The boiling temperature of nitrogen at atmospheric pressure at sea level ( 1 atm pressure) is \(-196^{\circ} \mathrm{C}\). Therefore, nitrogen is commonly used in low-temperature scientific studies since the temperature of liquid nitrogen in a tank open to the atmosphere will remain constant at \(-196^{\circ} \mathrm{C}\) until it is depleted. Any heat transfer to the tank will result in the evaporation of some liquid nitrogen, which has a heat of vaporization of \(198 \mathrm{~kJ} / \mathrm{kg}\) and a density of \(810 \mathrm{~kg} / \mathrm{m}^{3}\) at 1 atm. Consider a 3-m-diameter spherical tank that is initially filled with liquid nitrogen at 1 atm and \(-196^{\circ} \mathrm{C}\). The tank is exposed to ambient air at \(15^{\circ} \mathrm{C}\), with a combined convection and radiation heat transfer coefficient of \(35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The temperature of the thin-shelled spherical tank is observed to be almost the same as the temperature of the nitrogen inside. Determine the rate of evaporation of the liquid nitrogen in the tank as a result of the heat transfer from the ambient air if the tank is \((a)\) not insulated, \((b)\) insulated with 5 -cm-thick fiberglass insulation \((k=0.035 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\), and (c) insulated with 2 -cm-thick superinsulation which has an effective thermal conductivity of \(0.00005 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

Short Answer

Expert verified
Answer: The rates of evaporation of liquid nitrogen in the spherical tank are (a) 1.051 kg/s (non-insulated), (b) 0.021 kg/s (fiberglass insulation), and (c) 0.00037 kg/s (superinsulation).

Step by step solution

01

(Step 1: Calculate the heat transfer rate for each case)

First, let's calculate the heat transfer rate for each case. For that, we need to know the temperature difference between the liquid nitrogen and the ambient air, and the surface area of the tank. The heat transfer rate formula for each case will be different depending on the insulation. For the non-insulated case (a), we will apply the combined convection and radiation heat transfer coefficient. For the insulated cases (b) and (c), we'll need to apply the formula for heat conduction through the insulation.
02

(Step 2: Find the temperature difference and tank's surface area)

Determine the temperature difference between the liquid nitrogen (\(T_N= -196°C\)) and the ambient air (\(T_A = 15°C\)), which is the driving force for heat transfer: \(\Delta T = T_A - T_N = 15 - (-196) = 211 K\) Now calculate the surface area of the 3-m diameter spherical tank: \(A = 4 \pi r^2\) Where \(r\) is the radius of the tank, \(r = \frac{D}{2} = \frac{3}{2} = 1.5 \thinspace m\). Calculate the surface area: \(A = 4 \pi (1.5)^2 = 28.27 m^2\)
03

(Step 3: Calculate the heat transfer rate for Case A)

For the non-insulated case (a), the heat transfer rate (\(\dot{Q}\)) will be given by: \(\dot{Q}_A = h \cdot A \cdot \Delta T\) Where \(h = 35 \frac{W}{m^{2} \cdot K}\). Calculate the heat transfer rate for case (a): \(\dot{Q}_A = 35 \cdot 28.27 \cdot 211 = 208012.95 \thinspace W\)
04

(Step 4: Calculate the heat transfer rate for Case B)

For the fiberglass insulated case (b), the heat transfer rate will be given by: \(\dot{Q}_B = \frac{k \cdot A \cdot \Delta T}{L}\) Where \(k = 0.035 \frac{W}{m \cdot K}\) and \(L = 0.05 m\). Calculate the heat transfer rate for case (b): \(\dot{Q}_B = \frac{0.035 \cdot 28.27 \cdot 211}{0.05} = 4205.17 \thinspace W\)
05

(Step 5: Calculate the heat transfer rate for Case C)

