Editing Joule–Thomson effect

{{Short description|Phenomenon of non-ideal fluids changing temperature while being forced through small spaces}}
{{redirect|Throttling process|the concept in computing|rate limiting}}
{{Use dmy dates|date=October 2014}}
In [[thermodynamics]], the '''Joule–Thomson effect''' (also known as the '''Joule–Kelvin effect''' or '''Kelvin–Joule effect''') describes the temperature change of a [[Real gas|''real'' gas]] or [[liquid]] (as differentiated from an [[ideal gas]]) when it is expanding; typically caused by the pressure loss from flow through a [[expansion valve (steam engine)|valve]] or [[enthalpy#Throttling|porous plug]] while keeping it insulated so that [[Adiabatic process|no heat is exchanged]] with the environment.<ref name=Perry>
{{cite book
|author=R. H. Perry and D. W. Green
|title=Perry's Chemical Engineers' Handbook
|publisher=McGraw-Hill
|year=1984
|isbn=978-0-07-049479-4
|url-access=registration
|url=https://archive.org/details/perryschemicalen04newy
}}</ref><ref name=Roy>
{{cite book
|author=B. N. Roy
|title=Fundamentals of Classical and Statistical Thermodynamics
|publisher=John Wiley & Sons
|year=2002
|isbn=978-0-470-84313-0
|bibcode=2002fcst.book.....N
}}</ref><ref name=Edmister>
{{cite book
|author=W. C. Edmister, B. I. Lee
|title=Applied Hydrocarbon Thermodynamics
|edition=2nd
|volume=1
|publisher=Gulf Publishing
|year=1984
|isbn=978-0-87201-855-6
}}</ref> This procedure is called a ''throttling process'' or ''Joule–Thomson process''.<ref>
{{cite book
|author=F. Reif
|title=Fundamentals of Statistical and Thermal Physics
|chapter=Chapter 5 – Simple applications of macroscopic thermodynamics
|publisher=McGraw-Hill
|year=1965
|isbn=978-0-07-051800-1
|chapter-url=https://archive.org/details/fundamentalsofst00fred
}}</ref> The effect is purely due to deviation from ideality, as any ideal gas has no JT effect.

At room temperature, all gases except [[hydrogen]], [[helium]], and [[neon]] cool upon expansion by the Joule–Thomson process when being [[throttle]]d through an orifice; these three gases rise in temperature when forced through a porous plug at room temperature, but lowers in temperature when already at lower temperatures.<ref>
{{cite book
|author=A. W. Adamson
|title=A Textbook of Physical Chemistry
|edition=1st
|chapter=Chapter 4 – Chemical thermodynamics. The First Law of Thermodynamics|publisher=Academic Press
|year=1973
|lccn=72088328
}}</ref><ref>
{{cite book
|author=G. W. Castellan
|title=Physical Chemistry
|edition=2nd
|chapter=Chapter 7 – Energy and the First Law of Thermodynamics; Thermochemistry
|publisher=Addison-Wesley
|year=1971
|isbn=978-0-201-00912-5
|chapter-url=https://archive.org/details/physicalchemistr00cast
|url-access=registration
|url=https://archive.org/details/physicalchemistr00cast
}}</ref> Most liquids such as [[Hydraulics|hydraulic]] oils will be warmed by the Joule–Thomson throttling process. The temperature at which the JT effect switches sign is the [[inversion temperature]].

The gas-cooling throttling process is commonly exploited in [[Refrigeration|refrigeration processes]] such as [[Liquefied gas|liquefiers]] in [[air separation]] industrial process.<ref>{{cite book|last1=Moran|first1=M.J.|last2=Shapiro|first2=H.N.|title=Fundamentals of Engineering Thermodynamics|edition=5th|date=2006|publisher=John Wiley & Sons}}</ref><ref name="Basics of Joule–Thomson Liquefactio">{{cite journal|doi=10.1007/s10909-016-1733-3|title=Basics of Joule–Thomson Liquefaction and JT Cooling|journal=Journal of Low Temperature Physics|volume=186|issue=5–6|pages=385–403|year=2017|last1=De Waele|first1=A. T. A. M.|bibcode=2017JLTP..186..385D|doi-access=free}}</ref> In hydraulics, the warming effect from Joule–Thomson throttling can be used to find internally leaking valves as these will produce heat which can be detected by [[thermocouple]] or [[Thermal Imaging camera|thermal-imaging camera]]. Throttling is a fundamentally [[irreversible process]]. The throttling due to the flow resistance in supply lines, heat exchangers, regenerators, and other components of (thermal) machines is a source of losses that limits their performance.

