where \(Q\) is the heat transfer rate, \(h\) is the average convection heat transfer coefficient (given as 120 W/m²·K), \(A_s\) is the surface area of the tube, and \(\Delta T\) is the temperature difference between the tube surface and the water. The surface area of the tube can be calculated using the formula: \(A_s = 2\pi rL\) where \(r\) is the radius of the tube, and \(L\) is its length. Convert the diameter to meters and find the radius: \(r = \frac{12.5}{2}\times10^{-3} \mathrm{m}\) The length of the tube is given as 3 m, so the surface area of the tube is: \(A_s = 2\pi\cdot (6.25\times10^{-3}\mathrm{m})\cdot 3 \mathrm{m}\approx 0.235 \mathrm{m}^2\) Now we can calculate the heat transfer rate: \(Q = 120\ \mathrm{W/m}^2\cdot \mathrm{K\:} \times0.235 \: \mathrm{m}^2\times\Delta T\)
04

Calculate the temperature of the water at the tube exit

We know that the thermal energy supplied to the water is equal to the heat transfer rate: Thermal energy supplied = Heat transfer rate \(3600 \:/\: \mathrm{W} = 120\ \mathrm{W/m}^2\cdot \mathrm{K\:} \times0.235\: \mathrm{m}^2\times\Delta T\) Solving for \(\Delta T\) gives \(\Delta T = \frac{3600}{120\times0.235}= 128.72 \:/\: \mathrm{K}\) The temperature of the water at the tube exit is: \(T_f =T_i +\Delta T =10+128.72 = 138.72 \:/\: ^\circ \mathrm{C}\)
05

Compare the temperature at the tube exit to the maximum allowable temperature for the o-ring

The maximum allowable temperature for the EPDM o-ring is given as 150°C. Since the calculated temperature at the tube exit (138.72°C) is less than the maximum allowable temperature for the o-ring (150°C), the EPDM o-ring is suitable for this operation. As for evaluating fluid properties at 10°C, this temperature is suitable since it is the initial temperature of the water and the fluid properties are not expected to vary significantly within the range of temperatures experienced in this operation.

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Most popular questions from this chapter

The velocity profile in fully developed laminar flow in a circular pipe of inner radius \(R=10 \mathrm{~cm}\), in \(\mathrm{m} / \mathrm{s}\), is given by \(u(r)=4\left(1-r^{2} / R^{2}\right)\). Determine the mean and maximum velocities in the pipe, and determine the volume flow rate.

In fully developed laminar flow inside a circular pipe, the velocities at \(r=0.5 R\) (midway between the wall surface and the centerline) are measured to be 3,6 , and \(9 \mathrm{~m} / \mathrm{s}\). (a) Determine the maximum velocity for each of the measured midway velocities. (b) By varying \(r / R\) for $-1 \leq r / R \leq 1$, plot the velocity profile for each of the measured midway velocities with \(r / R\) as the \(y\)-axis and \(V(r / R)\) as the \(x\)-axis.

In a food processing plant, hot liquid water is being transported in a pipe \((k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), $D_{i}=2.5 \mathrm{~cm}, D_{o}=3 \mathrm{~cm}\(, and \)L=10 \mathrm{~m}$.) The hot water flowing with a mass flow rate of \(0.15 \mathrm{~kg} / \mathrm{s}\) enters the pipe at \(100^{\circ} \mathrm{C}\) and exits at \(60^{\circ} \mathrm{C}\). The plant supervisor thinks that since the hot water exits the pipe at $60^{\circ} \mathrm{C}$, the pipe's outer surface temperature should be safe from thermal burn hazards. In order to prevent thermal burn upon accidental contact with skin tissue for individuals working in the vicinity of the pipe, the pipe's outer surface temperature should be kept below \(45^{\circ} \mathrm{C}\). Determine whether or not there is a risk of thermal burn on the pipe's outer surface. Assume the pipe outer surface temperature remains constant.

\(100 \mathrm{~kg} / \mathrm{s}\) of crude oil is heated from $20^{\circ} \mathrm{C}\( to \)40^{\circ} \mathrm{C}$ through the tube side of a multitube heat exchanger. The crude oil flow is divided evenly among all 100 tubes in the tube bundle. The ID of each tube is \(10 \mathrm{~mm}\), and the inside tube-wall temperature is maintained at \(100^{\circ} \mathrm{C}\). Average properties of the crude oil are $\rho=950 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=1.9 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}, k=\( \)0.25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \mu=12 \mathrm{mPa} \cdot \mathrm{s}$, and \(\mu_{w}=4 \mathrm{mPa} \cdot \mathrm{s}\). Estimate the rate of heat transfer and the tube length.

What is the physical significance of the number of transfer units \(\mathrm{NTU}=h A_{s} / \dot{m} c_{p}\) ? What do small and large NTU values tell us about a heat transfer system?

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