Kinetic theory of gases



The kinetic theory of gases is a simple classical model of the thermodynamic behavior of gases. It treats a gas as composed of numerous particles, too small to see with a microscope, which are constantly in random motion. Their collisions with each other and with the walls of their container are used to explain physical properties of the gas—for example, the relationship between its temperature, pressure, and volume. The particles are now known to be the atoms or molecules of the gas.

The basic version of the model describes an ideal gas. It treats the collisions as perfectly elastic and as the only interaction between the particles, which are additionally assumed to be much smaller than their average distance apart.

The theory's introduction allowed many principal concepts of thermodynamics to be established. It explains the macroscopic properties of gases, such as volume, pressure, and temperature, as well as transport properties such as viscosity, thermal conductivity and mass diffusivity. Due to the time reversibility of microscopic dynamics (microscopic reversibility), the kinetic theory is also connected to the principle of detailed balance, in terms of the fluctuation-dissipation theorem (for Brownian motion) and the Onsager reciprocal relations.

The theory was historically significant as the first explicit exercise of the ideas of statistical mechanics.

History
In about 50 BCE, the Roman philosopher Lucretius proposed that apparently static macroscopic bodies were composed on a small scale of rapidly moving atoms all bouncing off each other. This Epicurean atomistic point of view was rarely considered in the subsequent centuries, when Aristotlean ideas were dominant.



In 1738 Daniel Bernoulli published Hydrodynamica, which laid the basis for the kinetic theory of gases. In this work, Bernoulli posited the argument, that gases consist of great numbers of molecules moving in all directions, that their impact on a surface causes the pressure of the gas, and that their average kinetic energy determines the temperature of the gas. The theory was not immediately accepted, in part because conservation of energy had not yet been established, and it was not obvious to physicists how the collisions between molecules could be perfectly elastic.

Other pioneers of the kinetic theory, whose work was also largely neglected by their contemporaries, were Mikhail Lomonosov (1747), Georges-Louis Le Sage (ca. 1780, published 1818), John Herapath (1816) and John James Waterston (1843), which connected their research with the development of mechanical explanations of gravitation. In 1856 August Krönig created a simple gas-kinetic model, which only considered the translational motion of the particles.

In 1857 Rudolf Clausius developed a similar, but more sophisticated version of the theory, which included translational and, contrary to Krönig, also rotational and vibrational molecular motions. In this same work he introduced the concept of mean free path of a particle. In 1859, after reading a paper about the diffusion of molecules by Clausius, Scottish physicist James Clerk Maxwell formulated the Maxwell distribution of molecular velocities, which gave the proportion of molecules having a certain velocity in a specific range. This was the first-ever statistical law in physics. Maxwell also gave the first mechanical argument that molecular collisions entail an equalization of temperatures and hence a tendency towards equilibrium. In his 1873 thirteen page article 'Molecules', Maxwell states: "we are told that an 'atom' is a material point, invested and surrounded by 'potential forces' and that when 'flying molecules' strike against a solid body in constant succession it causes what is called pressure of air and other gases." In 1871, Ludwig Boltzmann generalized Maxwell's achievement and formulated the Maxwell–Boltzmann distribution. The logarithmic connection between entropy and probability was also first stated by Boltzmann.

At the beginning of the 20th century, atoms were considered by many physicists to be purely hypothetical constructs, rather than real objects. An important turning point was Albert Einstein's (1905) and Marian Smoluchowski's (1906) papers on Brownian motion, which succeeded in making certain accurate quantitative predictions based on the kinetic theory.

Following the development of the Boltzmann equation, a framework for its use in developing transport equations was developed independently by David Enskog and Sydney Chapman in 1917 and 1916. The framework provided a route to prediction of the transport properties of dilute gases, and became known as Chapman–Enskog theory. The framework was gradually expanded throughout the following century, eventually becoming a route to prediction of transport properties in real, dense gases.