Since it is a constant-enthalpy process, it can be used to experimentally measure the lines of constant enthalpy (isenthalps) on the <math>(p, T)</math> diagram of a gas. Combined with the [[Specific heat capacity|specific heat capacity ''at constant pressure'']] <math>c_P = (\partial h / \partial T)_P</math> it allows the complete measurement of the [[thermodynamic potential]] for the gas.<ref name=":0" />

==History==
The effect is named after [[James Prescott Joule]] and [[William Thomson, 1st Baron Kelvin]], who discovered it in 1852. It followed upon earlier work by Joule on [[Joule expansion]], in which a gas undergoes free expansion in a [[vacuum]] and the temperature is unchanged, if the gas is [[ideal gas|ideal]].

==Description==
The ''[[adiabatic process|adiabatic]]'' (no heat exchanged) expansion of a gas may be carried out in a number of ways. The change in temperature experienced by the gas during expansion depends not only on the initial and final pressure, but also on the manner in which the expansion is carried out.

*If the expansion process is [[reversible process (thermodynamics)|reversible]], meaning that the gas is in [[thermodynamic equilibrium]] at all times, it is called an ''[[isentropic]]'' expansion. In this scenario, the gas does positive [[mechanical work|work]] during the expansion, and its temperature decreases.
*In a [[Joule expansion|free expansion]], on the other hand, the gas does no work and absorbs no heat, so the [[internal energy]] is conserved. Expanded in this manner, the temperature of an [[ideal gas]] would remain constant, but the temperature of a real gas decreases, except at very high temperature.<ref name=":Goussard">{{cite journal|doi=10.1119/1.17417|title=Free expansion for real gases|journal=American Journal of Physics|volume=61|issue=9|pages=845–848|year=1993|last1=Goussard|first1=Jacques-Olivier|last2=Roulet|first2=Bernard|bibcode=1993AmJPh..61..845G}}</ref>
*The method of expansion discussed in this article, in which a gas or liquid at pressure ''P''<sub>1</sub> flows into a region of lower pressure ''P''<sub>2</sub> without significant change in kinetic energy, is called the Joule–Thomson expansion. The expansion is inherently irreversible. During this expansion, [[enthalpy]] remains unchanged (see [[#Proof that the specific enthalpy remains constant|proof]] below). Unlike a free expansion, work is done, causing a change in internal energy. Whether the internal energy increases or decreases is determined by whether work is done on or by the fluid; that is determined by the initial and final states of the expansion and the properties of the fluid.

[[File:Joule-Thomson sign.png|thumb|Sign of the Joule–Thomson coefficient, <math>\mu_{\mathrm{JT}}</math> for N<sub>2</sub>. Within the region bounded by the red line, a Joule–Thomson expansion produces cooling (<math>\mu_{\mathrm{JT}} > 0 </math>); outside that region, the expansion produces heating. The gas–liquid coexistence curve is shown by the blue line, terminating at the critical point (the solid blue circle). The dashed lines demarcate the region where N<sub>2</sub> is a supercritical fluid (where properties smoothly transition between liquid-like and gas-like).]]
The temperature change produced during a Joule–Thomson expansion is quantified by the [[#The Joule–Thomson (Kelvin) coefficient|Joule–Thomson coefficient]], <math>\mu_{\mathrm{JT}}</math>. This  coefficient may be either positive (corresponding to cooling) or negative (heating); the regions where each occurs for molecular nitrogen, N<sub>2</sub>, are shown in the figure. Note that most conditions in the figure correspond to N<sub>2</sub> being a [[supercritical fluid]], where it has some properties of a gas and some of a liquid, but can not be really described as being either. The coefficient is negative at both very high and very low temperatures; at very high pressure it is negative at all temperatures. The maximum [[inversion temperature]] (621 K for N<sub>2</sub><ref name=":Atkins1">{{cite book|last=Atkins|first=Peter|date=1997|title=Physical Chemistry|edition=6th|location=New York|publisher=W.H. Freeman and Co.|page=[https://archive.org/details/physicalchemistr00atki/page/930 930]|isbn=978-0-7167-2871-9|url=https://archive.org/details/physicalchemistr00atki/page/930}}</ref>) occurs as zero pressure is approached. For N<sub>2</sub> gas at low pressures, <math>\mu_{\mathrm{JT}}</math> is negative at high temperatures and positive at low temperatures. At temperatures below the gas-liquid [[binodal|coexistence curve]], N<sub>2</sub> condenses to form a liquid and the coefficient again becomes negative. Thus, for N<sub>2</sub> gas below 621 K, a Joule–Thomson expansion can be used to cool the gas until liquid N<sub>2</sub> forms.

