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Kinetic theory of gases

From Wikipedia, the free encyclopedia
Understanding of gas properties in terms of molecular motion
Thetemperature of theideal gas is proportional to the averagekinetic energy of its particles. Thesize ofhelium atoms relative to their spacing is shown to scale under 1,950atmospheres of pressure. The atoms have an average speed relative to their size slowed down here twotrillion fold from that at room temperature.

Thekinetic theory of gases is a simpleclassical model of thethermodynamic behavior ofgases. Its introduction allowed many principal concepts of thermodynamics to be established. It treats a gas as composed of numerous particles, too small to be seen with a microscope, in constant, random motion. These particles are now known to be theatoms ormolecules of the gas. The kinetic theory of gases uses their collisions with each other and with the walls of their container to explainthe relationship between themacroscopic properties of gases, such asvolume,pressure, andtemperature, as well astransport properties such asviscosity,thermal conductivity andmass diffusivity.

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

Due to thetime reversibility of microscopic dynamics (microscopic reversibility), the kinetic theory is also connected to the principle ofdetailed balance, in terms of thefluctuation-dissipation theorem (forBrownian motion) and theOnsager reciprocal relations.

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

History

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See also:Heat § History,Atomism, andHistory of thermodynamics

Kinetic theory of matter

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Antiquity

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In about 50BCE, the Roman philosopherLucretius proposed that apparently static macroscopic bodies were composed on a small scale of rapidly moving atoms all bouncing off each other.[1] ThisEpicurean atomistic point of view was rarely considered in the subsequent centuries, whenAristotlean ideas were dominant.[citation needed]

Modern era

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"Heat is motion"
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Francis Bacon

One of the first and boldest statements on the relationship between motion of particles andheat was by the English philosopherFrancis Bacon in 1620. "It must not be thought that heat generates motion, or motion heat (though in some respects this be true), but that the very essence of heat ... is motion and nothing else."[2] "not a ... motion of the whole, but of the small particles of the body."[3] In 1623, inThe Assayer,Galileo Galilei, in turn, argued that heat, pressure, smell and other phenomena perceived by our senses are apparent properties only, caused by the movement of particles, which is a real phenomenon.[4][5]

John Locke

In 1665, inMicrographia, the English polymathRobert Hooke repeated Bacon's assertion,[6][7] and in 1675, his colleague, Anglo-Irish scientistRobert Boyle noted that a hammer's "impulse" is transformed into the motion of a nail's constituent particles, and that this type of motion is what heat consists of.[8] Boyle also believed that all macroscopic properties, including color, taste and elasticity, are caused by and ultimately consist of nothing but the arrangement and motion of indivisible particles of matter.[9] In a lecture of 1681, Hooke asserted a direct relationship between the temperature of an object and the speed of its internal particles. "Heat ... is nothing but the internal Motion of the Particles of [a] Body; and the hotter a Body is, the more violently are the Particles moved."[10] In a manuscript published 1720, the English philosopherJohn Locke made a very similar statement: "What in our sensation isheat, in the object is nothing butmotion."[11][12] Locke too talked about the motion of the internal particles of the object, which he referred to as its "insensible parts".

Catherine the Great visiting Mikhail Lomonosov

In his 1744 paperMeditations on the Cause of Heat and Cold, Russian polymathMikhail Lomonosov made a relatable appeal to everyday experience to gain acceptance of the microscopic and kinetic nature of matter and heat:[13]

Movement should not be denied based on the fact it is not seen. Who would deny that the leaves of trees move when rustled by a wind, despite it being unobservable from large distances? Just as in this case motion remains hidden due to perspective, it remains hidden in warm bodies due to the extremely small sizes of the moving particles. In both cases, the viewing angle is so small that neither the object nor their movement can be seen.

Lomonosov also insisted that movement of particles is necessary for the processes ofdissolution,extraction anddiffusion, providing as examples the dissolution and diffusion of salts by the action of water particles on the of the “molecules of salt”, the dissolution of metals in mercury, and the extraction of plant pigments by alcohol.[14]

Also thetransfer of heat was explained by the motion of particles. Around 1760, Scottish physicist and chemistJoseph Black wrote: "Many have supposed that heat is a tremulous ... motion of the particles of matter, which ... motion they imagined to be communicated from one body to another."[15]

Kinetic theory of gases

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Daniel Bernoulli
Hydrodynamica front cover

In 1738Daniel Bernoulli publishedHydrodynamica, which laid the basis for thekinetic theory ofgases. 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 averagekinetic energy determines the temperature of the gas. The theory was not immediately accepted, in part becauseconservation of energy had not yet been established, and it was not obvious tophysicists how the collisions between molecules could be perfectly elastic.[16]: 36–37 

Pioneers of the kinetic theory, whose work was also largely neglected by their contemporaries, were Mikhail Lomonosov (1747),[17]Georges-Louis Le Sage (ca. 1780, published 1818),[18]John Herapath (1816)[19] andJohn James Waterston (1843),[20] which connected their research with the development ofmechanical explanations of gravitation.

