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\gamma = rac{C_P}{C_V}

It should be noted that chemical engineers and many others commonly refer to the heat capacity ratio as \kappa rather than \gamma.

For a monoatomic Ideal Gas , \gamma = rac{5}{3}, while a diatomic Ideal Gas has \gamma = rac{7}{5}.

For a first approximation assuming Ideal Gas and C_P, C_V, and \gamma are constants, it can be written:

C_P = rac{\gamma R}{\gamma - 1}

C_V = rac{R}{\gamma - 1}

The value of \gamma for various gases @ 1 atm, 20°C is as follow:



















































Gas \gamma
H2 1.41
He 1.66
H2O 1.33
Ar 1.67
Dry Air 1.40
CO2 1.30
CO 1.40
O2 1.40
NO 1.40
N2O 1.31
Cl2 1.34
CH4 1.32


Source: Fluid Mechanics 4th edition McGraw Hill, Frank M. White

C_P and C_V increase with increasing temperature and \gamma decreases. Some correlations exist to provide values of \gamma as a function of the temperature.


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