An adiabatic process (//; from the Greek privative "a" + "diavaton") is a process which occurs with the transfer of neither heat nor matter between a system and its surroundings.^{[1]}^{[2]} A key concept in thermodynamics, adiabatic transfer provides a rigorous conceptual basis for the theory used to expound the first law of thermodynamics. It is also key in a practical sense, that many rapid chemical and physical processes are described using the adiabatic approximation; such processes are usually followed or preceded by events that do involve heat transfer.
Adiabatic processes are primarily and exactly defined for a system contained by walls that are completely thermally insulating and impermeable to matter; such walls are said to be adiabatic. An adiabatic transfer is a transfer of energy as work across an adiabatic wall or sector of a boundary.
Approximately, a transfer may be regarded as adiabatic if it happens in an extremely short time, so that there is no opportunity for significant heat exchange.^{[3]}
The adiabatic flame temperature is a virtual quantity. It is the temperature that would be achieved by a flame in the absence of heat loss to the surroundings.
Etymology
The term adiabatic literally means 'without passage'.^{[4]} It is formed from the privative "a" ("not") + "diavaton", from διάβατον, διαβατικόν: "able to pass", "of the passage", in turn deriving from διὰ ("through"), and βαῖνειν ("to pass").
The etymological origin corresponds here to an absence of transfer of energy as heat and of transfer of matter.
Description
An adiabatic transfer of energy as work may be described by the notation Q = 0 where Q is the quantity of energy transferred as heat across the adiabatic boundary or wall.
For a fictive quasistatic transfer of energy as heat, driven by an ideally infinitesimal temperature difference, the second law of thermodynamics provides that δQ = T d_{e}S, where δQ denotes an infinitesimal element of transfer of energy as heat into the system from its surroundings, T denotes the practically common temperature of system and surroundings at which the transfer takes place, and d_{e}S denotes the infinitesimal element of entropy transferred into the system from the surroundings with the heat transfer.
For a natural process of transfer of energy as heat, driven by a finite temperature difference, there is generation of entropy within the system, in addition to entropy that is transferred into the system from the surroundings. If the process is fairly slow, so that it can be described near enough by differentials, the second law of thermodynamics observes that δQ < T dS. Here T denotes the temperature of the system to which heat is transferred. Entropy d_{i}S is thereby generated internally within the system, in addition to the entropy δQ = d_{e}S transferred with the heat. Thus the total entropy increment within the system is given by dS = d_{i}S + d_{e}S.^{[5]} A natural adiabatic process is irreversible and is not isentropic.
An ideal or fictive adiabatic transfer of energy as work that occurs without friction or viscous dissipation within the system is said to be isentropic, with ΔS = 0.
Adiabatic transfer of energy as work can be analyzed into two extreme component kinds. One extreme kind is without friction or viscous dissipation within the system, and this is usually pressurevolume work, denoted customarily by P dV. This is an ideal case that does not exactly occur in nature. It may be regarded as "reversible". The other extreme kind is isochoric work, for which dV = 0, solely through friction or viscous dissipation within the system. Isochoric work is irreversible.^{[6]} The second law of thermodynamics observes that a natural process of transfer of energy as work, exactly considered, always consists at least of isochoric and often of both of these extreme kinds of work. Every natural process, exactly considered, is irreversible, however slight may be the friction or viscosity. For a natural process of transfer of energy as heat, driven by a finite temperature difference, entropy is generated within the system. Such a process is not isentropic.
Also of interest is a thermodynamic operation that starts with a rigid adiabatic enclosure that contains an impermeable immovable partition that separates two compartments at different pressures. The thermodynamic operation removes the partition, so that the compartment initially at higher pressure expands into the space of the compartment initially at lower pressure. The subsequent internal equilibration to a common homogeneous pressure is irreversible. There is no energy transfer between the rigid adiabatic enclosure and its surroundings, neither as work, nor as heat. This internal equilibration is isenthalpic. It brings about an increase in the entropy within the rigid adiabatic enclosure.
Adiabatic heating and cooling
Adiabatic changes in temperature occur due to changes in pressure of a gas while not adding or subtracting any heat. In contrast, free expansion is an isothermal process for an ideal gas.