In 1856August Krönig created a simple gas-kinetic model, which only considered thetranslational motion of the particles.[21] In 1857Rudolf Clausius developed a similar, but more sophisticated version of the theory, which included translational and, contrary to Krönig, alsorotational and vibrational molecular motions. In this same work he introduced the concept ofmean free path of a particle.[22] In 1859, after reading a paper about thediffusion of molecules by Clausius, Scottish physicistJames Clerk Maxwell formulated theMaxwell distribution of molecular velocities, which gave the proportion of molecules having a certain velocity in a specific range.[23] This was the first-ever statistical law in physics.[24] Maxwell also gave the first mechanical argument that molecular collisions entail an equalization of temperatures and hence a tendency towards equilibrium.[25] 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 calledpressure of air and other gases."[26]In 1871,Ludwig Boltzmann generalized Maxwell's achievement and formulated theMaxwell–Boltzmann distribution. Thelogarithmic connection betweenentropy andprobability 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 wasAlbert Einstein's (1905)[27] andMarian Smoluchowski's (1906)[28] papers onBrownian motion, which succeeded in making certain accurate quantitative predictions based on the kinetic theory.

Following the development of theBoltzmann equation, a framework for its use in developing transport equations was developed independently byDavid Enskog andSydney Chapman in 1917 and 1916. The framework provided a route to prediction of the transport properties of dilute gases, and became known asChapman–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

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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 thevolume 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 theirsize, 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 thethermodynamic 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 anduncorrelated, 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 otherforces 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 samemass 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 withDalton'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).[29]

More modern developments, such as therevised Enskog theory and the extendedBhatnagar–Gross–Krook model,[30] relax one or more of the above assumptions. These can accurately describe the properties of dense gases, and gases withinternal 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.[31] 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.[32]

Equilibrium properties

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Pressure and kinetic energy

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In the kinetic theory of gases, thepressure 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,vi{\textstyle v_{i}}, along thei^{\displaystyle {\hat {i}}}-direction in an enclosed volume withcharacteristic length,Li{\displaystyle L_{i}}, cross-sectional area,Ai{\displaystyle A_{i}}, and volume,V=AiLi{\displaystyle V=A_{i}L_{i}}. The gas particle encounters a boundary after characteristic timet=Li/vi.{\displaystyle t=L_{i}/v_{i}.}

Themomentum of the gas particle can then be described aspi=mvi=mLi/t.{\displaystyle p_{i}=mv_{i}=mL_{i}/t.}

We combine the above withNewton's second law, which states that the force experienced by a particle is related to the time rate of change of its momentum, such thatFi=dpidt=mLit2=mvi2Li.{\displaystyle F_{i}={\frac {\mathrm {d} p_{i}}{\mathrm {d} t}}={\frac {mL_{i}}{t^{2}}}={\frac {mv_{i}^{2}}{L_{i}}}.}

Now consider a large number,N{\displaystyle N}, of gas particles with random orientation in a three-dimensional volume. Because the orientation is random, the average particle speed,v{\textstyle v}, in every direction is identicalvx2=vy2=vz2.{\displaystyle v_{x}^{2}=v_{y}^{2}=v_{z}^{2}.}

Further, assume that the volume is symmetrical about its three dimensions,i^,j^,k^{\displaystyle {\hat {i}},{\hat {j}},{\hat {k}}}, such thatV=Vi=Vj=Vk,F=Fi=Fj=Fk,Ai=Aj=Ak.{\displaystyle {\begin{aligned}V={}&V_{i}=V_{j}=V_{k},\\F={}&F_{i}=F_{j}=F_{k},\\&A_{i}=A_{j}=A_{k}.\end{aligned}}}The total surface area on which the gas particles act is thereforeA=3Ai.{\displaystyle A=3A_{i}.}

The pressure exerted by the collisions of theN{\displaystyle 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=NF¯A=NLFV{\displaystyle P={\frac {N{\overline {F}}}{A}}={\frac {NLF}{V}}}PV=NLF=N3mv2.{\displaystyle \Rightarrow PV=NLF={\frac {N}{3}}mv^{2}.}

The total translationalkinetic energyKt{\displaystyle K_{\text{t}}} of the gas is defined asKt=N2mv2,{\displaystyle K_{\text{t}}={\frac {N}{2}}mv^{2},}providing the resultPV=23Kt.{\displaystyle PV={\frac {2}{3}}K_{\text{t}}.}

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

The mass density of a gasρ{\displaystyle \rho } is expressed through the total mass of gas particles and through volume of this gas:ρ=NmV{\displaystyle \rho ={\frac {Nm}{V}}}. Taking this into account, the pressure is equal toP=ρv23.{\displaystyle P={\frac {\rho v^{2}}{3}}.}

Relativistic expression for this formula is[33]

P=2ρc23((1v2¯/c2)1/21),{\displaystyle P={\frac {2\rho c^{2}}{3}}\left({\left(1-{\overline {v^{2}}}/c^{2}\right)}^{-1/2}-1\right),}wherec{\displaystyle c} isspeed of light. In the limit of small speeds, the expression becomesPρv2¯/3{\displaystyle P\approx \rho {\overline {v^{2}}}/3}.

