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Consider a 25-mm-diameter and 15-m-long smooth tube that is maintained at a constant surface temperature. Fluids enter the tube at \(50^{\circ} \mathrm{C}\) with a mass flow rate of \(0.01 \mathrm{~kg} / \mathrm{s}\). Determine the tube surface temperatures necessary to heat water, engine oil, and liquid mercury to the desired outlet temperature of \(150^{\circ} \mathrm{C}\).

Short Answer

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Question: Determine the tube surface temperatures necessary to heat water, engine oil, and liquid mercury to the desired outlet temperature of 150°C. Answer: To determine the tube surface temperatures necessary to heat water, engine oil, and liquid mercury to the desired outlet temperature of 150°C, follow these steps: 1. Calculate the heat transfer rates using the energy balance equation for each fluid. 2. Calculate the heat transfer rate using the heat transfer formula (conduction and convection) for each fluid. 3. Determine the tube surface temperatures for each fluid by substituting the calculated values into the rearranged heat transfer equation.

Step by step solution

01

Find heat transfer rates using energy balance for each fluid.

First, find the specific heat capacities of water, engine oil, and liquid mercury. The energy balance equation is: \(Q = m\cdot c_p (\Delta T)\) where \(Q\) is the heat transfer rate, \(m\) is the mass flow rate, \(c_p\) is the specific heat capacity, and \(\Delta T\) is the change in temperature. The mass flow rate is given as \(m = 0.01 \mathrm{~kg/s}\). The change in temperature for all fluids is the same as the difference between the desired outlet temperature and the inlet temperature: \(\Delta T = T_{outlet} - T_{inlet} = 150-50 = 100^{\circ}C\) Find the specific heat capacities of water (\(c_{p,w}\)), engine oil (\(c_{p,eo}\)), and liquid mercury (\(c_{p,lm}\)). Then, calculate the heat transfer rates for each fluid using the energy balance equation.
02

Calculate the heat transfer rate using the heat transfer formula for each fluid.

Next, we'll use the heat transfer equation for conduction and convection in a tube: \(Q = hA_s(T_s - T_m)\) where \(Q\) is the heat transfer rate, \(h\) is the heat transfer coefficient, \(A_s\) is the surface area of the tube, \(T_s\) is the tube surface temperature, and \(T_m\) is the mean temperature between the inlet and outlet temperatures. To find the surface area of the tube, use the formula: \(A_s = 2 \pi r L\) where \(r\) is the radius of the tube and \(L\) is its length. Calculate the mean temperature for each fluid: \(T_m = \frac{T_{inlet}+T_{outlet}}{2}\) For each fluid, look up the heat transfer coefficient (\(h\)) in a reference. Then, rearrange the heat transfer equation to solve for the tube surface temperature (\(T_s\)) for each fluid: \(T_s = T_m + \frac{Q}{hA_s}\)
03

Determine the tube surface temperatures for each fluid.

Using the heat transfer rates found in Step 1, the surface area calculated in Step 2, and the heat transfer coefficients (from reference) for each fluid, compute the tube surface temperature (\(T_s\)) for water, engine oil, and liquid mercury. In conclusion, follow these steps to determine the tube surface temperatures necessary to heat water, engine oil, and liquid mercury to the desired outlet temperature of \(150^{\circ}C\): 1. Calculate the heat transfer rates using the energy balance equation for each fluid. 2. Calculate the heat transfer rate using the heat transfer formula (conduction and convection) for each fluid. 3. Determine the tube surface temperatures for each fluid by substituting the calculated values into the rearranged heat transfer equation.

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Most popular questions from this chapter

A tube with a bell-mouth inlet configuration is subjected to uniform wall heat flux of \(3 \mathrm{~kW} / \mathrm{m}^{2}\). The tube has an inside diameter of \(0.0158 \mathrm{~m}(0.622 \mathrm{in})\) and a flow rate of $1.43 \times 10^{-4} \mathrm{~m}^{3} / \mathrm{s}(2.27 \mathrm{gpm})$. The liquid flowing inside the tube is an ethylene glycol-distilled water mixture with a mass fraction of \(2.27\). Determine the fully developed friction coefficient at a location along the tube where the Grashof number is Gr \(=16,600\). The physical properties of the ethylene glycol-distilled water mixture at the location of interest are Pr $=14.85, \nu=1.93 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\(, and \)\mu_{v} / \mu_{s}=1.07$.

Engine oil flows in a 15 -cm-diameter horizontal tube with a velocity of $1.3 \mathrm{~m} / \mathrm{s}\(, experiencing a pressure drop of \)12 \mathrm{kPa}$. The pumping power requirement to overcome this pressure drop is (a) \(190 \mathrm{~W}\) (b) \(276 \mathrm{~W}\) (c) \(407 \mathrm{~W}\) (d) \(655 \mathrm{~W}\) (e) \(900 \mathrm{~W}\)

An ethylene glycol-distilled water mixture with a mass fraction of \(0.72\) and a flow rate of \(2.05 \times 10^{-4} \mathrm{~m}^{3} / \mathrm{s}\) flows inside a tube with an inside diameter of \(0.0158 \mathrm{~m}\) and a uniform wall heat flux boundary condition. For this flow, determine the Nusselt number at the location \(x / D=10\) for the inlet tube configuration of \((a)\) bell-mouth and \((b)\) re-entrant. Compare the results for parts \((a)\) and \((b)\). Assume the Grashof number is \(\mathrm{Gr}=60,000\). The physical properties of an ethylene glycoldistilled water mixture are $\operatorname{Pr}=33.46, \nu=3.45 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\(, and \)\mu_{b} / \mu_{s}=2.0$.

The components of an electronic system dissipating \(220 \mathrm{~W}\) are located in a 1 -m-long horizontal duct whose cross section is $16 \mathrm{~cm} \times 16 \mathrm{~cm}$. The components in the duct are cooled by forced air, which enters at \(27^{\circ} \mathrm{C}\) at a rate of $0.65 \mathrm{~m}^{3} / \mathrm{min}$. Assuming 85 percent of the heat generated inside is transferred to air flowing through the duct and the remaining 15 percent is lost through the outer surfaces of the duct, determine \((a)\) the exit temperature of air and \((b)\) the highest component surface temperature in the duct. As a first approximation, assume fully developed turbulent flow in the channel. Evaluate the properties of air at a bulk mean temperature of \(35^{\circ} \mathrm{C}\). Is this a good assumption?

metal pipe $\left(k_{\text {pipe }}=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, D_{\text {, pipe }}=\right.\( \)5 \mathrm{~cm}, D_{o \text {, pipe }}=6 \mathrm{~cm}\(, and \)\left.L=10 \mathrm{~m}\right)$ situated in an engine room is used for transporting hot saturated water vapor at a flow rate of \(0.03 \mathrm{~kg} / \mathrm{s}\). The water vapor enters and exits the pipe at \(325^{\circ} \mathrm{C}\) and \(290^{\circ} \mathrm{C}\), respectively. Oil leakage can occur in the engine room, and when leaked oil comes in contact with hot spots above the oil's autoignition temperature, it can ignite spontaneously. To prevent any fire hazard caused by oil leakage on the hot surface of the pipe, determine the required insulation $\left(k_{\text {ins }}=0.95 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.$ ) layer thickness over the pipe for keeping the outer surface temperature below $180^{\circ} \mathrm{C}$.

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