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General Physics I:

Subsection 10.6.3 Application of I law of thermodynamics

  1. Specific heat capacity of a gas: Consider a mole of gas is heated in the cylinder with frictionless piston, then the change in internal energy of the gas is given by the first law of thermodynamics (10.6.1)
    \begin{equation*} \,dQ=\,dU+\,dW \end{equation*}
    where \(\,dW \) is the infinitesimal work done by the gas in moving a piston from initial position \(i\) to the final position \(f\text{,}\) and is given by
    \begin{equation*} \,dW = F\,dx= pA\,dx= p\,dV \end{equation*}
    where \(A\) is area of cross-section of the piston, \(F\) is force applied by the gas molecules on the surface of the piston.
    \begin{equation} \,dQ=\,dU+ p\,dV \tag{10.6.2} \end{equation}
    If the piston is fixed from moving, then at constant volume, \(\,dV = 0\text{,}\) and
    \begin{equation*} \,dW = p\,dV = 0 \end{equation*}
    \begin{equation} \therefore \quad \,dQ=\,dU \tag{10.6.3} \end{equation}
    But, for n mole of a gas
    \begin{equation*} \,dQ=n C\,dT \end{equation*}
    where C is molar specific heat capacity of the gas.
    \begin{equation*} \,dQ=mc\,dT \end{equation*}
    where \(m\) is mass of the gas, but it is convenient to take mole instead of mass as an amount of gas. At constant volume,
    \begin{equation} \,dQ=n C_{v}\,dT \tag{10.6.4} \end{equation}
    From eqns. (10.6.3) and (10.6.4), we have -
    \begin{equation} \frac{\,dU}{\,dT}=nC_{v} \tag{10.6.5} \end{equation}
    At constant pressure,
    \begin{equation} \,dQ=n C_{p}\,dT \tag{10.6.6} \end{equation}
    \begin{equation} \therefore\quad \frac{\,dQ}{\,dT}=nC_{p} \tag{10.6.7} \end{equation}
    Now, differentiating eqn. (10.6.2) with respect to \(T\text{,}\) we get -
    \begin{equation} \frac{\,dQ}{\,dT} = \frac{\,dU}{\,dT} +p\frac{\,dV}{\,dT} \tag{10.6.8} \end{equation}
    But from euation of state of a gas (10.5.8),
    \begin{equation*} pV = nRT \end{equation*}
    Differentiating this equation with respect to \(T\) at constant \(P\text{,}\) we get -
    \begin{equation} \text{or,}\quad p\frac{\,dV}{\,dT} = nR \tag{10.6.9} \end{equation}
    substituting the values in eqn. (10.6.8) from eqns. (10.6.5) and (10.6.7), we get -
    \begin{equation*} nC_{p}=nC_{v}+nR \end{equation*}
    \begin{equation} \therefore\quad C_{p}-C_{v} = R \tag{10.6.10} \end{equation}
    This is the relation between molar specific heat capacity of a gas at constant pressure \(C_{p}\) and molar specific heat capacity of a gas at constant volume \(C_{v}\text{.}\) From the kinetic theory of gas, the internal energy of a monoatomic gas [(10.5.11)] is given by
    \begin{equation*} U=\frac{3}{2}nRT \end{equation*}
    \begin{equation} \therefore\quad \frac{\,dU}{\,dT} = \frac{3}{2}nR \tag{10.6.11} \end{equation}
    Hence, from eqns. (10.6.8), (10.6.9), and (10.6.11), we have -
    \begin{equation*} \frac{\,dQ}{\,dT} =\frac{3}{2}nR + nR =\frac{5}{2}nR \end{equation*}
    Now, the ratio of the specific heat at constant pressure to the specific heat at constant volume of a monoatomic gas is given by
    \begin{equation*} \gamma = \frac{C_{p}}{C_{v}} = \frac{\frac{5}{2}nR}{\frac{3}{2}nR} = \frac{5}{3} \end{equation*}
    The idea of degrees of freedom can be extended to diatomic and polytomic gases. It can be shown that the value of \(\gamma\) can be expressed as
    \begin{equation*} \gamma=\frac{f+2}{f} \end{equation*}
    where \(f\) is the number of degrees of freedom per molecule. For a monatomic gas, we find that
    \begin{equation*} \gamma = \frac{3+2}{3} = \frac{5}{3} \end{equation*}
    since \(f=3\) for a monoatomic gas.
    \begin{equation*} \gamma = \frac{5+2}{3} = \frac{7}{3} \end{equation*}
    for a diatomic gas as \(f=5\) .