Temperature and kinetic energy

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Rewriting the above result for the pressure asPV=13Nmv2{\textstyle PV={\frac {1}{3}}Nmv^{2}}, we may combine it with theideal gas law

PV=NkBT,{\displaystyle PV=Nk_{\mathrm {B} }T,}1

wherekB{\displaystyle k_{\mathrm {B} }} is theBoltzmann constant andT{\displaystyle T} is theabsolutetemperature defined by the ideal gas law, to obtainkBT=13mv2,{\displaystyle k_{\mathrm {B} }T={\frac {1}{3}}mv^{2},}which leads to a simplified expression of the average translational kinetic energy per molecule,[34]12mv2=32kBT.{\displaystyle {\frac {1}{2}}mv^{2}={\frac {3}{2}}k_{\mathrm {B} }T.}The translational kinetic energy of the system isN{\displaystyle N} times that of a molecule, namelyKt=12Nmv2{\textstyle K_{\text{t}}={\frac {1}{2}}Nmv^{2}}. The temperature,T{\displaystyle T} is related to the translational kinetic energy by the description above, resulting in

T=13mv2kB{\displaystyle T={\frac {1}{3}}{\frac {mv^{2}}{k_{\mathrm {B} }}}}2

which becomes

T=23KtNkB.{\displaystyle T={\frac {2}{3}}{\frac {K_{\text{t}}}{Nk_{\mathrm {B} }}}.}3

Equation (3) 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 (1) and (3), we have

PV=23Kt.{\displaystyle PV={\frac {2}{3}}K_{\text{t}}.}4

Thus, the product of pressure and volume permole is proportional to the averagetranslational molecular kinetic energy.

Equations (1) and (4) are called the "classical results", which could also be derived fromstatistical mechanics;for more details, see:[35]

Theequipartition theorem requires that kinetic energy is partitioned equally between all kineticdegrees of freedom,D. A monatomic gas is axially symmetric about each spatial axis, so thatD = 3 comprising translational motion along each axis. A diatomic gas is axially symmetric about only one axis, so thatD = 5, comprising translational motion along three axes and rotational motion along two axes. A polyatomic gas, likewater, is not radially symmetric about any axis, resulting inD = 6, comprising 3 translational and 3 rotational degrees of freedom.

Because theequipartition theorem requires that kinetic energy is partitioned equally, the total kinetic energy isK=DKt=D2Nmv2.{\displaystyle K=DK_{\text{t}}={\frac {D}{2}}Nmv^{2}.}

Thus, the energy added to the system per gas particle kinetic degree of freedom isKND=12kBT.{\displaystyle {\frac {K}{ND}}={\frac {1}{2}}k_{\text{B}}T.}

Therefore, the kinetic energy per kelvin of one mole of monatomicideal gas (D = 3) isK=D2kBNA=32R,{\displaystyle K={\frac {D}{2}}k_{\text{B}}N_{\text{A}}={\frac {3}{2}}R,}whereNA{\displaystyle N_{\text{A}}} is theAvogadro constant, andR is theideal gas constant.

Thus, the ratio of the kinetic energy to the absolute temperature of an ideal monatomic gas can be calculated easily:

  • per mole: 12.47 J/K
  • per molecule: 20.7 yJ/K = 129 μeV/K

Atstandard 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 onD and the total molecular energy. Quantumstatistical mechanics is needed to accurately compute these contributions.[36]

Collisions with container wall

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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[37] based on naive kinetic theory, and the results can be used for analyzingeffusive flow rates, which is useful in applications such as thegaseous diffusion method forisotope separation.

Assume that in the container, the number density (number per unit volume) isn=N/V{\displaystyle n=N/V} and that the particles obeyMaxwell's velocity distribution:fMaxwell(vx,vy,vz)dvxdvydvz=(m2πkBT)3/2emv22kBTdvxdvydvz{\displaystyle f_{\text{Maxwell}}(v_{x},v_{y},v_{z})\,dv_{x}\,dv_{y}\,dv_{z}=\left({\frac {m}{2\pi k_{\text{B}}T}}\right)^{3/2}e^{-{\frac {mv^{2}}{2k_{\text{B}}T}}}\,dv_{x}\,dv_{y}\,dv_{z}}

Then for a small areadA{\displaystyle dA} on the container wall, a particle with speedv{\displaystyle v} at angleθ{\displaystyle \theta } from the normal of the areadA{\displaystyle dA}, will collide with the area within time intervaldt{\displaystyle dt}, if it is within the distancevdt{\displaystyle v\,dt} from the areadA{\displaystyle dA}. Therefore, all the particles with speedv{\displaystyle v} at angleθ{\displaystyle \theta } from the normal that can reach areadA{\displaystyle dA} within time intervaldt{\displaystyle dt} are contained in the tilted pipe with a height ofvcos(θ)dt{\displaystyle v\cos(\theta )dt} and a volume ofvcos(θ)dAdt{\displaystyle v\cos(\theta )\,dA\,dt}.

