Quick Recap — Advanced Thermodynamics (Multi-step)

  • Adiabatic work: W=P1V1P2V2γ1=nR(T1T2)γ1W=\dfrac{P_1V_1-P_2V_2}{\gamma-1}=\dfrac{nR(T_1-T_2)}{\gamma-1}. Adiabatic ratios: P2P1=(V1V2)γ\dfrac{P_2}{P_1}=\left(\dfrac{V_1}{V_2}\right)^\gamma, T2T1=(V1V2)γ1\dfrac{T_2}{T_1}=\left(\dfrac{V_1}{V_2}\right)^{\gamma-1}.
  • Multi-step / cyclic: apply the first law leg by leg; net W=W= enclosed area, net Q=Q= net WW.
  • Process molar heat capacity: for PVn=PV^n= const, C=CV+R1n=Rγ1+R1nC=C_V+\dfrac{R}{1-n}=\dfrac{R}{\gamma-1}+\dfrac{R}{1-n}.
  • Gas mixtures: CV,mix=n1CV1+n2CV2n1+n2C_{V,mix}=\dfrac{n_1C_{V1}+n_2C_{V2}}{n_1+n_2}, then γmix=CP,mixCV,mix\gamma_{mix}=\dfrac{C_{P,mix}}{C_{V,mix}}.
  • Engines in series: the pair between T1T_1 and T3T_3 has the Carnot efficiency of that overall span.

Worked mini-example. A diatomic gas (γ=1.4\gamma=1.4) is compressed adiabatically to half its volume: P2P1=21.4=2.64\dfrac{P_2}{P_1}=2^{1.4}=2.64, so the pressure rises to about 2.642.64 times its initial value while the temperature rises by 20.4=1.322^{0.4}=1.32.