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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 $180^{\circ} \mathrm{C}$.

Short Answer

Expert verified
The required insulation layer thickness is approximately 9.66 cm.

Step by step solution

01

Find Heat Loss from Pipe Without Insulation

Given the information about the water vapor flowing through the pipe, we can find the heat loss from the pipe. We know that the mass flow rate of the water vapor is 0.03 kg/s. The temperature difference across the pipe (hot to cold) is: \(\Delta T = T_{in} - T_{out} = 325°C - 290°C = 35°C\) Now, the heat loss from the pipe can be calculated using the formula: \(q = m \cdot c \cdot \Delta T\) Here, \(q\) represents the heat loss from the pipe in watts, \(m\) is the mass flow rate in kg/s, \(c\) is the specific heat capacity of water vapor (we can approximate it to be \(c \approx 2 J / g \cdot K\)), and \(\Delta T\) is the temperature difference in \(K\). Plugging in the given values, we get: \(q = 0.03 kg/s \cdot 2 \frac{J}{g \cdot K} \cdot 35 K = 2.1 \frac{J}{s}\)
02

Apply Steady-state Heat Conduction Equation

Now that we have the heat loss for the pipe without insulation, we can apply the steady-state heat conduction equation to find the required insulation layer thickness. The heat conduction equation can be written as: \(q = \frac{kA \Delta T}{d}\) Here, \(q\) represents the heat loss, \(k\) is the thermal conductivity of the insulation material, \(A\) is the surface area of the pipe, \(\Delta T\) is the temperature difference across the pipe, and \(d\) is the insulation layer thickness. We are given the thermal conductivity of the insulation (\(k_{ins} \approx 0.95 W/m\cdot K\)), and we also have the maximum allowed outer surface temperature of 180°C. We can use these values to find the required insulation layer thickness. First, calculate the temperature difference across the insulation layer: \(\Delta T_{ins} = T_{pipe} - T_{max} = 290°C - 180°C = 110°C\) Now, calculate the surface area of the pipe: \(A = \pi \times D_{o,pipe} \times L = \pi \times 0.06 m \times 10 m = 1.884 \, \mathrm{m}^2\) We can rearrange the heat conduction equation to solve for \(d\): \(d = \frac{k_{ins} A \Delta T_{ins}}{q}\) Plug in the values and calculate \(d\): \(d = \frac{0.95 \frac{W}{m \cdot K} \cdot 1.884 \, \mathrm{m}^2 \cdot 110 K}{2.1 \frac{J}{s}} = 0.0966 \, m\)
03

Finalize the Answer

Now we have obtained the required insulation layer thickness to be 0.0966 m. To express the answer more clearly, we can convert it to centimeters: \(d = 0.0966 m \times \frac{100 cm}{1 m} = 9.66 cm\) So, the required insulation layer thickness is approximately 9.66 cm to keep the outer surface temperature below 180°C and prevent any fire hazard.

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Most popular questions from this chapter

Air (1 atm) enters a 5-mm-diameter circular tube at an average velocity of $5 \mathrm{~m} / \mathrm{s}$. The tube wall is maintained at a constant surface temperature. Determine the convection heat transfer coefficient for \((a)\) a \(10-\mathrm{cm}\)-long tube and \((b)\) a \(50-\mathrm{cm}-\) long tube. Evaluate the air properties at \(50^{\circ} \mathrm{C}\).

Consider the velocity and temperature profiles for a fluid flow in a tube with a diameter of \(50 \mathrm{~mm}\) that can be expressed as $$ \begin{aligned} &u(r)=0.05\left[1-(r / R)^{2}\right] \\ &T(r)=400+80(r / R)^{2}-30(r / R)^{3} \end{aligned} $$ with units in \(\mathrm{m} / \mathrm{s}\) and \(\mathrm{K}\), respectively. Determine the average velocity and the mean (average) temperature from the given velocity and temperature profiles.

Liquid water flows in a circular tube at a mass flow rate of $7 \mathrm{~g} / \mathrm{s}\(. The water enters the tube at \)5^{\circ} \mathrm{C}$, and the average convection heat transfer coefficient for the internal flow is $20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\(. The tube is \)3 \mathrm{~m}$ long and has an inner diameter of \(25 \mathrm{~mm}\). The tube surface is maintained at a constant temperature. The inner surface of the tube is lined with polyvinylidene chloride (PVDC) lining. According to the ASME Code for Process Piping (ASME B31.3-2014, Table A.323.4.3), the recommended maximum temperature for PVDC lining is \(79^{\circ} \mathrm{C}\). If the water exits the tube at \(15^{\circ} \mathrm{C}\), determine the heat rate transferred to the water. Would the inner surface temperature of the tube exceed the recommended maximum temperature for PVDC lining?

Consider laminar forced convection in a circular tube. Will the heat flux be higher near the inlet of the tube or near the exit? Why?

A concentric annulus tube has inner and outer diameters of 1 in and 4 in, respectively. Liquid water flows at a mass flow rate of $396 \mathrm{lbm} / \mathrm{h}$ through the annulus with the inlet and outlet mean temperatures of \(68^{\circ} \mathrm{F}\) and \(172^{\circ} \mathrm{F}\), respectively. The inner tube wall is maintained with a constant surface temperature of $250^{\circ} \mathrm{F}$, while the outer tube surface is insulated. Determine the length of the concentric annulus tube. Assume flow is fully developed.

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