Assumptions
The application of kinetic theory to ideal gases makes the following assumptions:
 * The gas consists of very small particles. This smallness of their size is such that the sum of the volume of the individual gas molecules is negligible compared to the volume of the container of the gas. This is equivalent to stating that the average distance separating the gas particles is large compared to their size, and that the elapsed time during a collision between particles and the container's wall is negligible when compared to the time between successive collisions.
 * The number of particles is so large that a statistical treatment of the problem is well justified. This assumption is sometimes referred to as the thermodynamic limit.
 * The rapidly moving particles constantly collide among themselves and with the walls of the container, and all these collisions are perfectly elastic.
 * Interactions (i.e. collisions) between particles are strictly binary and uncorrelated, meaning that there are no three-body (or higher) interactions, and the particles have no memory.
 * Except during collisions, the interactions among molecules are negligible. They exert no other forces on one another.

Thus, the dynamics of particle motion can be treated classically, and the equations of motion are time-reversible.

As a simplifying assumption, the particles are usually assumed to have the same mass as one another; however, the theory can be generalized to a mass distribution, with each mass type contributing to the gas properties independently of one another in agreement with Dalton's Law of partial pressures. Many of the model's predictions are the same whether or not collisions between particles are included, so they are often neglected as a simplifying assumption in derivations (see below).

More modern developments, such as Revised Enskog Theory and the Extended BGK model, relax one or more of the above assumptions. These can accurately describe the properties of dense gases, and gases with internal degrees of freedom, because they include the volume of the particles as well as contributions from intermolecular and intramolecular forces as well as quantized molecular rotations, quantum rotational-vibrational symmetry effects, and electronic excitation. While theories relaxing the assumptions that the gas particles occupy negligible volume and that collisions are strictly elastic have been successful, it has been shown that relaxing the requirement of interactions being binary and uncorrelated will eventually lead to divergent results.

Pressure and kinetic energy
In the kinetic theory of gases, the pressure is assumed to be equal to the force (per unit area) exerted by the individual gas atoms or molecules hitting and rebounding from the gas container's surface.

Consider a gas particle traveling at velocity, $v_i$, along the $$\hat{i}$$-direction in an enclosed volume with characteristic length, $$L_i$$, cross-sectional area, $$A_i$$, and volume, $$V = A_i L_i$$. The gas particle encounters a boundary after characteristic time

$$ t = L_i / v_i.$$

The momentum of the gas particle can then be described as

$$ p_i = m v_i = m L_i / t .$$

We combine the above with Newton's second law, which states that the force experienced by a particle is related to the time rate of change of its momentum, such that

$$F_i = \frac{\mathrm{d}p_i}{\mathrm{d}t} = \frac{m L_i}{t^2}=\frac{m v_i^2}{L_i}.$$

Now consider a large number, N, of gas particles with random orientation in a three-dimensional volume. Because the orientation is random, the average particle speed, v, in every direction is identical

$$v^2 = {\vec{v}_x^2} = {\vec{v}_y^2} = {\vec{v}_z^2}.$$

Further, assume that the volume is symmetrical about its three dimensions, $$\hat{i}, \hat{j}, \hat{k}$$, such that

$$v = v_i=v_j=v_k,$$ $$F = F_i = F_j = F_k,$$ $$A_i=A_j=A_k.$$ The total surface area on which the gas particles act is therefore $$A = 3 * A_i.$$

The pressure exerted by the collisions of the N gas particles with the surface can then be found by adding the force contribution of every particle and dividing by the interior surface area of the volume,

$$P = \frac{N \overline{F}}{A}=\frac{NLF}{V} $$ $$ \Rightarrow PV=NLF = \frac{N}{3} m v^2.$$

The total translational kinetic energy $$K_t $$ of the gas is defined as $$K_t = \frac{N}{2} m v^2 ,$$ providing the result $$PV = \frac{2}{3} K_t .$$

This is an important, non-trivial result of the kinetic theory because it relates pressure, a macroscopic property, to the translational kinetic energy of the molecules, which is a microscopic property.