  2. Isothermal process: In an isothermal process system remains at constant temperature, \(T\text{,}\) hence,
    \begin{equation*} \,dT =0. \end{equation*}
    As internal energy of an ideal gas [(10.5.11)] is a function of temperature only,
    \begin{equation*} U=\frac{3}{2}nRT \end{equation*}
    we have
    \begin{equation*} \,dU = 0 \end{equation*}
    Therefore, from I law of thermodynamics, we have -
    \begin{equation*} \,dQ=\,dW= p\,dV \end{equation*}
  3. Adiabatic process: In an adiabatic process system does not exchange heat \(Q\text{,}\) with surroundings, hence,
    \begin{equation*} \,dQ =0. \end{equation*}
    Therefore, from I law of thermodynamics, we have -
    \begin{equation*} \,dQ=\,dU + p\,dV \end{equation*}
    \begin{equation*} \text{or,}\quad 0 = C_{v}\,dT+p\,dV \end{equation*}
    \begin{equation} \therefore \quad C_{v}\,dT = -p\,dV \tag{10.6.12} \end{equation}
    \begin{equation*} \text{or,} \quad \,dU = -\,dW \end{equation*}
    That is, internal energy increases exactly by the amount of work done on the system. Also,
    \begin{equation*} pV=RT \end{equation*}
    for 1 mole of a gas.
    \begin{equation*} \text{or,}\quad p\,dV + V\,dp = R\,dT =\left(C_{p}-C_{v}\right)\,dT \end{equation*}
    \begin{equation*} = C_{v}\left(\frac{C_{p}}{C_{v}}-1\right)\,dT = \left(\gamma-1\right)C_{v}\,dT \end{equation*}
    \begin{equation*} \text{or,}\quad p\,dV + V\,dp = - \left(\gamma-1\right)p\,dV \end{equation*}
    \begin{equation*} \text{or,}\quad p\,dV \left(1+\gamma-1\right) + V\,dp = 0 \end{equation*}
    \begin{equation*} \text{or,}\quad \gamma p\,dV + V\,dp =0 \end{equation*}
    \begin{equation*} \text{or,}\quad \frac{ \,dp}{p} +\gamma \frac{\,dV}{V} = 0 \end{equation*}
    integrating both sides, we get -
    \begin{equation*} \ln p +\gamma \ln V =constant \end{equation*}
    \begin{equation*} \text{or,}\quad \ln p + \ln V^{\gamma} =constant \end{equation*}
    \(\because n\ln m = \ln m^{n}]\)
    \begin{equation} \therefore \quad pV^{\gamma} =const.\tag{10.6.13} \end{equation}
    \([\because \ln m +\ln n = \ln (mn)] \)
  4. Isobaric process: A process at constant pressure,
    \begin{equation*} \,dp=0 \end{equation*}
    is called an isobaric process.
    \begin{equation*} \,dQ=\,dU+p\,dV \end{equation*}
    At the change of phase, temperature and pressure remains constant, i.e.,
    \begin{equation*} \,dT=0, \end{equation*}
    \begin{equation*} \text{and} \quad \,dp=0. \end{equation*}
    \begin{equation*} \therefore \,dQ=p\,dV \end{equation*}
    \([\because U \propto T]\)
  5. Isochoric process: A process at constant volume,
    \begin{equation*} \,dV=0 \end{equation*}
    is called an isochoric process.
    \begin{equation*} \,dQ=\,dU \end{equation*}
  6. Free expansion: It is an adiabatic process in which no work is performed on or by the system. Consider two chambers of an isolated system, the one chamber of which contains a gas while the other is completely evacuated. Both the chambers are connected with a stopcock. When stopcock is suddenly open, the gas rushes into the evacuated chamber and expands freely. Free expansion means gas has to do no work at all. Since an isolated system does not exchange heat from outside world,
    \begin{equation*} \,dQ=0 \end{equation*}
    and gas expands freely so
    \begin{equation*} \,dW=0 \end{equation*}
    Therefore from I law of thermodynamics,
    \begin{equation*} \,dU=0 \end{equation*}
    That is, initial internal energy of the gas is same as its final internal energy.