==Physical mechanism==

There are two factors that can change the temperature of a fluid during an adiabatic expansion: a change in internal energy or the conversion between potential and kinetic internal energy. [[Thermodynamic temperature|Temperature]] is the measure of thermal kinetic energy (energy associated with molecular motion); so a change in temperature indicates a change in thermal kinetic energy. The [[internal energy#Description and definition|internal energy]] is the sum of thermal kinetic energy and thermal potential energy.<ref name=":Rock">{{cite book|last=Rock|first=P. A.|date=1983|title=Chemical Thermodynamics|at=sec. 3-2|publisher=University Science Books|location=Mill Valley, CA|isbn=978-0-935702-12-5}}</ref> Thus, even if the internal energy does not change, the temperature can change due to conversion between kinetic and potential energy; this is what happens in a free expansion and typically produces a decrease in temperature as the fluid expands.<ref name=":Pippard">Pippard, A. B. (1957). "Elements of Classical Thermodynamics", p. 73. Cambridge University Press, Cambridge, U.K.</ref><ref>Tabor, D. (1991). ''Gases, liquids and solids'', p. 148. Cambridge University Press, Cambridge, U.K. {{ISBN|0 521 40667 6}}.</ref> If work is done on or by the fluid as it expands, then the total internal energy changes. This is what happens in a Joule–Thomson expansion and can produce larger heating or cooling than observed in a free expansion.

In a Joule–Thomson expansion the enthalpy remains constant. The enthalpy, <math>H</math>, is defined as
:<math>H = U + PV</math>
where <math>U</math> is internal energy, <math>P</math> is pressure, and <math>V</math> is volume. Under the conditions of a Joule–Thomson expansion, the change in <math>PV</math> represents the work done by the fluid (see the [[#Proof that the specific enthalpy remains constant|proof]] below). If <math>PV</math> increases, with <math>H</math> constant, then <math>U</math> must decrease as a result of the fluid doing work on its surroundings. This produces a decrease in temperature and results in a positive Joule–Thomson coefficient. Conversely, a decrease in <math>PV</math> means that work is done on the fluid and the internal energy increases. If the increase in kinetic energy exceeds the increase in potential energy, there will be an increase in the temperature of the fluid and the Joule–Thomson coefficient will be negative.

For an ideal gas, <math>PV</math> does not change during a Joule–Thomson expansion.<ref>Klotz, I.M. and R. M. Rosenberg (1991). ''Chemical Thermodynamics'', p. 83. Benjamin, Meno Park, California.</ref> As a result, there is no change in internal energy; since there is also no change in thermal potential energy, there can be no change in thermal kinetic energy and, therefore, no change in temperature. In real gases, <math>PV</math> does change.

The ratio of the value of <math>PV</math> to that expected for an ideal gas at the same temperature is called the [[compressibility factor]], <math>Z</math>. For a gas, this is typically less than unity at low temperature and greater than unity at high temperature (see the discussion in [[compressibility factor#Physical mechanism of temperature and pressure dependence|compressibility factor]]). At low pressure, the value of <math>Z</math> always moves towards unity as a gas expands.<ref name=":Atkins2">Atkins, Peter (1997). ''Physical Chemistry'' (6th ed.). New York: W.H. Freeman and Co. pp. 31–32. {{ISBN|0-7167-2871-0}}.</ref> Thus at low temperature, <math>Z</math> and <math>PV</math> will increase as the gas expands, resulting in a positive Joule–Thomson coefficient. At high temperature, <math>Z</math> and <math>PV</math> decrease as the gas expands; if the decrease is large enough, the Joule–Thomson coefficient will be negative.

For liquids, and for supercritical fluids under high pressure, <math>PV</math> increases as pressure increases.<ref name=":Atkins2"/> This is due to molecules being forced together, so that the volume can barely decrease due to higher pressure. Under such conditions, the Joule–Thomson coefficient is negative, as seen in the figure [[#Description|above]].

The physical mechanism associated with the Joule–Thomson effect is closely related to that of a [[shock wave]],<ref>{{cite journal|doi=10.1103/PhysRevLett.112.144504|pmid=24765974|title=Shock-Wave Compression and Joule–Thomson Expansion|journal=Physical Review Letters|volume=112|issue=14|pages=144504|year=2014|last1=Hoover|first1=Wm. G.|last2=Hoover|first2=Carol G.|last3=Travis|first3=Karl P.|bibcode=2014PhRvL.112n4504H|arxiv=1311.1717|s2cid=33580985}}</ref> although a shock wave differs in that the change in bulk kinetic energy of the gas flow is not negligible.