For the superinsulated case (c), the heat transfer rate will be given by: \(\dot{Q}_C = \frac{k \cdot A \cdot \Delta T}{L}\) Where \(k = 0.00005 \frac{W}{m \cdot K}\) and \(L = 0.02 m\). Calculate the heat transfer rate for case (c): \(\dot{Q}_C = \frac{0.00005 \cdot 28.27 \cdot 211}{0.02} = 73.85 \thinspace W\)
06

(Step 6: Determine the rate of evaporation for each case)

Finally, determine the rate of evaporation for each case by dividing the heat transfer rate by the heat of vaporization of liquid nitrogen: \(\dot{m} = \frac{\dot{Q}}{h_v}\) Where \(h_v = 198 \frac{kJ}{kg} = 198000 \frac{W \cdot s}{kg}\). Calculate the mass evaporation rate for case (a), (b), and (c): \(\dot{m}_A = \frac{208012.95}{198000} = 1.051 \thinspace kg/s\) \(\dot{m}_B = \frac{4205.17}{198000} = 0.021 \thinspace kg/s\) \(\dot{m}_C = \frac{73.85}{198000} = 0.00037 \thinspace kg/s\) The rates of evaporation of liquid nitrogen in the spherical tank for each case are \(\dot{m}_A = 1.051 \thinspace kg/s\) (non-insulated), \(\dot{m}_B = 0.021 \thinspace kg/s\) (fiberglass insulation), and \(\dot{m}_C = 0.00037 \thinspace kg/s\) (superinsulation).

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Hot water at an average temperature of \(53^{\circ} \mathrm{C}\) and an average velocity of \(0.4 \mathrm{~m} / \mathrm{s}\) is flowing through a \(5-\mathrm{m}\) section of a thin-walled hot-water pipe that has an outer diameter of \(2.5 \mathrm{~cm}\). The pipe passes through the center of a \(14-\mathrm{cm}\)-thick wall filled with fiberglass insulation \((k=0.035 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). If the surfaces of the wall are at \(18^{\circ} \mathrm{C}\), determine \((a)\) the rate of heat transfer from the pipe to the air in the rooms and \((b)\) the temperature drop of the hot water as it flows through this 5 -m-long section of the wall. Answers: \(19.6 \mathrm{~W}, 0.024^{\circ} \mathrm{C}\)

A turbine blade made of a metal alloy \((k=\) \(17 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) has a length of \(5.3 \mathrm{~cm}\), a perimeter of \(11 \mathrm{~cm}\), and a cross-sectional area of \(5.13 \mathrm{~cm}^{2}\). The turbine blade is exposed to hot gas from the combustion chamber at \(973^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(538 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The base of the turbine blade maintains a constant temperature of \(450^{\circ} \mathrm{C}\) and the tip is adiabatic. Determine the heat transfer rate to the turbine blade and temperature at the tip.

A \(5-\mathrm{mm}\)-diameter spherical ball at \(50^{\circ} \mathrm{C}\) is covered by a \(1-\mathrm{mm}\)-thick plastic insulation \((k=0.13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). The ball is exposed to a medium at \(15^{\circ} \mathrm{C}\), with a combined convection and radiation heat transfer coefficient of \(20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine if the plastic insulation on the ball will help or hurt heat transfer from the ball.

A 1-m-inner-diameter liquid-oxygen storage tank at a hospital keeps the liquid oxygen at \(90 \mathrm{~K}\). The tank consists of a \(0.5-\mathrm{cm}\)-thick aluminum ( \(k=170 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) shell whose exterior is covered with a 10 -cm-thick layer of insulation \((k=\) \(0.02 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). The insulation is exposed to the ambient air at \(20^{\circ} \mathrm{C}\) and the heat transfer coefficient on the exterior side of the insulation is \(5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The temperature of the exterior surface of the insulation is (a) \(13^{\circ} \mathrm{C}\) (b) \(9^{\circ} \mathrm{C}\) (c) \(2^{\circ} \mathrm{C}\) (d) \(-3^{\circ} \mathrm{C}\) (e) \(-12^{\circ} \mathrm{C}\)

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: \(47.1 \mathrm{~kW}\)

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free