Adiabatic heat occurs when the pressure of a gas is increased from work done on it by its surroundings, e.g., a piston compressing a gas contained within an adiabatic cylinder. This finds practical application in Diesel engines which rely on the lack of quick heat dissipation during their compression stroke to elevate the fuel vapor temperature sufficiently to ignite it.
Adiabatic heating also occurs in the Earth's atmosphere when an air mass descends, for example, in a katabatic wind or Foehn or chinook wind flowing downhill over a mountain range. When a parcel of air descends, the pressure on the parcel increases. Due to this increase in pressure, the parcel's volume decreases and its temperature increases, thus increasing the internal energy.
Adiabatic cooling occurs when the pressure of a substance is decreased as it does work on its surroundings. Adiabatic cooling occurs in the Earth's atmosphere with orographic lifting and lee waves, and this can form pileus or lenticular clouds if the air is cooled below the dew point. When the pressure applied on a parcel of air decreases, the air in the parcel is allowed to expand; as the volume increases, the temperature falls and internal energy decreases.
Adiabatic cooling does not have to involve a fluid. One technique used to reach very low temperatures (thousandths and even millionths of a degree above absolute zero) is adiabatic demagnetisation, where the change in magnetic field on a magnetic material is used to provide adiabatic cooling. Also, the contents of an expanding universe (to first order) can be described as an adiabatically cooling fluid. (See  Heat death of the universe)
Rising magma also undergoes adiabatic cooling before eruption, particularly significant in the case of magmas that rise quickly from great depths such as kimberlites.^{[7]}
Such temperature changes can be quantified using the ideal gas law, or the hydrostatic equation for atmospheric processes.
In practice, no process is truly adiabatic. Many processes rely on a large difference in time scales of the process of interest and the rate of heat dissipation across a system boundary, and thus are approximated by using an adiabatic assumption. There is always some heat loss, as no perfect insulators exist.
Ideal gas (reversible process)
The mathematical equation for an ideal gas undergoing a reversible (i.e., no entropy generation) adiabatic process is
 $P\; V^\{\backslash gamma\}\; =\; \backslash operatorname\{constant\}\; \backslash qquad$
where P is pressure, V is volume, and
 $\backslash gamma\; =\; \{C\_\{P\}\; \backslash over\; C\_\{V\}\}\; =\; \backslash frac\{f\; +\; 2\}\{f\},$
$C\_\{P\}$ being the specific heat for constant pressure,
$C\_\{V\}$ being the specific heat for constant volume, $\backslash gamma$ is the adiabatic index, and $f$ is the number of degrees of freedom (3 for monatomic gas, 5 for diatomic gas and collinear molecules e.g. carbon dioxide).
For a monatomic ideal gas, $\backslash gamma\; =\; 5/3\; \backslash ,$, and for a diatomic gas (such as nitrogen and oxygen, the main components of air) $\backslash gamma\; =\; 7/5\; \backslash ,$.^{[8]} Note that the above formula is only applicable to classical ideal gases and not Bose–Einstein or Fermi gases.
For reversible adiabatic processes, it is also true that
 $P^\{1\backslash gamma\}T^\{\backslash gamma\}=\; \backslash operatorname\{constant\}$
 $VT^\{f/2\}\; =\; \backslash operatorname\{constant\}$
where T is an absolute temperature.
This can also be written as
 $TV^\{\backslash gamma\; \; 1\}\; =\; \backslash operatorname\{constant\}$
Example of adiabatic compression
Let's now look at a common example of adiabatic compression the compression stroke in a gasoline engine. We will make a few simplifying assumptions: that the uncompressed volume of the cylinder is 1000cc's (one liter), that the gas within is nearly pure nitrogen (thus a diatomic gas with five degrees of freedom and so $\backslash gamma$ = 7/5), and that the compression ratio of the engine is 10:1 (that is, the 1000 cc volume of uncompressed gas will compress down to 100 cc when the piston goes from bottom to top). The uncompressed gas is at approximately room temperature and pressure (a warm room temperature of ~27 degC or 300 K, and a pressure of 1 bar ~ 100,000 Pa, or about 14.7 PSI, or typical sealevel atmospheric pressure).
$P\; V^\{\backslash gamma\}\; =\; \backslash operatorname\{constant\}\; =\; 100,000\; \backslash operatorname\{pa\}\; *\; 1000^\{7/5\}\; =\; 100\; \backslash times\; 10^3\; *\; 15.8\; \backslash times\; 10^3\; =\; 1.58\; \backslash times\; 10^9$
so our adiabatic constant for this experiment is about 1.58 billion.
