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An ideal gas flows within a small diameter tube. Derive an expression for the transition density of the gas \(\rho_{c}\) below which microscale effects must be accounted for. Express your result in terms of the gas molecule diameter, universal gas constant, Boltzmann's constant, and the tube diameter. Evaluate the transition density for a \(D=10-\mu \mathrm{m}\)-diameter tube for hydrogen, air, and carbon dioxide. Compare the calculated transition densities with the gas density at atmospheric pressure and \(T=23^{\circ} \mathrm{C}\).

Short Answer

Expert verified
The transition density \(\rho_c\) of an ideal gas flowing within a small diameter tube is given by the expression \(\rho_c = \frac{k}{\sqrt{2} \pi d^2 D R}\), where d is the gas molecule diameter, R is the universal gas constant, k is Boltzmann's constant, and D is the tube diameter. Using this expression, we find the transition densities for a 10-µm diameter tube for hydrogen, air, and carbon dioxide to be \(6.656 \times 10^{-5} kg/m^3\), \(6.531 \times 10^{-4} kg/m^3\), and \(1.148 \times 10^{-3} kg/m^3\), respectively. Comparing these transition densities with their gas densities at atmospheric pressure (\(1.01325 \times 10^5 Pa\)) and 23°C (296.15 K), we conclude that microscale effects are unlikely to occur for hydrogen at typical atmospheric conditions, but might be encountered for air and carbon dioxide under certain lower-density conditions.

Step by step solution

01

Identify relevant parameters

Here are the relevant parameters mentioned in the problem: - Gas molecule diameter (denoted as d) - Universal gas constant (denoted as R) - Boltzmann's constant (denoted as k) - Tube diameter (denoted as D) We need to derive an expression for the transition density (denoted as \(\rho_c\)) that depends on these parameters.
02

Derive the expression for transition density

Consider an ideal gas flowing within a small-diameter tube. When microscale effects begin to manifest, the mean free path (denoted as \(l\)) of a gas molecule is of a similar length scale to the tube diameter \(D\). The mean free path can be calculated using the following formula: \[l = \frac{kT}{\sqrt{2} \pi d^2 P}\] Where T is the temperature and P is the pressure. We have to find the transition density (\(\rho_c\)) below which microscale effects must be accounted for. Let's rewrite the ideal gas law in terms of density (\(\rho\)): \[PV = mRT \quad \Rightarrow \quad \frac{m}{V} = \rho = \frac{P}{RT}\] Now, rearrange the pressure term in the mean free path formula and replace it using the ideal gas law written in terms of density: \[P = \frac{kT}{\sqrt{2} \pi d^2 l} = \rho RT\] Now we can solve for transition density (\(\rho_c\)): \[\rho_c = \frac{kT}{\sqrt{2} \pi d^2 l RT} = \frac{k}{\sqrt{2} \pi d^2 D R}\]
03

Evaluate the transition density for the 10-μm diameter tube

Given that the tube diameter \(D = 10 \mu m\), we will now calculate the transition densities for hydrogen, air, and carbon dioxide: For hydrogen: - Molecule diameter \(d_H = 2.89 \times 10^{-10}m\) - Molecular weight \(M_H = 2 \times 1.0079 \, g/mol\) For air (considered as a mixture of 78% Nitrogen and 22% Oxygen, by volume): - Molecule diameter \(d_{air} = 3.62 \times 10^{-10}m\) - Molecular weight \(M_{air} = 0.78 \times 28.0134 + 0.22 \times 31.9988\, g/mol\) For carbon dioxide: - Molecule diameter \(d_{CO2} = 3.3 \times 10^{-10}m\) - Molecular weight \(M_{CO2} = 44.01 \, g/mol\) Now, we can find the transition densities for each gas using the derived expression for \(\rho_c\): \[\rho_c = \frac{k}{\sqrt{2} \pi d^2 D R}\] Using the universal gas constant \(R = 8.3145 \, J/(mol\cdot K)\) and Boltzmann's constant \(k = 1.38066 \times 10^{-23} J/K\), we find the following results: For hydrogen: \(\rho_{c,H} = 6.656 \times 10^{-5} kg/m^3\) For air: \(\rho_{c,air} = 6.531 \times 10^{-4} kg/m^3\) For carbon dioxide: \(\rho_{c,CO2} = 1.148 \times 10^{-3} kg/m^3\)
04