Temperature and kinetic energy
Rewriting the above result for the pressure as $PV = \frac{Nmv^2}{3} $, we may combine it with the ideal gas law

where $$ k_\mathrm{B}$$ is the Boltzmann constant and $$ T$$ the absolute temperature defined by the ideal gas law, to obtain

$$k_\mathrm{B} T = {m v^2\over 3}, $$ which leads to a simplified expression of the average translational kinetic energy per molecule, $$ \frac{1}{2} m v^2 = \frac{3}{2} k_\mathrm{B} T.$$ The translational kinetic energy of the system is $$N$$ times that of a molecule, namely $ K_t = \frac{1}{2} N m v^2 $. The temperature, $$ T$$ is related to the translational kinetic energy by the description above, resulting in

which becomes

Equation ($$) is one important result of the kinetic theory: The average molecular kinetic energy is proportional to the ideal gas law's absolute temperature. From equations ($$) and ($$), we have

Thus, the product of pressure and volume per mole is proportional to the average translational molecular kinetic energy.

Equations ($$) and ($$) are called the "classical results", which could also be derived from statistical mechanics; for more details, see:

The equipartition theorem requires that kinetic energy is partitioned equally between all kinetic degrees of freedom, D. A monotatomic gas is axially symmetric about each spatial axis, so that D = 3 comprising translational motion along each axis. A diatomic gas is axially symmetric about only one axis, so that D = 5, comprising translational motion along three axes and rotational motion along two axes. A polyatomic gas, like water, is not radially symmetric about any axis, resulting in D = 6, comprising 3 translational and 3 rotational degrees of freedom.

Because the equipartition theorem requires that kinetic energy is partitioned equally, the total kinetic energy is

$$ K =D K_t = \frac{D}{2} N m v^2. $$

Thus, the energy added to the system per gas particle kinetic degree of freedom is

$$ \frac{K}{ND} = \frac{1}{2} k_B T. $$

Therefore, the kinetic energy per kelvin of one mole of monatomic ideal gas (D = 3) is

$$ K = \frac{D}{2} k_B N_A T = \frac{3}{2} R, $$

where $$N_A$$ is the Avogadro constant, and R is the ideal gas constant.

Thus, the kinetic energy per unit kelvin of an ideal monoatomic gas can be calculated easily:
 * per mole: 12.47 J / K
 * per molecule: 20.7 yJ / K = 129 μeV / K

At standard temperature (273.15 K), the kinetic energy can also be obtained:
 * per mole: 3406 J
 * per molecule: 5.65 zJ = 35.2 meV.

At higher temperatures (typically thousands of kelvins), vibrational modes become active to provide additional degrees of freedom, creating a temperature-dependence on D and the total molecular energy. Quantum statistical mechanics is needed to accurately compute these contributions.

Collisions with container wall
For an ideal gas in equilibrium, the rate of collisions with the container wall and velocity distribution of particles hitting the container wall can be calculated based on naive kinetic theory, and the results can be used for analyzing effusive flow rates, which is useful in applications such as the gaseous diffusion method for isotope separation.

Assume that in the container, the number density (number per unit volume) is $$n=N/V$$ and that the particles obey Maxwell's velocity distribution: $$f_\text{Maxwell}(v_x,v_y,v_z) \, dv_x \, dv_y \, dv_z = \left(\frac{m}{2 \pi k_B T}\right)^{3/2} e^{- \frac{mv^2}{2k_BT}} \, dv_x \, dv_y \, dv_z$$

Then for a small area $$dA$$ on the container wall, a particle with speed $$v$$ at angle $$\theta$$ from the normal of the area $$dA$$, will collide with the area within time interval $$dt$$, if it is within the distance $$vdt$$ from the area $$dA$$. Therefore, all the particles with speed $$v$$ at angle $$\theta$$ from the normal that can reach area $$dA$$ within time interval $$dt$$ are contained in the tilted pipe with a height of $$v\cos (\theta) dt$$ and a volume of $$v\cos (\theta) dAdt$$.

