Development of the Adiabatic Condition绝热条件的发展
![]() Since the adiabatic constant γ for a gas is the ratio of the specific heats as indicated above, it depends upon the effective number of degrees of freedom in the molecular motion. It can in fact be expressed as γ = (f+2)/f where f is the number of degrees of freedom in the molecular motion. For a monoatomic gas like helium, f=3 and γ = 5/3. For diatomic molecules like N2 and O2, you include two degrees of rotational freedom, so f=5 and γ = 1.4 . Since almost all of the atmosphere is nitrogen and oxygen, γ = 1.4 can be used for air in such calculations as the speed of sound. For polyatomic molecules, there are three degrees of rotational freedom and this along with the three translational degrees of freedom would give γ = 4/3. But in the specific heats of polyatomic molecules, there is evidence of contribution by vibrational degrees of freedom, and this would further reduce the value of γ.
由于气体的绝热常数γ如上所述是比热容的比值,它取决于分子运动的有效自由度数。事实上,它可以表示为γ = (f+2)/f,其中f是分子运动的自由度数。对于单原子气体如氦,f=3,γ = 5/3。对于双原子分子如N₂和O₂,你包括两个旋转自由度,所以f=5,γ = 1.4。由于大气中几乎全部都是氮气和氧气,因此在计算如声速这样的问题时,可以使用γ = 1.4。对于多原子分子,有三个旋转自由度,加上三个平动自由度,会得到γ = 4/3。但在多原子分子的定容比热和定压比热中,有证据表明振动自由度也有所贡献,这会进一步降低γ的值。 |
Index Heat engine concepts 热机概念索引 | ||
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