The total number of particles that reach areadA{\displaystyle dA} within time intervaldt{\displaystyle dt} also depends on the velocity distribution; All in all, it calculates to be:nvcos(θ)dAdt×(m2πkBT)3/2emv22kBT(v2sin(θ)dvdθdϕ).{\displaystyle nv\cos(\theta )\,dA\,dt\times \left({\frac {m}{2\pi k_{\text{B}}T}}\right)^{3/2}e^{-{\frac {mv^{2}}{2k_{\text{B}}T}}}\left(v^{2}\sin(\theta )\,dv\,d\theta \,d\phi \right).}

Integrating this over all appropriate velocities within the constraintv>0{\displaystyle v>0},0<θ<π2{\textstyle 0<\theta <{\frac {\pi }{2}}},0<ϕ<2π{\displaystyle 0<\phi <2\pi } yields the number of atomic or molecular collisions with a wall of a container per unit area per unit time:Jcollision=0π/2cos(θ)sin(θ)dθ0πsin(θ)dθ×nv¯=14nv¯=n48kBTπm.{\displaystyle J_{\text{collision}}={\frac {\displaystyle \int _{0}^{\pi /2}\cos(\theta )\sin(\theta )\,d\theta }{\displaystyle \int _{0}^{\pi }\sin(\theta )\,d\theta }}\times n{\bar {v}}={\frac {1}{4}}n{\bar {v}}={\frac {n}{4}}{\sqrt {\frac {8k_{\mathrm {B} }T}{\pi m}}}.}

This quantity is also known as the "impingement rate" in vacuum physics. Note that to calculate the average speedv¯{\displaystyle {\bar {v}}} of the Maxwell's velocity distribution, one has to integrate overv>0{\displaystyle v>0},0<θ<π{\displaystyle 0<\theta <\pi },0<ϕ<2π{\displaystyle 0<\phi <2\pi }.

The momentum transfer to the container wall from particles hitting the areadA{\displaystyle dA} with speedv{\displaystyle v} at angleθ{\displaystyle \theta } from the normal, in time intervaldt{\displaystyle dt} is:[2mvcos(θ)]×nvcos(θ)dAdt×(m2πkBT)3/2emv22kBT(v2sin(θ)dvdθdϕ).{\displaystyle [2mv\cos(\theta )]\times nv\cos(\theta )\,dA\,dt\times \left({\frac {m}{2\pi k_{\text{B}}T}}\right)^{3/2}e^{-{\frac {mv^{2}}{2k_{\text{B}}T}}}\left(v^{2}\sin(\theta )\,dv\,d\theta \,d\phi \right).}Integrating this over all appropriate velocities within the constraintv>0{\displaystyle v>0},0<θ<π2{\textstyle 0<\theta <{\frac {\pi }{2}}},0<ϕ<2π{\displaystyle 0<\phi <2\pi } yields thepressure (consistent withIdeal gas law):P=20π/2cos2(θ)sin(θ)dθ0πsin(θ)dθ×nmvrms2=13nmvrms2=23nEkin=nkBT{\displaystyle P={\frac {\displaystyle 2\int _{0}^{\pi /2}\cos ^{2}(\theta )\sin(\theta )\,d\theta }{\displaystyle \int _{0}^{\pi }\sin(\theta )\,d\theta }}\times nmv_{\text{rms}}^{2}={\frac {1}{3}}nmv_{\text{rms}}^{2}={\frac {2}{3}}n\langle E_{\text{kin}}\rangle =nk_{\mathrm {B} }T}If this small areaA{\displaystyle A} is punched to become a small hole, theeffusive flow rate will be:Φeffusion=JcollisionA=nAkBT2πm.{\displaystyle \Phi _{\text{effusion}}=J_{\text{collision}}A=nA{\sqrt {\frac {k_{\mathrm {B} }T}{2\pi m}}}.}

Combined with theideal gas law, this yieldsΦeffusion=PA2πmkBT.{\displaystyle \Phi _{\text{effusion}}={\frac {PA}{\sqrt {2\pi mk_{\mathrm {B} }T}}}.}

The above expression is consistent withGraham's law.