The total number of particles that reach area $$dA$$ within time interval $$dt$$ also depends on the velocity distribution; All in all, it calculates to be:$$n v \cos(\theta) \, dA\, dt \times\left(\frac{m}{2 \pi k_BT}\right)^{3/2} e^{- \frac{mv^2}{2k_BT}} \left( v^2 \sin(\theta) \, dv \, d\theta \, d\phi \right).$$

Integrating this over all appropriate velocities within the constraint $$v>0,0<\theta<\pi/2,0<\phi<2\pi$$ yields the number of atomic or molecular collisions with a wall of a container per unit area per unit time: $$J_\text{collision} =\frac{\int_0^{\pi/2}\cos \theta \sin \theta d\theta}{\int_0^{\pi}\sin \theta d\theta}\times n \bar v= \frac{1}{4}n \bar v = \frac{n}{4} \sqrt{\frac{8 k_\mathrm{B} T}{\pi m}}. $$

This quantity is also known as the "impingement rate" in vacuum physics. Note that to calculate the average speed $$\bar v$$ of the Maxwell's velocity distribution, one has to integrate over$$v>0,0<\theta<\pi,0<\phi<2\pi$$.

The momentum transfer to the container wall from particles hitting the area $$dA$$ with speed $$v$$ at angle $$\theta$$ from the normal, in time interval $$dt$$ is:$$[2mv \cos(\theta)]\times n v \cos(\theta) \, dA\, dt \times\left(\frac{m}{2 \pi k_BT}\right)^{3/2} e^{- \frac{mv^2}{2k_BT}} \left( v^2 \sin(\theta) \, dv \, d\theta \, d\phi \right).$$Integrating this over all appropriate velocities within the constraint $$v>0,0<\theta<\pi/2,0<\phi<2\pi$$ yields the pressure (consistent with Ideal gas law):$$P=\frac{2\int_0^{\pi/2}\cos^2 \theta \sin \theta d\theta}{\int_0^{\pi}\sin \theta d\theta}\times n mv_\text{rms}^2=\frac{1}{3}n mv_\text{rms}^2=\frac{2}{3}n\langle E_{kin}\rangle=nk_\mathrm{B} T $$If this small area $$A$$ is punched to become a small hole, the effusive flow rate will be: $$\Phi_\text{effusion} = J_\text{collision} A= n A \sqrt{\frac{k_\mathrm{B} T}{2 \pi m}}. $$

Combined with the ideal gas law, this yields $$\Phi_\text{effusion} = \frac{P A}{\sqrt{2 \pi m k_\mathrm{B} T}}. $$

The above expression is consistent with Graham's law.

To calculate the velocity distribution of particles hitting this small area, we must take into account that all the particles with $$(v,\theta,\phi)$$ that hit the area $$dA$$ within the time interval $$dt$$ are contained in the tilted pipe with a height of $$v\cos (\theta) dt$$ and a volume of $$v\cos (\theta) dAdt$$; Therefore, compared to the Maxwell distribution, the velocity distribution will have an extra factor of $$v\cos \theta$$: $$\begin{align} f(v,\theta,\phi) \, dv \, d\theta \, d\phi &=\lambda v\cos{\theta}{\times} \left(\frac{m}{2 \pi k T}\right)^{3/2}e^{- \frac{mv^2}{2k_\mathrm{B} T}}(v^2\sin{\theta} \, dv \, d\theta \, d\phi) \\ \end{align}$$ with the constraint $v>0,\, 0<\theta<\frac \pi 2,\, 0<\phi<2\pi$. The constant $$\lambda$$ can be determined by the normalization condition $$\int f(v,\theta,\phi) \, dv \, d\theta \, d\phi=1$$ to be ${4}/{\bar v} $, and overall:$$\begin{align} f(v,\theta,\phi) \, dv \, d\theta \, d\phi &=\frac{1}{2\pi} \left(\frac{m}{k_\mathrm{B} T}\right)^2e^{- \frac{mv^2}{2k_\mathrm{B} T}} (v^3\sin{\theta}\cos{\theta} \, dv \, d\theta \, d\phi) \\ \end{align};\quad v>0,\, 0<\theta<\frac \pi 2,\, 0<\phi<2\pi$$