Compare with gas densities at atmospheric pressure and 23°C

Now, we will compare the calculated transition densities with the gas densities at atmospheric pressure and a temperature of 23°C (296.15 K). Atmospheric pressure is given as: \(P_{atm} = 1.01325 \times 10^5 Pa\) Using the ideal gas law, we can calculate the gas densities: For hydrogen: - \(\rho_{H} = \frac{P_{atm} M_H}{R T} = 8.170 \times 10^{-2} kg/m^3\) For air: - \(\rho_{air} = \frac{P_{atm} M_{air}}{R T} = 1.146 \times 10 kg/m^3\) For carbon dioxide: - \(\rho_{CO2} = \frac{P_{atm} M_{CO2}}{R T} = 1.814 \times 10 kg/m^3\) Comparing the transition densities with the gas densities at atmospheric pressure and 23°C, we can observe the following: - For hydrogen, the calculated transition density \(\rho_{c,H}\) is significantly smaller than its gas density at atmospheric pressure and 23°C. Therefore, microscale effects are unlikely to be encountered at typical atmospheric conditions. - For air and carbon dioxide, the transition densities \(\rho_{c,air}\) and \(\rho_{c,CO2}\) are smaller than their gas densities at atmospheric pressure and 23°C. This indicates that microscale effects might occur under certain conditions when gas density becomes lower than the typical atmospheric conditions.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Ideal Gas Behavior
The behavior of an ideal gas is a foundational topic in chemistry and physics, providing a basic understanding of how gases respond to different conditions. The ideal gas law, expressed as \( PV = nRT \), relates the pressure \( P \), volume \( V \), number of moles \( n \), temperature \( T \) and the universal gas constant \( R \). This law assumes that gas particles are point particles with no volume and that there are no intermolecular forces between them.

In this context, density \( \rho \) can also be derived from the ideal gas law by considering \( \rho = \frac{m}{V} \) and \( PV = mRT \) for a given mass of gas. It simplifies further to \( \rho = \frac{P}{RT} \), setting the stage to explore microscale effects in conditions where gas molecules are packed closely, like within a small diameter tube as in the exercise.
Microscale Effects
Microscale effects become significant when dealing with the flow of gases at scales comparable to the molecules themselves. Such effects are neglected in macroscopic descriptions of gas behavior, like the ideal gas law, which makes certain assumptions that break down at the microscale.

Microscale effects can include slippage of the gas at boundaries, variance from the classic viscosity and thermal conductivity assumptions, and non-equilibrium thermodynamics. Understanding these effects is crucial for applications in microfluidics and in industries where gas behavior at microscales affects performance and efficiency. The transition to conditions where microscale effects must be considered is governed by the Knudsen number, which is a ratio of the mean free path of gas molecules to a characteristic length scale—such as the diameter of the tube.
Mean Free Path
The mean free path \( l \) is a measure of the average distance a molecule travels between collisions with other molecules. It is calculated by \( l = \frac{kT}{\sqrt{2} \pi d^2 P} \) where \( k \) is the Boltzmann's constant, \( d \) is the diameter of the gas molecule, \( P \) is the pressure, and \( T \) is the temperature.

For an ideal gas within a small diameter tube, when the mean free path is comparable to the tube diameter, microscale effects become important, and the standard continuum assumptions of fluid dynamics do not hold. This is why the transition density \( \rho_c \) was derived, helping to indicate when to consider these microscale effects for accurate gas flow behavior analysis in confined geometries. In general, gases with a high mean free path relative to the system dimensions exhibit behavior that may require a departure from the ideal gas model and a look into the kinetic theory of gases.

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Most popular questions from this chapter

An air heater for an industrial application consists of an insulated, concentric tube annulus, for which air flows through a thin-walled inner tube. Saturated steam flows through the outer annulus, and condensation of the steam maintains a uniform temperature \(T_{s}\) on the tube surface. Consider conditions for which air enters a 50 -mmdiameter tube at a pressure of \(5 \mathrm{~atm}\), a temperature of \(T_{m, i}=17^{\circ} \mathrm{C}\), and a flow rate of \(\dot{m}=0.03 \mathrm{~kg} / \mathrm{s}\), while saturated steam at \(2.455\) bars condenses on the outer surface of the tube. If the length of the annulus is \(L=5 \mathrm{~m}\), what are the outlet temperature \(T_{m, o}\) and pressure \(p_{o}\) of the air? What is the mass rate at which condensate leaves the annulus?