To calculate the velocity distribution of particles hitting this small area, we must take into account that all the particles with(v,θ,ϕ){\displaystyle (v,\theta ,\phi )} that hit the areadA{\displaystyle dA} within the time intervaldt{\displaystyle dt} are contained in the tilted pipe with a height ofvcos(θ)dt{\displaystyle v\cos(\theta )\,dt} and a volume ofvcos(θ)dAdt{\displaystyle v\cos(\theta )\,dA\,dt}; Therefore, compared to the Maxwell distribution, the velocity distribution will have an extra factor ofvcosθ{\displaystyle v\cos \theta }:f(v,θ,ϕ)dvdθdϕ=λvcosθ(m2πkT)3/2emv22kBT(v2sinθdvdθdϕ){\displaystyle {\begin{aligned}f(v,\theta ,\phi )\,dv\,d\theta \,d\phi &=\lambda v\cos {\theta }\left({\frac {m}{2\pi kT}}\right)^{3/2}e^{-{\frac {mv^{2}}{2k_{\mathrm {B} }T}}}(v^{2}\sin {\theta }\,dv\,d\theta \,d\phi )\end{aligned}}}with the constraintv>0{\textstyle v>0},0<θ<π2{\textstyle 0<\theta <{\frac {\pi }{2}}},0<ϕ<2π{\displaystyle 0<\phi <2\pi }. The constantλ{\displaystyle \lambda } can be determined by the normalization conditionf(v,θ,ϕ)dvdθdϕ=1{\textstyle \int f(v,\theta ,\phi )\,dv\,d\theta \,d\phi =1} to be4/v¯{\textstyle 4/{\bar {v}}}, and overall:f(v,θ,ϕ)dvdθdϕ=12π(mkBT)2emv22kBT(v3sinθcosθdvdθdϕ);v>0,0<θ<π2,0<ϕ<2π{\displaystyle {\begin{aligned}f(v,\theta ,\phi )\,dv\,d\theta \,d\phi &={\frac {1}{2\pi }}\left({\frac {m}{k_{\mathrm {B} }T}}\right)^{2}e^{-{\frac {mv^{2}}{2k_{\mathrm {B} }T}}}(v^{3}\sin {\theta }\cos {\theta }\,dv\,d\theta \,d\phi )\\\end{aligned}};\quad v>0,\,0<\theta <{\frac {\pi }{2}},\,0<\phi <2\pi }

Speed of molecules

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From the kinetic energy formula it can be shown thatvp=2kBTm,{\displaystyle v_{\text{p}}={\sqrt {2\cdot {\frac {k_{\mathrm {B} }T}{m}}}},}v¯=2πvp=8πkBTm,{\displaystyle {\bar {v}}={\frac {2}{\sqrt {\pi }}}v_{p}={\sqrt {{\frac {8}{\pi }}\cdot {\frac {k_{\mathrm {B} }T}{m}}}},}vrms=32vp=3kBTm,{\displaystyle v_{\text{rms}}={\sqrt {\frac {3}{2}}}v_{p}={\sqrt {{3}\cdot {\frac {k_{\mathrm {B} }T}{m}}}},}wherev is in m/s,T is in kelvin, andm is the mass of one molecule of gas in kg. The most probable (or mode) speedvp{\displaystyle v_{\text{p}}} is 81.6% of the root-mean-square speedvrms{\displaystyle v_{\text{rms}}}, and the mean (arithmetic mean, or average) speedv¯{\displaystyle {\bar {v}}} is 92.1% of the rms speed (isotropicdistribution of speeds).

See:

Mean free path

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Main article:Mean free path

In kinetic theory of gases, themean free path is the average distance traveled by a molecule, or a number of molecules per volume, before they make their first collision. Letσ{\displaystyle \sigma } be the collisioncross section of one molecule colliding with another. As in the previous section, the number densityn{\displaystyle n} is defined as the number of molecules per (extensive) volume, orn=N/V{\displaystyle n=N/V}. The collision cross section per volume or collision cross section density isnσ{\displaystyle n\sigma }, and it is related to the mean free path{\displaystyle \ell } by=1nσ2{\displaystyle \ell ={\frac {1}{n\sigma {\sqrt {2}}}}}

Notice that the unit of the collision cross section per volumenσ{\displaystyle n\sigma } is reciprocal of length.

Transport properties

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See also:Transport phenomena

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 asviscosity,thermal conductivity,mass diffusivity andthermal 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 byE. G. D. Cohen,J. M. Kincaid andM. Lòpez de Haro,[38][39][40][41] building on work byH. van Beijeren andM. H. Ernst.[42]

Viscosity and kinetic momentum

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See also:Viscosity § Momentum transport

In books on elementary kinetic theory[43] 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 aCouette 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 forceF. 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 componentu{\displaystyle u} which increase uniformly with distancey{\displaystyle y} above the lower plate. The non-equilibrium flow is superimposed on aMaxwell-Boltzmann equilibrium distribution of molecular motions.

Inside a dilute gas in aCouette flow setup, letu0{\displaystyle u_{0}} be the forward velocity of the gas at a horizontal flat layer (labeled asy=0{\displaystyle y=0});u0{\displaystyle u_{0}} is along the horizontal direction. The number of molecules arriving at the areadA{\displaystyle dA} on one side of the gas layer, with speedv{\displaystyle v} at angleθ{\displaystyle \theta } from the normal, in time intervaldt{\displaystyle dt} isnvcos(θ)dAdt×(m2πkBT)3/2emv22kBT(v2sinθdvdθdϕ){\displaystyle nv\cos({\theta })\,dA\,dt\times \left({\frac {m}{2\pi k_{\mathrm {B} }T}}\right)^{3/2}\,e^{-{\frac {mv^{2}}{2k_{\mathrm {B} }T}}}(v^{2}\sin {\theta }\,dv\,d\theta \,d\phi )}

These molecules made their last collision aty=±cosθ{\displaystyle y=\pm \ell \cos \theta }, where{\displaystyle \ell } is themean free path. Each molecule will contribute a forward momentum ofpx±=m(u0±cosθdudy),{\displaystyle p_{x}^{\pm }=m\left(u_{0}\pm \ell \cos \theta {\frac {du}{dy}}\right),}where plus sign applies to molecules from above, and minus sign below. Note that the forward velocity gradientdu/dy{\displaystyle du/dy} can be considered to be constant over a distance of mean free path.