==The Joule–Thomson (Kelvin) coefficient==
[[File:Joule-Thomson curves 2.svg|thumb|400px|Fig. 1 – Joule–Thomson coefficients for various gases at atmospheric pressure]]

The rate of change of temperature <math>T</math> with respect to pressure <math>P</math> in a Joule–Thomson process (that is, at constant enthalpy <math>H</math>) is the ''Joule–Thomson (Kelvin) coefficient'' <math>\mu_{\mathrm{JT}}</math>. This coefficient can be expressed in terms of the gas's specific volume <math>V</math>, its [[specific heat capacity#Heat capacity of compressible bodies|heat capacity at constant pressure]] <math>C_{\mathrm{p}}</math>, and its [[coefficient of thermal expansion]] <math>\alpha</math> as:<ref name=Perry/><ref name=Edmister/><ref>{{cite web|url=http://www.chem.arizona.edu/~salzmanr/480a/480ants/jadjte/jadjte.html|title=Joule Expansion|author=W.R. Salzman|publisher=Department of Chemistry, [[University of Arizona]]|access-date=23 July 2005|archive-url=https://web.archive.org/web/20120613235628/http://www.chem.arizona.edu/~salzmanr/480a/480ants/jadjte/jadjte.html|archive-date=13 June 2012|url-status=dead}}</ref>
:<math>\mu_{\mathrm{JT}} = \left( {\partial T \over \partial P} \right)_H = \frac V {C_{\mathrm{p}}}(\alpha T - 1)\,</math>

See the {{section link||Derivation of the Joule–Thomson coefficient}} below for the proof of this relation. The value of <math>\mu_{\mathrm{JT}}</math> is typically expressed in °C/[[bar (unit)|bar]] (SI units: [[kelvin|K]]/[[pascal (unit)|Pa]]) and depends on the type of gas and on the temperature and pressure of the gas before expansion. Its pressure dependence is usually only a few percent for pressures up to 100 bar.

All real gases have an ''inversion point'' at which the value of <math>\mu_{\mathrm{JT}}</math> changes sign. The temperature of this point, the ''Joule–Thomson inversion temperature'', depends on the pressure of the gas before expansion.

In a gas expansion the pressure decreases, so the sign of <math>\partial P</math> is negative by definition. With that in mind, the following table explains when the Joule–Thomson effect cools or warms a real gas:

{| class="wikitable" style="text-align:center;"
! If the gas temperature is
! then <math>\mu_\text{JT}</math> is
! since <math>\partial P</math> is
! thus <math>\partial T</math> must be
! so the gas
|-
| below the inversion temperature
| positive
| rowspan=2 | always negative
| negative
| cools
|-
| above the inversion temperature
| negative
| positive
| warms
|}

[[Helium]] and [[hydrogen]] are two gases whose Joule–Thomson inversion temperatures at a pressure of one [[atmosphere (unit)|atmosphere]] are very low (e.g., about 40 K, −233&nbsp;°C for helium). Thus, helium and hydrogen warm when expanded at constant enthalpy at typical room temperatures. On the other hand, [[nitrogen]] and [[oxygen]], the two most abundant gases in air, have inversion temperatures of 621 K (348&nbsp;°C) and 764 K (491&nbsp;°C) respectively: these gases can be cooled from room temperature by the Joule–Thomson effect.<ref name=Perry/><ref name=":Atkins1" />

For an ideal gas, <math>\mu_\text{JT}</math> is always equal to zero: ideal gases neither warm nor cool upon being expanded at constant enthalpy.

=== Theoretical models ===
[[File:Dieterici gas inversion temperature plot.png|thumb|For the Dieterici gas, the relation between reduced pressure and reduced inversion temperature is <math>\tilde p = (8-\tilde T_I) e^{\frac 52 - \frac 4{8-\tilde T_I}}</math>. Reproduced from Fig. 17 of <ref name=":0" />.]]
For a [[Van der Waals equation|Van der Waals gas]], the coefficient is<ref>{{Cite web |date=2017-01-25 |title=10.3: The Joule-Thomson Experiment |url=https://phys.libretexts.org/Bookshelves/Thermodynamics_and_Statistical_Mechanics/Book%3A_Heat_and_Thermodynamics_(Tatum)/10%3A_The_Joule_and_Joule-Thomson_Experiments/10.03%3A_The_Joule-Thomson_Experiment |access-date=2023-07-05 |website=Physics LibreTexts |language=en}}</ref><math display="block">\mu_\text{JT}=-\frac{V_m}{C_{p}} \frac{R T V_m^{2} b-2 a(V_m-b)^{2}}{R T V_m^{3}-2 a(V_m-b)^{2}}.</math>with inversion temperature <math>\frac{2a}{bR}\left(1 - \frac{b}{V_m}\right)^2</math>.