Air flowing through a tube of \(75-\mathrm{mm}\) diameter passes over a 150 -mm- long roughened section that is constructed from naphthalene having the properties \(M=128.16 \mathrm{~kg} / \mathrm{kmol}\) and \(p_{\mathrm{sat}}(300 \mathrm{~K})=1.31 \times 10^{-4} \mathrm{bar}\). The air is at \(1 \mathrm{~atm}\) and \(300 \mathrm{~K}\), and the Reynolds number is \(R e_{D}=35,000\). In an experiment for which flow was maintained for \(3 \mathrm{~h}\), mass loss due to sublimation from the roughened surface was determined to be \(0.01 \mathrm{~kg}\). What is the associated convection mass transfer coefficient? What would be the corresponding convection heat transfer coefficient? Contrast these results with those predicted by conventional smooth tube correlations.

A thin-walled, uninsulated \(0.3\)-m-diameter duct is used to route chilled air at \(0.05 \mathrm{~kg} / \mathrm{s}\) through the attic of a large commercial building. The attic air is at \(37^{\circ} \mathrm{C}\), and natural circulation provides a convection coefficient of \(2 \mathrm{~W} / \mathrm{m}^{2}+\mathrm{K}\) at the outer surface of the duct. If chilled air enters a \(15-\mathrm{m}\)-long duct at \(7^{\circ} \mathrm{C}\), what is its exit temperature and the rate of heat gain? Properties of the chilled air may be evaluated at an assumed average temperature of \(300 \mathrm{~K}\).

A mass transfer operation is preceded by laminar flow of a gaseous species B through a circular tube that is sufficiently long to achieve a fully developed velocity profile. Once the fully developed condition is reached, the gas enters a section of the tube that is wetted with a liquid film (A). The film maintains a uniform vapor density \(\rho_{\Lambda_{S}}\) along the tube surface. (a) Write the differential equation and boundary conditions that govern the species A mass density distribution, \(\rho_{A}(x, r)\), for \(x>0\). (b) What is the heat transfer analog to this problem? From this analog, write an expression for the average Sherwood number associated with mass exchange over the region \(0 \leq x \leq L\). (c) Beginning with application of conservation of species to a differential control volume of extent \(\pi r_{o}^{2} d x\), derive an expression (Equation 8.86) that may be used to determine the mean vapor density \(\rho_{\mathrm{A}, \mathrm{m}, \mathrm{Q}}\) at \(x=L\). (d) Consider conditions for which species \(\mathrm{B}\) is air at \(25^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) and the liquid film consists of water, also at \(25^{\circ} \mathrm{C}\). The flow rate is \(\dot{m}=2.5 \times 10^{-4} \mathrm{~kg} / \mathrm{s}\), and the tube diameter is \(D=10 \mathrm{~mm}\). What is the mean vapor density at the tube outlet if \(L=1 \mathrm{~m}\) ?

In the final stages of production, a pharmaceutical is sterilized by heating it from 25 to \(75^{\circ} \mathrm{C}\) as it moves at \(0.2 \mathrm{~m} / \mathrm{s}\) through a straight thin-walled stainless steel tube of \(12.7=\mathrm{mm}\) diameter. A uniform heat flux is maintained by an electric resistance heater wrapped around the outer surface of the tube. If the tube is \(10 \mathrm{~m}\) long, what is the required heat flux? If fluid enters the tube with a fully developed velocity profile and a uniform temperature profile, what is the surface temperature at the tube exit and at a distance of \(0.5 \mathrm{~m}\) from the entrance? Fluid properties may be approximated as \(\rho=\) \(1000 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=4000 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, m=2 \times 10^{-3} \mathrm{~kg} / \mathrm{s} \cdot \mathrm{m}\), \(k=0.8 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and \(P r=10\).

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