Integrating over all appropriate velocities within the constraintv>0{\displaystyle v>0},0<θ<π2{\textstyle 0<\theta <{\frac {\pi }{2}}},0<ϕ<2π{\displaystyle 0<\phi <2\pi } yields the forward momentum transfer per unit time per unit area (also known asshear stress):τ±=14v¯nm(u0±23dudy){\displaystyle \tau ^{\pm }={\frac {1}{4}}{\bar {v}}n\cdot m\left(u_{0}\pm {\frac {2}{3}}\ell {\frac {du}{dy}}\right)}

The net rate of momentum per unit area that is transported across the imaginary surface is thusτ=τ+τ=13v¯nmdudy{\displaystyle \tau =\tau ^{+}-\tau ^{-}={\frac {1}{3}}{\bar {v}}nm\cdot \ell {\frac {du}{dy}}}

Combining the above kinetic equation withNewton's law of viscosityτ=ηdudy{\displaystyle \tau =\eta {\frac {du}{dy}}}gives the equation for shear viscosity, which is usually denotedη0{\displaystyle \eta _{0}} when it is a dilute gas:η0=13v¯nm{\displaystyle \eta _{0}={\frac {1}{3}}{\bar {v}}nm\ell }

Combining this equation with the equation for mean free path givesη0=132mv¯σ{\displaystyle \eta _{0}={\frac {1}{3{\sqrt {2}}}}{\frac {m{\bar {v}}}{\sigma }}}

Maxwell-Boltzmann distribution gives the average (equilibrium) molecular speed asv¯=2πvp=22πkBTm{\displaystyle {\bar {v}}={\frac {2}{\sqrt {\pi }}}v_{p}=2{\sqrt {{\frac {2}{\pi }}{\frac {k_{\mathrm {B} }T}{m}}}}}wherevp{\displaystyle v_{p}} is the most probable speed. We note thatkBNA=RandM=mNA{\displaystyle k_{\text{B}}N_{\text{A}}=R\quad {\text{and}}\quad M=mN_{\text{A}}}

and insert the velocity in the viscosity equation above. This gives the well known equation[44] (withσ{\displaystyle \sigma } subsequently estimated below) forshear viscosity for dilute gases:η0=23πmkBTσ=23πMRTσNA{\displaystyle \eta _{0}={\frac {2}{3{\sqrt {\pi }}}}\cdot {\frac {\sqrt {mk_{\mathrm {B} }T}}{\sigma }}={\frac {2}{3{\sqrt {\pi }}}}\cdot {\frac {\sqrt {MRT}}{\sigma N_{\text{A}}}}}andM{\displaystyle M} is themolar 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 inRevised 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 byσ=π(2r)2=πd2{\displaystyle \sigma =\pi \left(2r\right)^{2}=\pi d^{2}}

The radiusr{\displaystyle r} is called collision cross section radius or kinetic radius, and the diameterd{\displaystyle d} is called collision cross section diameter orkinetic diameter of a molecule in a monomolecular gas. There are no simple general relation between the collisioncross 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 theLennard-Jones potential orMorse 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 requiredcollision integrals.

The expression for viscosity obtained fromRevised Enskog Theory reduces to the above expression in the limit of infinite dilution, and can be written asη=(1+αη)η0+ηc{\displaystyle \eta =(1+\alpha _{\eta })\eta _{0}+\eta _{c}}whereαη{\displaystyle \alpha _{\eta }} is a term that tends to zero in the limit of infinite dilution that accounts for excluded volume, andηc{\displaystyle \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

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See also:Thermal conductivity

Following a similar logic as above, one can derive the kinetic model forthermal conductivity[43] 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 asthermal reservoirs. The upper plate has a higher temperature than the lower plate. The molecules in the gas layer have a molecular kinetic energyε{\displaystyle \varepsilon } which increases uniformly with distancey{\displaystyle y} above the lower plate. The non-equilibrium energy flow is superimposed on aMaxwell-Boltzmann equilibrium distribution of molecular motions.

Letε0{\displaystyle \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 areadA{\displaystyle dA} on one side of the gas layer, with speedv{\displaystyle v} at angleθ{\displaystyle \theta } from the normal, in time intervaldt{\displaystyle dt} isnvcos(θ)dAdt×(m2πkBT)3/2emv22kBT(v2sin(θ)dvdθdϕ){\displaystyle nv\cos(\theta )\,dA\,dt\times \left({\frac {m}{2\pi k_{\mathrm {B} }T}}\right)^{3/2}e^{-{\frac {mv^{2}}{2k_{\text{B}}T}}}(v^{2}\sin(\theta )\,dv\,d\theta \,d\phi )}

These molecules made their last collision at a distancecosθ{\displaystyle \ell \cos \theta } above and below the gas layer, and each will contribute a molecular kinetic energy ofε±=(ε0±mcvcosθdTdy),{\displaystyle \varepsilon ^{\pm }=\left(\varepsilon _{0}\pm mc_{v}\ell \cos \theta \,{\frac {dT}{dy}}\right),}wherecv{\displaystyle c_{v}} is thespecific heat capacity. Again, plus sign applies to molecules from above, and minus sign below. Note that the temperature gradientdT/dy{\displaystyle dT/dy} can be considered to be constant over a distance of mean free path.