For the [[Real gas#Dieterici model|Dieterici gas]], the reduced inversion temperature is <math>\tilde T_I = 8 - 4/\tilde V_m</math>, and the relation between reduced pressure and reduced inversion temperature is <math>\tilde p = (8-\tilde T_I) e^{\frac 52 - \frac 4{8-\tilde T_I}}</math>. This is plotted on the right. The critical point falls inside the region where the gas cools on expansion. The outside region is where the gas warms on expansion.<ref name=":0">{{Cite book |last=Pippard |first=Alfred B. |title=Elements of classical thermodynamics: for advanced students of physics |date=1981 |publisher=Univ. Pr |isbn=978-0-521-09101-5 |edition=Repr |location=Cambridge |pages=74–77}}</ref>

==Applications==

In practice, the Joule–Thomson effect is achieved by allowing the gas to expand through a [[throttle|throttling device]] (usually a [[valve]]) which must be very well insulated to prevent any heat transfer to or from the gas. No external work is extracted from the gas during the expansion (the gas must not be expanded through a [[turbine]], for example).

The cooling produced in the Joule–Thomson expansion makes it a valuable tool in [[refrigeration]].<ref name="Basics of Joule–Thomson Liquefactio"/><ref>Keenan, J.H. (1970). ''Thermodynamics'', Chapter 15. M.I.T. Press, Cambridge, Massachusetts.</ref> The effect is applied in the [[Hampson–Linde cycle|Linde technique]] as a standard process in the [[petrochemical industry]], where the cooling effect is used to [[liquefaction of gases|liquefy gases]], and in many [[cryogenic]] applications (e.g. for the production of liquid oxygen, nitrogen, and [[argon]]). A gas must be below its inversion temperature to be liquefied by the Linde cycle. For this reason, simple Linde cycle liquefiers, starting from ambient temperature, cannot be used to liquefy helium, hydrogen, or [[neon]]. They must first be cooled to their inversion temperatures, which are −233&nbsp;°C (helium), −71&nbsp;°C (hydrogen), and −42&nbsp;°C (neon).<ref name=":Atkins1"/>

==Proof that the specific enthalpy remains constant==
{{sister project|project=Wikiversity
|text=[[v:Engineering thermodynamics/Joule-Thomson effect|Wikiversity analyzes this proof in more detail]]}}
In thermodynamics so-called "specific" quantities are quantities per unit mass (kg) and are denoted by lower-case characters. So ''h'', ''u'', and ''v'' are the [[enthalpy#Specific enthalpy|specific enthalpy]], specific internal energy, and specific volume (volume per unit mass, or reciprocal density), respectively. In a Joule–Thomson process the specific [[enthalpy]] ''h'' remains constant.<ref>See e.g. M.J. Moran and H.N. Shapiro "Fundamentals of Engineering Thermodynamics" 5th Edition (2006) John Wiley & Sons, Inc. page 147</ref> To prove this, the first step is to compute the net work done when a mass ''m'' of the gas moves through the plug. This amount of gas has a volume of ''V''<sub>1</sub> = ''m'' ''v''<sub>1</sub> in the region at pressure ''P''<sub>1</sub> (region 1) and a volume ''V''<sub>2</sub> = ''m'' ''v''<sub>2</sub> when in the region at pressure ''P''<sub>2</sub> (region 2). Then in region 1, the "flow work" done ''on'' the amount of gas by the rest of the gas is: W<sub>1</sub> = ''m'' ''P''<sub>1</sub>''v''<sub>1</sub>. In region 2, the work done ''by'' the amount of gas on the rest of the gas is: W<sub>2</sub> = ''m'' ''P''<sub>2</sub>''v''<sub>2</sub>. So, the total work done ''on'' the mass ''m'' of gas is
:<math>W = mP_1 v_1 - mP_2 v_2.</math>

The change in internal energy minus the total work done ''on'' the amount of gas is, by the [[first law of thermodynamics]], the total heat supplied to the amount of gas.
:<math> U - W = Q </math>