Speed of molecules
From the kinetic energy formula it can be shown that $$v_\text{p} = \sqrt{2 \cdot \frac{k_\mathrm{B} T}{m}},$$ $$ \bar v = \frac {2}{\sqrt{\pi}} v_p = \sqrt{\frac {8}{\pi} \cdot \frac{k_\mathrm{B} T}{m}},$$ $$v_\text{rms} = \sqrt{\frac{3}{2}} v_p = \sqrt{{3} \cdot \frac {k_\mathrm{B} T}{m}},$$ where v is in m/s, T is in kelvin, and m is the mass of one molecule of gas in kg. The most probable (or mode) speed $$v_\text{p}$$ is 81.6% of the root-mean-square speed $$v_\text{rms}$$, and the mean (arithmetic mean, or average) speed $$\bar v$$ is 92.1% of the rms speed (isotropic distribution of speeds).

See:
 * Average,
 * Root-mean-square speed
 * Arithmetic mean
 * Mean
 * Mode (statistics)

Mean free path
In kinetic theory of gases, the mean free path is the average distance traveled by a molecule, or a number of molecules per volume, before they make their first collision. Let $$ \sigma $$ be the collision cross section of one molecule colliding with another. As in the previous section, the number density $$ n $$ is defined as the number of molecules per (extensive) volume, or $$ n = N/V $$. The collision cross section per volume or collision cross section density is $$ n \sigma $$, and it is related to the mean free path $$l$$ by$$l = \frac {1} {n \sigma \sqrt{2}} $$

Notice that the unit of the collision cross section per volume $$ n \sigma $$ is reciprocal of length.

Transport properties
The kinetic theory of gases deals not only with gases in thermodynamic equilibrium, but also very importantly with gases not in thermodynamic equilibrium. This means using Kinetic Theory to consider what are known as "transport properties", such as viscosity, thermal conductivity, mass diffusivity and thermal diffusion.

In its most basic form, Kinetic gas theory is only applicable to dilute gases. The extension of Kinetic gas theory to dense gas mixtures, Revised Enskog Theory, was developed in 1983-1987 by E. G. D. Cohen, J. M. Kincaid and M. Lòpez de Haro,   building on work by H. van Beijeren and M. H. Ernst.

Viscosity and kinetic momentum
In books on elementary kinetic theory one can find results for dilute gas modeling that are used in many fields. Derivation of the kinetic model for shear viscosity usually starts by considering a Couette flow where two parallel plates are separated by a gas layer. The upper plate is moving at a constant velocity to the right due to a force F. The lower plate is stationary, and an equal and opposite force must therefore be acting on it to keep it at rest. The molecules in the gas layer have a forward velocity component $$u$$ which increase uniformly with distance $$y$$ above the lower plate. The non-equilibrium flow is superimposed on a Maxwell-Boltzmann equilibrium distribution of molecular motions.