Integrating over all appropriate velocities within the constraintv>0{\displaystyle v>0},0<θ<π2{\textstyle 0<\theta <{\frac {\pi }{2}}},0<ϕ<2π{\displaystyle 0<\phi <2\pi } yields the energy transfer per unit time per unit area (also known asheat flux):qy±=14v¯n(ε0±23mcvdTdy){\displaystyle q_{y}^{\pm }=-{\frac {1}{4}}{\bar {v}}n\cdot \left(\varepsilon _{0}\pm {\frac {2}{3}}mc_{v}\ell {\frac {dT}{dy}}\right)}

Note that the energy transfer from above is in they{\displaystyle -y} direction, and therefore the overall minus sign in the equation. The net heat flux across the imaginary surface is thusq=qy+qy=13v¯nmcvdTdy{\displaystyle q=q_{y}^{+}-q_{y}^{-}=-{\frac {1}{3}}{\bar {v}}nmc_{v}\ell \,{\frac {dT}{dy}}}

Combining the above kinetic equation withFourier's lawq=κdTdy{\displaystyle q=-\kappa \,{\frac {dT}{dy}}}gives the equation for thermal conductivity, which is usually denotedκ0{\displaystyle \kappa _{0}} when it is a dilute gas:κ0=13v¯nmcv{\displaystyle \kappa _{0}={\frac {1}{3}}{\bar {v}}nmc_{v}\ell }

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 asκ=ακκ0+κc{\displaystyle \kappa =\alpha _{\kappa }\kappa _{0}+\kappa _{c}}whereακ{\displaystyle \alpha _{\kappa }} is a term that tends to unity in the limit of infinite dilution, accounting for excluded volume, andκc{\displaystyle \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

[edit]
See also:Fick's laws of diffusion

Following a similar logic as above, one can derive the kinetic model formass diffusivity[43] of a dilute gas:

Consider asteady 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 uniformnumber 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 densityn{\displaystyle n} in the layer increases uniformly with distancey{\displaystyle y} above the lower plate. The non-equilibrium molecular flow is superimposed on aMaxwell–Boltzmann equilibrium distribution of molecular motions.

Letn0{\displaystyle n_{0}} be the number density of the gas at an imaginary horizontal surface inside the layer. The number of molecules arriving at an areadA{\displaystyle dA} on one side of the gas layer, with speedv{\displaystyle v} at angleθ{\displaystyle \theta } from the normal, in time intervaldt{\displaystyle dt} isnvcos(θ)dAdt×(m2πkBT)3/2emv22kBT(v2sin(θ)dvdθdϕ){\displaystyle nv\cos(\theta )\,dA\,dt\times \left({\frac {m}{2\pi k_{\mathrm {B} }T}}\right)^{3/2}e^{-{\frac {mv^{2}}{2k_{\text{B}}T}}}(v^{2}\sin(\theta )\,dv\,d\theta \,d\phi )}

These molecules made their last collision at a distancecosθ{\displaystyle \ell \cos \theta } above and below the gas layer, where the local number density isn±=(n0±cosθdndy){\displaystyle n^{\pm }=\left(n_{0}\pm \ell \cos \theta \,{\frac {dn}{dy}}\right)}

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

Integrating over all appropriate velocities within the constraintv>0{\displaystyle v>0},0<θ<π2{\textstyle 0<\theta <{\frac {\pi }{2}}},0<ϕ<2π{\displaystyle 0<\phi <2\pi } yields the molecular transfer per unit time per unit area (also known asdiffusion flux):Jy±=14v¯(n0±23dndy){\displaystyle J_{y}^{\pm }=-{\frac {1}{4}}{\bar {v}}\cdot \left(n_{0}\pm {\frac {2}{3}}\ell \,{\frac {dn}{dy}}\right)}

Note that the molecular transfer from above is in they{\displaystyle -y} direction, and therefore the overall minus sign in the equation. The net diffusion flux across the imaginary surface is thusJ=Jy+Jy=13v¯dndy{\displaystyle J=J_{y}^{+}-J_{y}^{-}=-{\frac {1}{3}}{\bar {v}}\ell {\frac {dn}{dy}}}

Combining the above kinetic equation withFick's first law of diffusionJ=Ddndy{\displaystyle J=-D{\frac {dn}{dy}}}gives the equation for mass diffusivity, which is usually denotedD0{\displaystyle D_{0}} when it is a dilute gas:D0=13v¯{\displaystyle D_{0}={\frac {1}{3}}{\bar {v}}\ell }

The corresponding expression obtained fromRevised Enskog Theory may be written asD=αDD0{\displaystyle D=\alpha _{D}D_{0}}whereαD{\displaystyle \alpha _{D}} is a factor that tends to unity in the limit of infinite dilution, which accounts for excluded volume and the variationchemical potentials with density.