In the Joule–Thomson process, the gas is insulated, so no heat is absorbed. This means that
:<math>\begin{align}
     (mu_2 - mu_1) &- (mP_1 v_1 - mP_2 v_2) = 0 \\
   mu_1 + mP_1 v_1 &= mu_2 + mP_2 v_2 \\
     u_1 + P_1 v_1 &= u_2 + P_2 v_2
\end{align}</math>

where ''u''<sub>1</sub> and ''u''<sub>2</sub> denote the specific internal energies of the gas in regions 1 and 2, respectively. Using the definition of the specific enthalpy ''h = u + Pv'', the above equation implies that
:<math>h_1 = h_2</math>

where h<sub>1</sub> and ''h''<sub>2</sub> denote the specific enthalpies of the amount of gas in regions 1 and 2, respectively.

==Throttling in the ''T''-''s'' diagram==
[[File:Throttling in Ts diagram 01.jpg|450px|thumb|right|Fig. 2 – ''T''-''s'' diagram of nitrogen. The red dome represents the two-phase region with the low-entropy side (the saturated liquid) and the high-entropy side (the saturated gas). The black curves give the ''T''-''s'' relation along isobars. The pressures are indicated in bar. The blue curves are isenthalps (curves of constant specific enthalpy). The specific enthalpies are indicated in kJ/kg. The specific points a, b, etc., are treated in the main text.]]

A convenient way to get a quantitative understanding of the throttling process is by using diagrams such as ''h''-''T'' diagrams, ''h''-''P'' diagrams, and others. Commonly used are the so-called ''T''-''s'' diagrams. Figure 2 shows the ''T''-''s'' diagram of nitrogen as an example.<ref>Figure composed with data obtained with [[REFPROP]], NIST Standard Reference Database 23</ref> Various points are indicated as follows:{{ordered list
 | list-style-type=lower-alpha;
 | 1= ''T'' = 300{{nbsp}}K, ''p'' = 200 bar, ''s'' = 5.16{{nbsp}}kJ/(kgK), ''h'' = 430{{nbsp}}kJ/kg;
 | 2= ''T'' = 270{{nbsp}}K, ''p'' = 1 bar, ''s'' = 6.79{{nbsp}}kJ/(kgK), ''h'' = 430{{nbsp}}kJ/kg;
 | 3= ''T'' = 133{{nbsp}}K, ''p'' = 200 bar, ''s'' = 3.75{{nbsp}}kJ/(kgK), ''h'' = 150{{nbsp}}kJ/kg;
 | 4= ''T'' = 77.2{{nbsp}}K, ''p'' = 1 bar, ''s'' = 4.40{{nbsp}}kJ/(kgK), ''h'' = 150{{nbsp}}kJ/kg;
 | 5= ''T'' = 77.2{{nbsp}}K, ''p'' = 1 bar, ''s'' = 2.83{{nbsp}}kJ/(kgK), ''h'' = 28{{nbsp}}kJ/kg (saturated liquid at 1 bar);
 | 6= ''T'' = 77.2{{nbsp}}K, ''p'' = 1 bar, ''s'' = 5.41{{nbsp}}kJ/(kgK), ''h'' = 230{{nbsp}}kJ/kg (saturated gas at 1 bar).
}}

As shown before, throttling keeps ''h'' constant. E.g. throttling from 200 bar and 300{{nbsp}}K (point a in fig. 2) follows the isenthalpic (line of constant specific enthalpy) of 430{{nbsp}}kJ/kg. At 1 bar it results in point b which has a temperature of 270{{nbsp}}K. So throttling from 200 bar to 1 bar gives a cooling from room temperature to below the freezing point of water. Throttling from 200 bar and an initial temperature of 133{{nbsp}}K (point c in fig. 2) to 1 bar results in point d, which is in the two-phase region of nitrogen at a temperature of 77.2{{nbsp}}K. Since the enthalpy is an extensive parameter the enthalpy in d (''h''<sub>d</sub>) is equal to the enthalpy in e (''h''<sub>e</sub>) multiplied with the mass fraction of the liquid in d (''x''<sub>d</sub>) plus the enthalpy in f (''h''<sub>f</sub>) multiplied with the mass fraction of the gas in d (1 − ''x''<sub>d</sub>). So
:<math>h_d = x_d h_e + (1 - x_d) h_f.</math>

With numbers: 150 = ''x''<sub>d</sub> 28 + (1 − ''x''<sub>d</sub>) 230 so ''x''<sub>d</sub> is about 0.40. This means that the mass fraction of the liquid in the liquid–gas mixture leaving the throttling valve is 40%.