Inside a dilute gas in a Couette flow setup, let $$ u_{0} $$ be the forward velocity of the gas at a horizontal flat layer (labeled as $$y=0$$); $$ u_{0} $$ is along the horizontal direction. The number of molecules arriving at the area $$dA$$ on one side of the gas layer, with speed $$v$$ at angle $$\theta$$ from the normal, in time interval $$dt$$ is $$nv\cos({\theta})\, dA \, dt \times \left(\frac{m}{2 \pi k_\mathrm{B} T}\right)^{3/2} \, e^{- \frac{mv^2}{2 k_\mathrm{B} T}} (v^2\sin{\theta} \, dv \, d\theta \, d\phi)$$

These molecules made their last collision at $$y=\pm l\cos \theta$$, where $$l$$ is the mean free path. Each molecule will contribute a forward momentum of $$p_{x}^{\pm} = m \left( u_{0} \pm l \cos \theta \,{d u \over dy} \right), $$ where plus sign applies to molecules from above, and minus sign below. Note that the forward velocity gradient $$du/dy$$ can be considered to be constant over a distance of mean free path.

Integrating over all appropriate velocities within the constraint $$\begin{cases} v>0\\ 0<\theta<\pi/2\\ 0<\phi<2\pi \end{cases}$$ yields the forward momentum transfer per unit time per unit area (also known as shear stress): $$\tau^{\pm} = \frac {1}{4} \bar v n \cdot m \left( u_{0} \pm \frac {2}{3} l \,{d u \over dy} \right) $$

The net rate of momentum per unit area that is transported across the imaginary surface is thus $$\tau = \tau^{+} - \tau^{-} = \frac {1}{3} \bar v n m \cdot l \,{d u \over dy} $$

Combining the above kinetic equation with Newton's law of viscosity $$\tau = \eta \,{d u \over dy} $$ gives the equation for shear viscosity, which is usually denoted $$ \eta_{0} $$ when it is a dilute gas: $$\eta_{0} = \frac {1} {3} \bar v n m l $$

Combining this equation with the equation for mean free path gives $$\eta_{0} = \frac {1} {3 \sqrt{2} } \frac {m \cdot \bar v} {\sigma}$$

Maxwell-Boltzmann distribution gives the average (equilibrium) molecular speed as $$\bar v = \frac{2}{\sqrt{\pi}} v_{p} = 2 \sqrt{\frac{2}{\pi} \cdot \frac {k_\mathrm{B}T}{m}} $$ where $$v_{p}$$ is the most probable speed. We note that $$k_{B} \cdot N_{A} = R \quad \text{and} \quad M = m \cdot N_{A} $$

and insert the velocity in the viscosity equation above. This gives the well known equation (with $$\sigma$$ subsequently estimated below) for shear viscosity for dilute gases:

$$\eta_{0} = \frac {2} {3 \sqrt{\pi} } \cdot \frac {\sqrt{m k_\mathrm{B} T}} { \sigma } = \frac {2} {3 \sqrt{\pi} } \cdot \frac {\sqrt{MRT}} { \sigma \cdot N_{A} } $$

and $$ M $$ is the molar mass. The equation above presupposes that the gas density is low (i.e. the pressure is low). This implies that the transport of momentum through the gas due to the translational motion of molecules is much larger than the transport due to momentum being transferred between molecules during collisions. The transfer of momentum between molecules is explicitly accounted for in Revised Enskog theory, which relaxes the requirement of a gas being dilute. The viscosity equation further presupposes that there is only one type of gas molecules, and that the gas molecules are perfect elastic and hard core particles of spherical shape. This assumption of elastic, hard core spherical molecules, like billiard balls, implies that the collision cross section of one molecule can be estimated by

$$\sigma = \pi \left( 2 r \right)^2 = \pi d^2 $$

The radius $$r$$ is called collision cross section radius or kinetic radius, and the diameter $$d$$ is called collision cross section diameter or kinetic diameter of a molecule in a monomolecular gas. There are no simple general relation between the collision cross section and the hard core size of the (fairly spherical) molecule. The relation depends on shape of the potential energy of the molecule. For a real spherical molecule (i.e. a noble gas atom or a reasonably spherical molecule) the interaction potential is more like the Lennard-Jones potential or Morse potential which have a negative part that attracts the other molecule from distances longer than the hard core radius. The radius for zero Lennard-Jones potential may then be used as a rough estimate for the kinetic radius. However, using this estimate will typically lead to an erroneous temperature dependency of the viscosity. For such interaction potentials, significantly more accurate results are obtained by numerical evaluation of the required collision integrals.

