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Consider the flow of oil at \(10^{\circ} \mathrm{C}\) in a \(40-\mathrm{cm}\)-diameter pipeline at an average velocity of $0.5 \mathrm{~m} / \mathrm{s}\(. A \)1500-\mathrm{m}$-long section of the pipeline passes through icy waters of a lake at \(0^{\circ} \mathrm{C}\). Measurements indicate that the surface temperature of the pipe is very nearly \(0^{\circ} \mathrm{C}\). Disregarding the thermal resistance of the pipe material, determine \((a)\) the temperature of the oil when the pipe leaves the lake, \((b)\) the rate of heat transfer from the oil, and \((c)\) the pumping power required to overcome the pressure losses and to maintain the flow of oil in the pipe.

Short Answer

Expert verified
Question: Determine (a) the temperature of the oil when the pipe leaves the lake, (b) the rate of heat transfer from the oil, and (c) the pumping power required to overcome the pressure losses and to maintain the flow of oil in the pipe.

Step by step solution

01

Calculate the temperature of the oil after leaving the lake

For this step, we will use the logarithmic mean temperature difference (LMTD) method to calculate the temperature difference between the inlet and outlet temperatures. The LMTD formula is: \[ \Delta T_\mathrm{lm} = \frac{\Delta T_\mathrm{in} - \Delta T_\mathrm{out}}{\ln(\Delta T_\mathrm{in} / \Delta T_\mathrm{out})} \] where - \(\Delta T_\mathrm{in}\) is the initial temperature difference between the oil and the lake (10°C - 0°C = 10°C), - \(\Delta T_\mathrm{out}\) is the final temperature difference between the oil and the lake (unknown), - \(\Delta T_\mathrm{lm}\) is the logarithmic mean temperature difference. We also have a heat transfer equation: \[ q = U \cdot A \cdot \Delta T_\mathrm{lm} \] where - \(q\) is the rate of heat transfer, - \(U\) is the overall heat transfer coefficient, - \(A\) is the surface area of the pipe. We will use these two equations to determine the temperature of the oil after leaving the lake.
02

Calculate the rate of heat transfer from the oil

We can calculate the rate of heat transfer from the oil using the following equation: \[ q = m \cdot C_p \cdot \Delta T \] where - \(m\) is the mass flow rate of the oil, - \(C_p\) is the specific heat capacity of the oil, - \(\Delta T\) is the temperature change. To calculate the mass flow rate of the oil: \[ m = \rho \cdot A_\mathrm{c} \cdot v \] where - \(\rho\) is the density of the oil, - \(A_\mathrm{c}\) is the cross-sectional area of the pipeline, - \(v\) is the average velocity of the oil. We now have all the equations needed to calculate the rate of heat transfer from the oil.
03

Calculate the pumping power required

To calculate the pumping power required to overcome the pressure losses and maintain the flow of oil in the pipe, we can use the following equation: \[ W_\mathrm{p} = \Delta P \cdot \frac{m}{\rho} = m \cdot g \cdot h_\mathrm{loss} = m \cdot (h_\mathrm{p} - h_\mathrm{loss}) \] where - \(W_\mathrm{p}\) is the pumping power, - \(\Delta P\) is the pressure loss, - \(g\) is the acceleration due to gravity, - \(h_\mathrm{loss}\) is the head loss due to friction, - \(h_\mathrm{p}\) is the pump head. We can calculate the head loss using the Darcy-Weisbach equation: \[ h_\mathrm{loss} = f \cdot \frac{L}{D} \cdot \frac{v^2}{2g} \] where - \(f\) is the friction factor, - \(L\) is the length of the pipe, - \(D\) is the diameter of the pipe. Now we have all the equations needed to calculate the pumping power required. Using the information provided and solving these equations, you will be able to determine \((a)\) the temperature of the oil when the pipe leaves the lake, \((b)\) the rate of heat transfer from the oil, and \((c)\) the pumping power required to overcome the pressure losses and to maintain the flow of oil in the pipe.

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Most popular questions from this chapter

Water at $10^{\circ} \mathrm{C}\left(\rho=999.7 \mathrm{~kg} / \mathrm{m}^{3}\right.\( and \)\mu=1.307 \times\( \)10^{-3} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\( ) is flowing in a \)0.20-\mathrm{cm}$-diameter, 15 -m-long pipe steadily at an average velocity of $1.2 \mathrm{~m} / \mathrm{s}\(. Determine \)(a)\( the pressure drop and \)(b)$ the pumping power requirement to overcome this pressure drop. Assume flow is fully developed. Is this a good assumption? Answers: (a) \(188 \mathrm{kPa}\), (b) $0.71 \mathrm{~W}$

Consider fully developed laminar flow in a circular pipe. If the viscosity of the fluid is reduced by half by heating while the flow rate is held constant, how will the pressure drop change?

What does the logarithmic mean temperature difference represent for flow in a tube whose surface temperature is constant? Why do we use the logarithmic mean temperature instead of the arithmetic mean temperature?

Consider a fluid with mean inlet temperature \(T_{i}\) flowing through a tube of diameter \(D\) and length \(L\), at a mass flow rate \(\dot{m}\). The tube is subjected to a surface heat flux that can be expressed as $\dot{q}_{s}(x)=a+b \sin (x \pi / L)\(, where \)a\( and \)b$ are constants. Determine an expression for the mean temperature of the fluid as a function of the \(x\)-coordinate.

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