==Derivation of the Joule–Thomson coefficient==

It is difficult to think physically about what the Joule–Thomson coefficient, <math>\mu_{\mathrm{JT}}</math>, represents. Also, modern determinations of <math>\mu_{\mathrm{JT}}</math> do not use the original method used by Joule and Thomson, but instead measure a different, closely related quantity.<ref>{{cite book|title=Physical Chemistry|last=Atkins|first=Peter|publisher=W.H. Freeman and Co.|year=1997|isbn=978-0-7167-2871-9|location=New York|pages=[https://archive.org/details/physicalchemistr00atki/page/89 89–90]|edition=6th|url=https://archive.org/details/physicalchemistr00atki/page/89}}</ref> Thus, it is useful to derive relationships between <math>\mu_{\mathrm{JT}}</math> and other, more conveniently measured quantities, as described below.

The first step in obtaining these results is to note that the Joule–Thomson coefficient involves the three variables ''T'', ''P'', and ''H''. A useful result is immediately obtained by applying the [[triple product rule|cyclic rule]]; in terms of these three variables that rule may be written
:<math>\left(\frac{\partial T}{\partial P}\right)_H\left(\frac{\partial H}{\partial T}\right)_P \left(\frac{\partial P}{\partial H}\right)_T = -1.</math>

Each of the three partial derivatives in this expression has a specific meaning. The first is <math>\mu_{\mathrm{JT}}</math>, the second is the constant pressure [[heat capacity]], <math>C_{\mathrm{p}}</math>, defined by
:<math>C_{\mathrm{p}} = \left(\frac{\partial H}{\partial T}\right)_P </math>

and the third is the inverse of the ''isothermal Joule–Thomson coefficient'', <math>\mu_{\mathrm{T}}</math>, defined by
:<math>\mu_{\mathrm{T}} = \left(\frac{\partial H}{\partial P}\right)_T </math>.
This last quantity is more easily measured than <math>\mu_{\mathrm{JT}}</math> .<ref>{{cite journal|title=The pressure variation of the heat function as a direct measure of the van der Waals forces|last1=Keyes|first1=F.G.|date=1932|journal=Proc. Natl. Acad. Sci. U.S.A.|doi=10.1073/pnas.18.4.328|pmid=16587688|last2=Collins|first2=S.C.|volume=18|issue=4|pages=328–333|bibcode=1932PNAS...18..328K|pmc=1076221|doi-access=free}}</ref><ref>{{cite journal|title=A flow calorimeter for the measurement of the isothermal Joule–Thomson coefficient of gases at elevated temperatures and pressures. Results for nitrogen at temperatures up to 473 K and pressures up to 10 MPa and for carbon dioxide at temperatures up to 500 K and pressures up to 5 MPa|last1=Cusco|first1=L.|date=1995|journal= The Journal of Chemical Thermodynamics|doi=10.1006/jcht.1995.0073|last2=McBain|first2=S.E.|last3=Saville|first3=G.|volume=27|issue=7|pages=721–733}}</ref> Thus, the expression from the cyclic rule becomes
:<math>\mu_{\mathrm{JT}} = - \frac{\mu_{\mathrm{T}}} {C_p}.</math>

This equation can be used to obtain Joule–Thomson coefficients from the more easily measured isothermal Joule–Thomson coefficient. It is used in the following to obtain a mathematical expression for the Joule–Thomson coefficient in terms of the volumetric properties of a fluid.

To proceed further, the starting point is the [[fundamental thermodynamic relation|fundamental equation of thermodynamics]] in terms of enthalpy; this is
:<math>\mathrm{d}H = T \mathrm{d}S + V \mathrm{d}P.</math>

Now "dividing through" by d''P'', while holding temperature constant, yields
:<math>\left(\frac{\partial H}{\partial P}\right)_T = T\left(\frac{\partial S}{\partial P}\right)_T + V</math>
The partial derivative on the left is the isothermal Joule–Thomson coefficient, <math>\mu_{\mathrm{T}}</math>, and the one on the right can be expressed in terms of the coefficient of thermal expansion via a [[Maxwell relation]]. The appropriate relation is
:<math>\left(\frac{\partial S}{\partial P}\right)_T= -\left(\frac{\partial V}{\partial T}\right)_P= -V\alpha\,</math>
where ''α'' is the cubic [[coefficient of thermal expansion]]. Replacing these two partial derivatives yields
:<math>\mu_{\mathrm{T}} = - T V\alpha\ + V. </math>