Detailed balance

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Fluctuation and dissipation

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Main article:Fluctuation-dissipation theorem

The kinetic theory of gases entails that due to themicroscopic reversibility of the gas particles' detailed dynamics, the system must obey the principle ofdetailed balance. Specifically, thefluctuation-dissipation theorem applies to theBrownian motion (ordiffusion) and thedrag force, which leads to theEinstein–Smoluchowski equation:[45]D=μkBT,{\displaystyle D=\mu \,k_{\text{B}}T,} where

Note that the mobilityμ =vd/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.

Onsager reciprocal relations

[edit]
Main article: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 theOnsager reciprocal relations (i.e. the detailed balance of thereversible dynamics of the particles), when applied to theconvection (matter flow due to temperature gradient, and heat flow due to pressure gradient) andadvection (matter flow due to the velocity of particles, and momentum transfer due to pressure gradient) of the ideal (dilute) gas.

See also

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Statistical mechanics

References

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Citations

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  2. ^Bacon, F. (1902) [1620]. Dewey, J. (ed.).Novum Organum: Or True Suggestions for the Interpretation of Nature. P. F. Collier & son. p. 153.
  3. ^Bacon, F. (1902) [1620]. Dewey, J. (ed.).Novum Organum: Or True Suggestions for the Interpretation of Nature. P. F. Collier & son. p. 156.
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  7. ^Hooke, Robert (1665).Micrographia: Or Some Physiological Descriptions of Minute Bodies Made by Magnifying Glasses with Observations and Inquiries Thereupon. Printed by Jo. Martyn, and Ja. Allestry, Printers to the Royal Society. p. 12. (Machine-readable, no pagination){{cite book}}: CS1 maint: postscript (link)
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  14. ^Lomonosov, Mikhail Vasil'evich (1970) [1750]."Meditations on the Cause of Heat and Cold". In Leicester, Henry M. (ed.).Mikhail Vasil'evich Lomonosov on the Corpuscular Theory. Harvard University Press. pp. 102–3.
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  23. ^See:
  24. ^Mahon, Basil (2003).The Man Who Changed Everything – the Life of James Clerk Maxwell. Hoboken, NJ: Wiley.ISBN 0-470-86171-1.OCLC 52358254.
  25. ^Gyenis, Balazs (2017). "Maxwell and the normal distribution: A colored story of probability, independence, and tendency towards equilibrium".Studies in History and Philosophy of Modern Physics.57:53–65.arXiv:1702.01411.Bibcode:2017SHPMP..57...53G.doi:10.1016/j.shpsb.2017.01.001.S2CID 38272381.
  26. ^Maxwell 1873
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  28. ^Smoluchowski 1906
  29. ^Chang, Raymond; Thoman, John W. Jr. (2014).Physical Chemistry for the Chemical Sciences. New York, NY: University Science Books. p. 37.
  30. ^van Enk, Steven J.; Nienhuis, Gerard (1991-12-01)."Inelastic collisions and gas-kinetic effects of light".Physical Review A.44 (11):7615–7625.Bibcode:1991PhRvA..44.7615V.doi:10.1103/PhysRevA.44.7615.PMID 9905900.
  31. ^McQuarrie, Donald A. (1976).Statistical Mechanics. New York, NY: University Science Press.
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  33. ^Fedosin, Sergey G. (2021). "The potentials of the acceleration field and pressure field in rotating relativistic uniform system".Continuum Mechanics and Thermodynamics.33 (3):817–834.arXiv:2410.17289.Bibcode:2021CMT....33..817F.doi:10.1007/s00161-020-00960-7.S2CID 230076346.
  34. ^The average kinetic energy of a fluid is proportional to theroot mean-square velocity, which always exceeds the mean velocity -Kinetic Molecular Theory[usurped]
  35. ^Configuration integral (statistical mechanics)Archived 2012-04-28 at theWayback Machine
  36. ^Chang, Raymond; Thoman, John W. Jr. (2014).Physical Chemistry for the Chemical Sciences. New York: University Science Books. pp. 56–61.
  37. ^"5.62 Physical Chemistry II"(PDF).MIT OpenCourseWare.
  38. ^Lòpez de Haro, M.; Cohen, E. G. D.; Kincaid, J. M. (1983)."The Enskog theory for multicomponent mixtures. I. Linear transport theory".The Journal of Chemical Physics.78 (5):2746–2759.Bibcode:1983JChPh..78.2746L.doi:10.1063/1.444985.
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  40. ^Lòpez de Haro, M.; Cohen, E. G. D. (1984)."The Enskog theory for multicomponent mixtures. III. Transport properties of dense binary mixtures with one tracer component".The Journal of Chemical Physics.80 (1):408–415.Bibcode:1984JChPh..80..408L.doi:10.1063/1.446463.
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Sources cited

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Further reading

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