Heat capacity ratio
Thermodynamics  

The classical Carnot heat engine  
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Book:Thermodynamics  
Heat capacity ratio for various gases^{[1]}^{[2]}  

Temp.  Gas  γ  Temp.  Gas  γ  Temp.  Gas  γ  
−181 °C  H_{2}  1.597  200 °C  Dry air  1.398  20 °C  NO  1.400  
−76 °C  1.453  400 °C  1.393  20 °C  N_{2}O  1.310  
20 °C  1.410  1000 °C  1.365  −181 °C  N_{2}  1.470  
100 °C  1.404  2000 °C  1.088  15 °C  1.404  
400 °C  1.387  0 °C  CO_{2}  1.310  20 °C  Cl_{2}  1.340  
1000 °C  1.358  20 °C  1.300  −115 °C  CH_{4}  1.410  
2000 °C  1.318  100 °C  1.281  −74 °C  1.350  
20 °C  He  1.660  400 °C  1.235  20 °C  1.320  
20 °C  H_{2}O  1.330  1000 °C  1.195  15 °C  NH_{3}  1.310  
100 °C  1.324  20 °C  CO  1.400  19 °C  Ne  1.640  
200 °C  1.310  −181 °C  O_{2}  1.450  19 °C  Xe  1.660  
−180 °C  Ar  1.760  −76 °C  1.415  19 °C  Kr  1.680  
20 °C  1.670  20 °C  1.400  15 °C  SO_{2}  1.290  
0 °C  Dry air  1.403  100 °C  1.399  360 °C  Hg  1.670  
20 °C  1.400  200 °C  1.397  15 °C  C_{2}H_{6}  1.220  
100 °C  1.401  400 °C  1.394  16 °C  C_{3}H_{8}  1.130 
In thermal physics and thermodynamics, the heat capacity ratio or adiabatic index or ratio of specific heats or Poisson constant, is the ratio of the heat capacity at constant pressure (C_{P}) to heat capacity at constant volume (C_{V}). It is sometimes also known as the isentropic expansion factor and is denoted by γ (gamma) for an ideal gas or κ (kappa), the isentropic exponent for a real gas. The symbol gamma is used by aerospace and chemical engineers. Mechanical engineers use the Roman letter k.^{[3]}
where C is the heat capacity and c the specific heat capacity (heat capacity per unit mass) of a gas. The suffixes P and V refer to constant pressure and constant volume conditions, respectively.
To understand this relation, consider the following thought experiment. A closed pneumatic cylinder contains air. The piston is locked. The pressure inside is equal to atmospheric pressure. This cylinder is heated to a certain target temperature. Since the piston cannot move, the volume is constant. The temperature and pressure will rise. When the target temperature is reached, the heating is stopped. The amount of energy added equals C_{V}ΔT, with ΔT representing the change in temperature. The piston is now freed and moves outwards, stopping as the pressure inside the chamber reaches atmospheric pressure. We assume the expansion occurs without exchange of heat (adiabatic expansion). Doing this work, air inside the cylinder will cool to below the target temperature. To return to the target temperature (still with a free piston), the air must be heated, but is no longer under constant volume since the piston is free to move as the gas is reheated. This extra heat amounts to about 40% more than the previous amount added. In this example, the amount of heat added with a locked piston is proportional to C_{V}, whereas the total amount of heat added is proportional to C_{P}. Therefore, the heat capacity ratio in this example is 1.4.
Another way of understanding the difference between C_{P} and C_{V} is that C_{P} applies if work is done to the system which causes a change in volume (such as by moving a piston so as to compress the contents of a cylinder), or if work is done by the system which changes its temperature (such as heating the gas in a cylinder to cause a piston to move). C_{V} applies only if P dV – that is, the work done – is zero. Consider the difference between adding heat to the gas with a locked piston, and adding heat with a piston free to move, so that pressure remains constant. In the second case, the gas will both heat and expand, causing the piston to do mechanical work on the atmosphere. The heat that is added to the gas goes only partly into heating the gas, while the rest is transformed into the mechanical work performed by the piston. In the first, constantvolume case (locked piston) there is no external motion, and thus no mechanical work is done on the atmosphere; C_{V} is used. In the second case, additional work is done as the volume changes, so the amount of heat required to raise the gas temperature (the specific heat capacity) is higher for this constant pressure case.
Ideal gas relations
For an ideal gas, the heat capacity is constant with temperature. Accordingly, we can express the enthalpy as H = C_{P}T and the internal energy as U = C_{V}T. Thus, it can also be said that the heat capacity ratio is the ratio between the enthalpy to the internal energy:
Furthermore, the heat capacities can be expressed in terms of heat capacity ratio (γ) and the gas constant (R):
where n is the amount of substance in moles.
It can be rather difficult to find tabulated information for C_{V}, since C_{P} is more commonly tabulated. The following relation, can be used to determine C_{V}:
Relation with degrees of freedom
The heat capacity ratio (γ) for an ideal gas can be related to the degrees of freedom ( f ) of a molecule by:
Thus we observe that for a monatomic gas, with three degrees of freedom:
while for a diatomic gas, with five degrees of freedom (at room temperature: three translational and two rotational degrees of freedom; the vibrational degree of freedom is not involved except at high temperatures):
For example, the terrestrial air is primarily made up of diatomic gases (around 78% nitrogen (N_{2}) and 21% oxygen (O_{2})) and at standard conditions it can be considered to be an ideal gas. The above value of 1.4 is highly consistent with the measured adiabatic indices for dry air within a temperature range of 0–200 °C, exhibiting a deviation of only 0.2% (see tablation above).
Real gas relations
As temperature increases, higher energy rotational and vibrational states become accessible to molecular gases, thus increasing the number of degrees of freedom and lowering γ. For a real gas, both C_{P} and C_{V} increase with increasing temperature, while continuing to differ from each other by a fixed constant (as above, C_{P} = C_{V} + nR) which reflects the relatively constant PV difference in work done during expansion, for constant pressure vs. constant volume conditions. Thus, the ratio of the two values, γ, decreases with increasing temperature. For more information on mechanisms for storing heat in gases, see the gas section of specific heat capacity.
Thermodynamic expressions
Values based on approximations (particularly C_{P} − C_{V} = nR) are in many cases not sufficiently accurate for practical engineering calculations such as flow rates through pipes and valves. An experimental value should be used rather than one based on this approximation, where possible. A rigorous value for the ratio C_{P}/C_{V} can also be calculated by determining C_{V} from the residual properties expressed as:
Values for C_{P} are readily available and recorded, but values for C_{V} need to be determined via relations such as these. See here for the derivation of the thermodynamic relations between the heat capacities.
The above definition is the approach used to develop rigorous expressions from equations of state (such as Peng–Robinson), which match experimental values so closely that there is little need to develop a database of ratios or C_{V} values. Values can also be determined through finite difference approximation.
Adiabatic process
This ratio gives the important relation for an isentropic (quasistatic, reversible, adiabatic process) process of a simple compressible caloricallyperfect ideal gas:
where p is pressure and v is the gas specific volume.
See also
 Relations between heat capacities
 Heat capacity
 Specific heat capacity
 Speed of sound
 Thermodynamic equations
 Thermodynamics
 Volumetric heat capacity