This expression can now replace <math>\mu_{\mathrm{T}}</math> in the earlier equation for <math>\mu_{\mathrm{JT}}</math> to obtain:
:<math>\mu_{\mathrm{JT}} \equiv \left( \frac{\partial T}{\partial P} \right)_H = \frac V {C_{\mathrm{p}}} (\alpha T - 1).\,</math>

This provides an expression for the Joule–Thomson coefficient in terms of the commonly available properties heat capacity, molar volume, and thermal expansion coefficient. It shows that the Joule–Thomson inversion temperature, at which <math>\mu_{\mathrm{JT}}</math> is zero, occurs when the coefficient of thermal expansion is equal to the inverse of the temperature. Since this is true at all temperatures for ideal gases (see [[thermal expansion#Isobaric expansion in ideal gases|expansion in gases]]), the Joule–Thomson coefficient of an ideal gas is zero at all temperatures.<ref>{{cite book|title=Thermodynamics|url=https://archive.org/details/thermodynamicsin00call|url-access=registration|last=Callen|first=H.B|publisher=John Wiley and Sons|year=1960|location=New York|pages=[https://archive.org/details/thermodynamicsin00call/page/112 112–114]}}</ref>

==Joule's second law==
{{See also|Joule's first law}}
It is easy to verify that for an [[ideal gas]] defined by suitable microscopic postulates that ''αT'' = 1, so the temperature change of such an ideal gas at a Joule–Thomson expansion is zero.
For such an ideal gas, this theoretical result implies that:
:''The internal energy of a fixed mass of an ideal gas depends only on its temperature (not pressure or volume).''

This rule was originally found by Joule experimentally for real gases and is known as '''Joule's second law'''. More refined experiments found important deviations from it.<ref>[[J.R. Partington|Partington, J.R.]] (1949). ''An Advanced Treatise on Physical Chemistry'', volume 1 ''Fundamental Principles. The Properties of Gases'', [[Longman|Longmans, Green and Co.]], London, pp. 614–615.</ref><ref>Adkins, C.J. (1968/1983). ''Equilibrium Thermodynamics'', (1st edition 1968), third edition 1983, Cambridge University Press, Cambridge UK, {{ISBN|0-521-25445-0}}, p. 116.</ref><ref>Bailyn, M. (1994). ''A Survey of Thermodynamics'', American Institute of Physics Press, New York, {{ISBN|0-88318-797-3}}, p. 81.</ref>

==See also==
*[[Critical point (thermodynamics)]]
*[[Enthalpy]] and [[Isenthalpic process]]
*[[Ideal gas]]
*[[Liquefaction of gases]]
*[[MIRI (Mid-Infrared Instrument)]], a J–T loop is used on one of the instruments of the [[James Webb Space Telescope]]
*[[Refrigeration]]
*[[Reversible process (thermodynamics)]]

==References==
{{Reflist}}

==Bibliography==
*{{cite book
|author=M. W. Zemansky
|title=Heat and Thermodynamics; An Intermediate Textbook
|url=https://archive.org/details/heatthermodynami0000zema
|url-access=registration
|publisher=McGraw-Hill
|year=1968
|pages=[https://archive.org/details/heatthermodynami0000zema/page/182 182], 355
|lccn=67026891
}}
*{{cite book
|author=D. V. Schroeder
|title=An Introduction to Thermal Physics
|url=https://archive.org/details/introductiontoth00schr_817
|url-access=limited
|publisher=Addison Wesley Longman
|year=2000
|isbn=978-0-201-38027-9
|page=[https://archive.org/details/introductiontoth00schr_817/page/n153 142]
}}
*{{cite book
|author=C. Kittel, H. Kroemer
|title=Thermal Physics
|publisher=W. H. Freeman
|year=1980
|isbn=978-0-7167-1088-2
}}

==External links==
{{Commons category|Joule-Thomson effect}}
*{{ScienceWorld|title=Joule-Thomson process|urlname=physics/Joule-ThomsonProcess}}
*{{ScienceWorld|title=Joule-Thomson coefficient|urlname=/physics/Joule-ThomsonCoefficient}}
*{{cite web|url=http://demonstrations.wolfram.com/InversionCurveOfJouleThomsonUsingThePengRobinsonCubicEquatio/ |title=Inversion Curve of Joule-Thomson Effect using Peng-Robinson CEOS|work=Demonstrations Projects of Wolfram Mathematica}}
*[https://web.archive.org/web/20050612085146/http://www.nd.edu/~ed/Joule_Thomson/joule_thomson.htm Joule–Thomson effect module], University of Notre Dame

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