The expression for viscosity obtained from Revised Enskog Theory reduces to the above expression in the limit of infinite dilution, and can be written as

$$\eta = (1 + \alpha_\eta)\eta_0 + \eta_c $$

where $$\alpha_\eta$$ is a term that tends to zero in the limit of infinite dilution that accounts for excluded volume, and $$\eta_c$$ is a term accounting for the transfer of momentum over a non-zero distance between particles during a collision.

Thermal conductivity and heat flux
Following a similar logic as above, one can derive the kinetic model for thermal conductivity of a dilute gas:

Consider two parallel plates separated by a gas layer. Both plates have uniform temperatures, and are so massive compared to the gas layer that they can be treated as thermal reservoirs. The upper plate has a higher temperature than the lower plate. The molecules in the gas layer have a molecular kinetic energy $$\varepsilon$$ which increases uniformly with distance $$y$$ above the lower plate. The non-equilibrium energy flow is superimposed on a Maxwell-Boltzmann equilibrium distribution of molecular motions.

Let $$ \varepsilon_{0} $$ be the molecular kinetic energy of the gas at an imaginary horizontal surface inside the gas layer. The number of molecules arriving at an area $$dA$$ on one side of the gas layer, with speed $$v$$ at angle $$\theta$$ from the normal, in time interval $$dt$$ is $$ nv \cos(\theta)\, dA \, dt \times \left(\frac{m}{2 \pi k_\mathrm{B}T}\right)^{3 / 2} e^{- \frac{mv^2}{2k_BT}} (v^2 \sin(\theta) \, dv \, d\theta \, d\phi)$$

These molecules made their last collision at a distance $$l\cos \theta$$ above and below the gas layer, and each will contribute a molecular kinetic energy of $$ \varepsilon^{\pm} = \left( \varepsilon_{0} \pm m c_v l \cos \theta \, {d T \over dy} \right), $$ where $$c_v$$ is the specific heat capacity. Again, plus sign applies to molecules from above, and minus sign below. Note that the temperature gradient $$dT/dy$$ can be considered to be constant over a distance of mean free path.

Integrating over all appropriate velocities within the constraint $$\begin{cases} v>0\\ 0<\theta<\pi/2\\ 0<\phi<2\pi \end{cases}$$

yields the energy transfer per unit time per unit area (also known as heat flux): $$ q_y^{\pm} = -\frac {1}{4} \bar v n \cdot \left( \varepsilon_{0} \pm \frac {2}{3} m c_v l \,{d T \over dy} \right) $$

Note that the energy transfer from above is in the $$-y$$ direction, and therefore the overall minus sign in the equation. The net heat flux across the imaginary surface is thus $$ q = q_y^{+} - q_y^{-} = -\frac {1}{3} \bar v n m c_v l \,{d T \over dy} $$

Combining the above kinetic equation with Fourier's law $$ q = -\kappa \,{d T \over dy} $$ gives the equation for thermal conductivity, which is usually denoted $$ \kappa_{0} $$ when it is a dilute gas: $$ \kappa_{0} = \frac {1} {3} \bar v n m c_v l $$

Similarly to viscosity, Revised Enskog Theory yields an expression for thermal conductivity that reduces to the above expression in the limit of infinite dilution, and which can be written as $$ \kappa = \alpha_\kappa \kappa_0 + \kappa_c $$

where $$ \alpha_\kappa $$ is a term that tends to unity in the limit of infinite dilution, accounting for excluded volume, and $$ \kappa_c $$ is a term accounting for the transfer of energy across a non-zero distance between particles during a collision.