The gas is now compressed to a 100cc volume (we will assume this happens quickly enough that no heat can enter or leave the gas). The new volume is 100 ccs, but the constant for this experiment is still 1.58 billion:
$P\; *\; V^\{\backslash gamma\}\; =\; \backslash operatorname\{constant\}\; =\; 1.58\; \backslash times\; 10^9\; =\; P\; *\; 100^\{7/5\}$
so solving for P:
$P\; =\; 1.58\; \backslash times\; 10^9\; /\; \{100^\{7/5\}\}\; =\; 1.58\; \backslash times\; 10^9\; /\; 630.9\; =\; 2.50\; \backslash times\; 10^6\; \backslash operatorname\{\; Pa\}$
or about 362 PSI or 24.5 atm. Note that this pressure increase is more than a simple 10:1 compression ratio would indicate; this is because the gas is not only compressed, but the work done to compress the gas has also heated the gas and the hotter gas will have a greater pressure even if the volume had not changed.
We can solve for the temperature of the compressed gas in the engine cylinder as well, using the ideal gas law.
Our initial conditions are 100,000 pa of pressure, 1000 cc volume, and 300 K of temperature, so our experimental constant is:
$\{P\; V\; \backslash over\; T\}\; =\; \backslash operatorname\; \{constant\}\; =\; \}\; =\; T\; =\; =\; 751$
That's a final temperature of 751 K, or 477 °C, or 892 °F, well above the ignition point of many fuels. This is why a high compression engine requires fuels specially formulated to not selfignite (which would cause engine knocking when operated under these conditions of temperature and pressure), or that a supercharger and inter cooler to provide a lower temperature at the same pressure would be advantageous. A diesel engine operates under even more extreme conditions, with compression ratios of 20:1 or more being typical, in order to provide a very high gas temperature which ensures immediate ignition of injected fuel.
Adiabatic free expansion of a gas
For an adiabatic free expansion of an ideal gas, the gas is contained in an insulated container and then allowed to expand in a vacuum. Because there is no external pressure for the gas to expand against, the work done by or on the system is zero. Since this process does not involve any heat transfer or work, the First Law of Thermodynamics then implies that the net internal energy change of the system is zero. For an ideal gas, the temperature remains constant because the internal energy only depends on temperature in that case. Since at constant temperature, the entropy is proportional to the volume, the entropy increases in this case, therefore this process is irreversible.
Derivation of continuous formula for adiabatic heating and cooling
The definition of an adiabatic process is that heat transfer to the system is zero, $\backslash delta\; Q=0$. Then, according to the first law of thermodynamics,
 $\backslash text\{(1)\}\; \backslash qquad\; d\; U\; +\; \backslash delta\; W\; =\; \backslash delta\; Q\; =\; 0,$
where dU is the change in the internal energy of the system and δW is work done
by the system. Any work (δW) done must be done at the expense of internal energy U, since no heat δQ is being supplied from the surroundings. Pressurevolume work δW done by the system is defined as
 $\backslash text\{(2)\}\; \backslash qquad\; \backslash delta\; W\; =\; P\; \backslash ,\; dV.$
However, P does not remain constant during an adiabatic process but
instead changes along with V.
It is desired to know how the values of dP and
dV relate to each other as the adiabatic process proceeds.
For an ideal gas the internal energy is given by
 $\backslash text\{(3)\}\; \backslash qquad\; U\; =\; \backslash alpha\; n\; R\; T,$
where $\{\backslash alpha\}$ is the number of degrees of freedom divided by two, R is the universal gas constant and n is the number of moles in the system (a constant).
Differentiating Equation (3) and use of the ideal gas law, $P\; V\; =\; n\; R\; T$, yields
 $\backslash text\{(4)\}\; \backslash qquad\; d\; U\; =\; \backslash alpha\; n\; R\; \backslash ,\; dT$
= \alpha \, d (P V)
= \alpha (P \, dV + V \, dP).
Equation (4) is often expressed as $d\; U\; =\; n\; C\_\{V\}\; \backslash ,\; d\; T$
because $C\_\{V\}\; =\; \backslash alpha\; R$.
