A 0.6-m-diameter, 1.9-m-long cylindrical tank containing liquefied natural gas (LNG) at \(-160^{\circ} \mathrm{C}\) is placed at the center of a 1.9-m-long \(1.4-\mathrm{m} \times 1.4-\mathrm{m}\) square solid bar made of an insulating material with \(k=0.0002 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). If the outer surface temperature of the bar is \(12^{\circ} \mathrm{C}\), determine the rate of heat transfer to the tank. Also, determine the LNG temperature after one month. Take the density and the specific heat of LNG to be \(425 \mathrm{~kg} / \mathrm{m}^{3}\) and \(3.475 \mathrm{~kJ} / \mathrm{kg} \cdot{ }^{\circ} \mathrm{C}\), respectively.

Short Answer

Expert verified
Answer: The rate of heat transfer to the tank is 74.88 W, and the temperature of the LNG after one month is -135.66°C.

Step by step solution

01

Find the rate of heat transfer through the insulating material

The formula for the rate of heat transfer (Q) through a cylinder is given by $$Q = \frac {2\pi kL(T_1-T_2)}{\ln \left(\frac{r_2}{r_1} \right)}$$ where L is the length of the cylinder, k is the thermal conductivity of the material, \(T_1\) and \(T_2\) are the inner and outer surface temperatures, and \(r_1\) and \(r_2\) are the inner and outer radii. Given the problem's parameters: Diameter of the cylinder: \(0.6 \,\text{m}\) Length of the cylinder: \(1.9 \,\text{m}\) Thermal conductivity: \(0.0002 \,\frac{\text{W}}{\text{m}\cdot{^{\circ}\text{C}}}\) Inner surface temperature: \(-160^{\circ} \mathrm{C}\) Outer surface temperature: \(12^{\circ} \mathrm{C}\) First, calculate the inner and outer radii. \(r_1 = \frac{0.6\,\text{m}}{2} = 0.3\,\text{m}\) (radius of LNG tank) The square solid bar is \(1.4\,\text{m}\) wide, so the insulating material thickness is \(\frac{1.4\,\text{m}-0.6\,\text{m}}{2} = 0.4\,\text{m}\). Then, \(r_2 = r_1 + 0.4\,\text{m} = 0.7\,\text{m}\). Now, substitute the given values into the formula and find Q. $$Q = \frac {2\pi (0.0002)(1.9)((12)-(-160))}{\ln \left(\frac{0.7}{0.3} \right)} = 74.88\,\text{W}$$
02

Calculating the energy gain by the LNG

Find the energy gain by LNG after one month, and determine the temperature rise. The energy gain (E) can be calculated using the formula: $$E = Qt$$ where t is the time in seconds. One month has approximately \(30 \times 24 \times 60 \times 60\) seconds. Calculate the energy gain by LNG after one month: $$E = (74.88\,\text{W}) \times (30 \times 24 \times 60 \times 60\,\text{s}) = 194348160 \, \text{J}$$
03

Calculating the temperature rise of the LNG

To find the temperature rise, we will use the formula: $$\Delta T = \frac{E}{mc}$$ where m is the mass of the LNG, and c is the specific heat of the LNG. Given the density (\(\rho\)) and specific heat (c) of the LNG are \(425\,\frac{\text{kg}}{\text{m}^3}\) and \(3475\,\frac{\text{J}}{\text{kg}\cdot{^{\circ}\text{C}}}\), respectively. First, find the volume and mass of the LNG: $$V_\text{LNG}= \pi r_\text{LNG}^2L_\text{LNG}=\pi(0.3\,\text{m})^2(1.9\,\text{m})=0.54\,\text{m}^3$$ $$m = \rho V_\text{LNG} = (425\,\frac{\text{kg}}{\text{m}^3})(0.54\,\text{m}^3) = 229.5\,\text{kg}$$ Now, find the temperature rise of the LNG: $$\Delta T = \frac{194348160\,\text{J}}{(229.5\,\text{kg})(3475\,\frac{\text{J}}{\text{kg}\cdot{^{\circ}\text{C}}})} = 24.34^{\circ}\text{C}$$
04

Calculating the final temperature of the LNG

Now that we have the temperature rise, we can calculate the final temperature of the LNG by adding the initial temperature. $$T_\text{final} = T_\text{initial} + \Delta T$$ $$T_\text{final} = -160^{\circ} \mathrm{C} + 24.34^{\circ}\text{C} = -135.66^{\circ}\text{C}$$ The rate of heat transfer to the tank is \(74.88 \,\text{W}\), and the temperature of the LNG after one month is \(-135.66^{\circ} \mathrm{C}\).

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Most popular questions from this chapter

Cold conditioned air at \(12^{\circ} \mathrm{C}\) is flowing inside a \(1.5\)-cm- thick square aluminum \((k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) duct of inner cross section \(22 \mathrm{~cm} \times 22 \mathrm{~cm}\) at a mass flow rate of \(0.8 \mathrm{~kg} / \mathrm{s}\). The duct is exposed to air at \(33^{\circ} \mathrm{C}\) with a combined convection-radiation heat transfer coefficient of \(13 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The convection heat transfer coefficient at the inner surface is \(75 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). If the air temperature in the duct should not increase by more than \(1^{\circ} \mathrm{C}\) determine the maximum length of the duct.

Two flow passages with different cross-sectional shapes, one circular another square, are each centered in a square solid bar of the same dimension and thermal conductivity. Both configurations have the same length, \(T_{1}\), and \(T_{2}\). Determine which configuration has the higher rate of heat transfer through the square solid bar for \((a) a=1.2 b\) and \((b) a=2 b\).

Steam at \(320^{\circ} \mathrm{C}\) flows in a stainless steel pipe \((k=\) \(15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) ) whose inner and outer diameters are \(5 \mathrm{~cm}\) and \(5.5 \mathrm{~cm}\), respectively. The pipe is covered with \(3-\mathrm{cm}\)-thick glass wool insulation \((k=0.038 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). Heat is lost to the surroundings at \(5^{\circ} \mathrm{C}\) by natural convection and radiation, with a combined natural convection and radiation heat transfer coefficient of \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Taking the heat transfer coefficient inside the pipe to be \(80 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the rate of heat loss from the steam per unit length of the pipe. Also determine the temperature drops across the pipe shell and the insulation.

A pipe is insulated to reduce the heat loss from it. However, measurements indicate that the rate of heat loss has increased instead of decreasing. Can the measurements be right?

Consider a 25-m-long thick-walled concrete duct \((k=\) \(0.75 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) of square cross section. The outer dimensions of the duct are \(20 \mathrm{~cm} \times 20 \mathrm{~cm}\), and the thickness of the duct wall is \(2 \mathrm{~cm}\). If the inner and outer surfaces of the duct are at \(100^{\circ} \mathrm{C}\) and \(30^{\circ} \mathrm{C}\), respectively, determine the rate of heat transfer through the walls of the duct. Answer: \(47.1 \mathrm{~kW}\)

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