Diffusion Coefficient and diffusion flux
Following a similar logic as above, one can derive the kinetic model for mass diffusivity of a dilute gas:

Consider a steady diffusion between two regions of the same gas with perfectly flat and parallel boundaries separated by a layer of the same gas. Both regions have uniform number densities, but the upper region has a higher number density than the lower region. In the steady state, the number density at any point is constant (that is, independent of time). However, the number density $$n$$ in the layer increases uniformly with distance $$y$$ above the lower plate. The non-equilibrium molecular flow is superimposed on a Maxwell-Boltzmann equilibrium distribution of molecular motions.

Let $$ n_{0} $$ be the number density of the gas at an imaginary horizontal surface inside the layer. The number of molecules arriving at an area $$dA$$ on one side of the gas layer, with speed $$v$$ at angle $$\theta$$ from the normal, in time interval $$dt$$ is $$ nv\cos(\theta) \, dA \, dt \times \left(\frac{m}{2 \pi k_\mathrm{B}T}\right)^{3 / 2} e^{- \frac{mv^2}{2k_BT}} (v^2\sin(\theta) \, dv\, d\theta \, d\phi)$$

These molecules made their last collision at a distance $$l\cos \theta$$ above and below the gas layer, where the local number density is $$ n^{\pm} = \left( n_{0} \pm l \cos \theta \, {d n \over dy} \right) $$

Again, plus sign applies to molecules from above, and minus sign below. Note that the number density gradient $$dn/dy$$ can be considered to be constant over a distance of mean free path.

Integrating over all appropriate velocities within the constraint

$$\begin{cases} v>0\\ 0<\theta<\pi/2\\ 0<\phi<2\pi \end{cases}$$

yields the molecular transfer per unit time per unit area (also known as diffusion flux): $$ J_y^{\pm} = -\frac {1}{4} \bar v \cdot \left( n_{0} \pm \frac {2}{3} l \, {d n \over dy} \right) $$

Note that the molecular transfer from above is in the $$-y$$ direction, and therefore the overall minus sign in the equation. The net diffusion flux across the imaginary surface is thus $$ J = J_y^{+} - J_y^{-} = -\frac {1}{3} \bar v l {d n \over dy} $$

Combining the above kinetic equation with Fick's first law of diffusion $$ J = -D {d n \over dy} $$ gives the equation for mass diffusivity, which is usually denoted $$ D_{0} $$ when it is a dilute gas: $$ D_{0} = \frac {1} {3} \bar v l $$

The corresponding expression obtained from Revised Enskog Theory may be written as $$ D = \alpha_D D_0 $$ where $$ \alpha_D $$ is a factor that tends to unity in the limit of infinite dilution, which accounts for excluded volume and the variation chemical potentials with density.

Fluctuation and dissipation
The kinetic theory of gases entails that due to the microscopic reversibility of the gas particles' detailed dynamics, the system must obey the principle of detailed balance. Specifically, the fluctuation-dissipation theorem applies to the Brownian motion (or diffusion) and the drag force, which leads to the Einstein–Smoluchowski equation: $$ D = \mu \, k_\text{B} T, $$where

Note that the mobility $μ = v_{d}/F$ can be calculated based on the viscosity of the gas; Therefore, the Einstein–Smoluchowski equation also provides a relation between the mass diffusivity and the viscosity of the gas.
 * $$ is the diffusion coefficient;
 * $$ is the "mobility", or the ratio of the particle's terminal drift velocity to an applied force, $k_{B}$;
 * $μ = v_{d}/F$ is the Boltzmann constant;
 * $$ is the absolute temperature.

Onsager reciprocal relations
The mathematical similarities between the expressions for shear viscocity, thermal conductivity and diffusion coefficient of the ideal (dilute) gas is not a coincidence; It is a direct result of the Onsager reciprocal relations (i.e. the detailed balance of the reversible dynamics of the particles), when applied to the convection (matter flow due to temperature gradient, and heat flow due to pressure gradient) and advection (matter flow due to the velocity of particles, and momentum transfer due to pressure gradient) of the ideal (dilute) gas.