Now substitute equations (2) and (4) into equation (1) to obtain
 $P\; \backslash ,\; dV\; =\; \backslash alpha\; P\; \backslash ,\; dV\; +\; \backslash alpha\; V\; \backslash ,\; dP,$
factorize :$P\; \backslash ,\; dV,$:
 $\; (\backslash alpha\; +\; 1)\; P\; \backslash ,\; dV\; =\; \backslash alpha\; V\; \backslash ,\; dP,$
and divide both sides by PV:
 $(\backslash alpha\; +\; 1)\; \{d\; V\; \backslash over\; V\}\; =\; \backslash alpha\; \{d\; P\; \backslash over\; P\}.$
After integrating the left and right sides from $V\_0$ to V and from $P\_0$ to P and changing the sides respectively,
 $\backslash ln\; \backslash left(\; \{P\; \backslash over\; P\_0\}\; \backslash right)\; =\; \{\{\backslash alpha\; +\; 1\; \backslash over\; \backslash alpha\}\}\; \backslash ln\; \backslash left(\; \{V\; \backslash over\; V\_0\}\; \backslash right).$
Exponentiate both sides, and substitute $\{\backslash alpha\; +\; 1\; \backslash over\; \backslash alpha\}$ with $\backslash gamma$, the heat capacity ratio
 $\backslash left(\; \{P\; \backslash over\; P\_0\}\; \backslash right)\; =\; \backslash left(\; \{V\; \backslash over\; V\_0\}\; \backslash right)^\{\{\backslash gamma\}\},$
and eliminate the negative sign to obtain
 $\backslash left(\; \{P\; \backslash over\; P\_0\}\; \backslash right)\; =\; \backslash left(\; \{V\_0\; \backslash over\; V\}\; \backslash right)^\{\backslash gamma\}.$
Therefore,
 $\backslash left(\; \{P\; \backslash over\; P\_0\}\; \backslash right)\; \backslash left(\; \{V\; \backslash over\; V\_0\}\; \backslash right)^\{\backslash gamma\}\; =\; 1$
and
 $P\_0\; V\_0^\{\backslash gamma\}\; =\; P\; V^\backslash gamma\; =\; \backslash operatorname\{constant\}.$
Derivation of discrete formula
The change in internal energy of a system, measured from state 1 to state 2, is equal to
 $\backslash text\{(1)\}\; \backslash qquad\; \backslash Delta\; U\; =\; \backslash alpha\; R\; nT\_2\; \; \backslash alpha\; R\; nT\_1\; =\; \backslash alpha\; Rn\; \backslash Delta\; T$
At the same time, the work done by the pressurevolume changes as a result from this process, is equal to
 $\backslash text\{(2)\}\; \backslash qquad\; W\; =\; \backslash int\_\{V\_1\}^\{V\_2\}P\backslash ,\; dV$
Since we require the process to be adiabatic, the following equation needs to be true
 $\backslash text\{(3)\}\; \backslash qquad\; \backslash Delta\; U\; +\; W\; =\; 0$
By the previous derivation,
 $\backslash text\{(4)\}\; \backslash qquad\; P\; V^\backslash gamma\; =\; \backslash text\{constant\}\; =\; P\_1\; V\_1^\backslash gamma$
Rearranging (4) gives
 $P\; =\; P\_1\; \backslash left(\backslash frac\{V\_1\}\{V\}\; \backslash right)^\backslash gamma$
Substituting this into (2) gives
 $W\; =\; \backslash int\_\{V\_1\}^\{V\_2\}P\_1\; \backslash left(\backslash frac\{V\_1\}\{V\}\; \backslash right)^\backslash gamma\backslash ,\; dV$
Integrating,
 $W\; =\; P\_1\; V\_1^\backslash gamma\; \backslash frac\{V\_2^\{1\backslash gamma\}V\_1^\{1\backslash gamma\}\}\{1\backslash gamma\}$
Substituting $\backslash gamma\; =\; \backslash frac\{\backslash alpha+1\}\{\backslash alpha\}$,
 $W\; =\; \; \backslash alpha\; P\_1\; V\_1^\{\backslash gamma\}\; \backslash left(\; V\_2^\{1\backslash gamma\}\; \; V\_1^\{1\backslash gamma\}\; \backslash right)$
Rearranging,
 $W\; =\; \; \backslash alpha\; P\_1\; V\_1\; \backslash left(\; \backslash left(\; \backslash frac\{V\_2\}\{V\_1\}\; \backslash right)^\{1\backslash gamma\}\; \; 1\; \backslash right)$
Using the ideal gas law and assuming a constant molar quantity (as often happens in practical cases),
 $W\; =\; \; \backslash alpha\; n\; R\; T\_1\; \backslash left(\; \backslash left(\; \backslash frac\{V\_2\}\{V\_1\}\; \backslash right)^\{1\backslash gamma\}\; \; 1\; \backslash right)$
By the continuous formula,
 $\backslash frac\{P\_2\}\{P\_1\}=\backslash left(\backslash frac\{V\_2\}\{V\_1\}\backslash right)^\{\backslash gamma\}$
Or,
 $\backslash left(\backslash frac\{P\_2\}\{P\_1\}\backslash right)^\{1\; \backslash over\; \backslash gamma\}=\backslash frac\{V\_2\}\{V\_1\}$
Substituting into the previous expression for $W$,
 $W\; =\; \; \backslash alpha\; n\; R\; T\_1\; \backslash left(\; \backslash left(\; \backslash frac\{P\_2\}\{P\_1\}\; \backslash right)^\{\backslash frac\{\backslash gamma1\}\{\backslash gamma\}\}\; \; 1\; \backslash right)$
Substituting this expression and (1) in (3) gives
 $\backslash alpha\; n\; R\; (T\_2\; \; T\_1)\; =\; \backslash alpha\; n\; R\; T\_1\; \backslash left(\; \backslash left(\; \backslash frac\{P\_2\}\{P\_1\}\; \backslash right)^\{\backslash frac\{\backslash gamma1\}\{\backslash gamma\}\}\; \; 1\; \backslash right)$
Simplifying,
 $T\_2\; \; T\_1\; =\; T\_1\; \backslash left(\; \backslash left(\; \backslash frac\{P\_2\}\{P\_1\}\; \backslash right)^\{\backslash frac\{\backslash gamma1\}\{\backslash gamma\}\}\; \; 1\; \backslash right)$
Simplifying,
 $\backslash frac\{T\_2\}\{T\_1\}1\; =\; \backslash left(\; \backslash frac\{P\_2\}\{P\_1\}\; \backslash right)^\{\backslash frac\{\backslash gamma1\}\{\backslash gamma\}\}\; \; 1$
Simplifying,
 $T\_2\; =\; T\_1\; \backslash left(\; \backslash frac\{P\_2\}\{P\_1\}\; \backslash right)^\{\backslash frac\{\backslash gamma1\}\{\backslash gamma\}\}$
Graphing adiabats
An adiabat is a curve of constant entropy on the PV diagram. Properties of adiabats on a PV diagram are:
 Every adiabat asymptotically approaches both the V axis and the P axis (just like isotherms).
 Each adiabat intersects each isotherm exactly once.
 An adiabat looks similar to an isotherm, except that during an expansion, an adiabat loses more pressure than an isotherm, so it has a steeper inclination (more vertical).
 If isotherms are concave towards the "northeast" direction (45 °), then adiabats are concave towards the "east northeast" (31 °).
 If adiabats and isotherms are graphed severally at regular changes of entropy and temperature, respectively (like altitude on a contour map), then as the eye moves towards the axes (towards the southwest), it sees the density of isotherms stay constant, but it sees the density of adiabats grow. The exception is very near absolute zero, where the density of adiabats drops sharply and they become rare (see Nernst's theorem).
The following diagram is a PV diagram with a superposition of adiabats and isotherms:
The isotherms are the red curves and the adiabats are the black curves.
The adiabats are isentropic.
Volume is the horizontal axis and pressure is the vertical axis.
See also
References

 Broholm, Collin. "Adiabatic free expansion." Physics & Astronomy @ Johns Hopkins University. N.p., 26 Nov. 1997. Web. 14 Apr. *Nave, Carl Rod. "Adiabatic Processes." HyperPhysics. N.p., n.d. Web. 14 Apr. 2011. [1].
 Thorngren, Dr. Jane R.. "Adiabatic Processes." Daphne – A Palomar College Web Server. N.p., 21 July 1995. Web. 14 Apr. 2011. [2].
External links
 Article in HyperPhysics Encyclopaedia
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