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In thermodynamics, the heat capacity at constant volume, $C V$ , and the heat capacity at constant pressure, $C P$ , are extensive properties that can be written in dimensions of energy/degree temperature. The laws of thermodynamics imply the following relations between these two heat capacities (Gaskell 2003:23):

$C_{P} - C_{V}= V T\frac{\alpha^{2}}{\beta_{T}}\,$

$\frac{C_{P}}{C_{V}}=\frac{\beta_{T}}{\beta_{S}}\,$

Here $α$ is the thermal expansion coefficient:

$\alpha=\frac{1}{V}\left(\frac{\partial V}{\partial T}\right)_{P}\,$

$β T$ is the isothermal compressibility:

$\beta_{T}=-\frac{1}{V}\left(\frac{\partial V}{\partial P}\right)_{T}\,$

and $β S$ is the isentropic compressibility:

$\beta_{S}=-\frac{1}{V}\left(\frac{\partial V}{\partial P}\right)_{S}\,$

A corresponding expression for the difference in specific heat capacities (intensive properties) at constant volume and constant pressure is:

$c_p - c_v = \frac{\alpha^2 T}{\rho \beta_T}$

where ρ is the density of the substance under the applicable conditions.

The corresponding expression for the ratio of specific heat capacities remains the same since the thermodynamic system size-dependent quantities, whether on a per mass or per mole basis, cancel out in the ratio because specific heat capacities are intensive properties. Thus:

$\frac{c_{p}}{c_{v}}=\frac{\beta_{T}}{\beta_{S}}\,$

The difference relation allows one to obtain the heat capacity for solids at constant volume which is not readily measured in terms of quantities that are more easily measured. The ratio relation allows one to express the isentropic compressibility in terms of the heat capacity ratio.

[edit] Derivation

If an infinitesimal small amount of heat $δ Q$ is supplied to a system in a quasistatic way then, according to the second law of thermodynamics, the entropy change of the system is given by:

$dS = \frac{\delta Q}{T}\,$

Since

$\delta Q = C dT\,$

where C is the heat capacity, it follows that:

$T dS = C dT\,$

The heat capacity depends on how the external variables of the system are changed when the heat is supplied. If the only external variable of the system is the volume, then we can write:

$dS = \left(\frac{\partial S}{\partial T}\right)_{V}dT+\left(\frac{\partial S}{\partial V}\right)_{T}dV$

From this we see that:

$C_{V}=T\left(\frac{\partial S}{\partial T}\right)_{V}\,$

Expressing dS in terms of dT and dP similarly as above leads to the expression:

$C_{P}=T\left(\frac{\partial S}{\partial T}\right)_{P}\,$

We can find the above expression for $C P - C V$ by expressing dV in terms of dP and dT in the above expression for dS. We have

$dV = \left(\frac{\partial V}{\partial T}\right)_{P}dT+\left(\frac{\partial V}{\partial P}\right)_{T}dP\,$

which gives

$dS = \left[\left(\frac{\partial S}{\partial T}\right)_{V}+ \left(\frac{\partial S}{\partial V}\right)_{T}\left(\frac{\partial V}{\partial T}\right)_{P}\right]dT+\left(\frac{\partial S}{\partial V}\right)_{T}\left(\frac{\partial V}{\partial P}\right)_{T}dP$

and we see that:

$C_{P} - C_{V} = T\left(\frac{\partial S}{\partial V}\right)_{T}\left(\frac{\partial V}{\partial T}\right)_{P}=VT\alpha\left(\frac{\partial S}{\partial V}\right)_{T}\,$

The partial derivative $\left(\frac{\partial S}{\partial V}\right)_{T}$ can be rewritten in terms of variables that do not involve the entropy using a suitable Maxwell relation. These relations follow from the fundamental thermodynamic relation:

$dE = T dS - P dV\,$

It follows from this that the differential of the Helmholtz free energy $F = E - T S$ is:

$dF = -S dT - P dV\,$

This means that

$-S = \left(\frac{\partial F}{\partial T}\right)_{V}\,$

and

$-P = \left(\frac{\partial F}{\partial V}\right)_{T}\,$

The symmetry of second derivatives of F with respect to T and V then implies

$\left(\frac{\partial S}{\partial V}\right)_{T} =\left(\frac{\partial P}{\partial T}\right)_{V}\,$

allowing us to write:

$C_{P} - C_{V} = VT\alpha\left(\frac{\partial P}{\partial T}\right)_{V}\,$

The r.h.s. contains a derivative at constant volume, which can be difficult to measure. We can rewrite it as follows. In general, we have:

$dV= \left(\frac{\partial V}{\partial P}\right)_{T}dP+\left(\frac{\partial V}{\partial T}\right)_{P}dT\,$

Since the partial derivative $\left(\frac{\partial P}{\partial T}\right)_{V}$ is just the ratio of dP and dT for dV = 0, we can obtain this by putting dV = 0 in the above equation and solving for this ratio. We then obtain:

$\left(\frac{\partial P}{\partial T}\right)_{V}=-\frac{\left(\frac{\partial V}{\partial T}\right)_{P}}{\left(\frac{\partial V}{\partial P}\right)_{T}}=\frac{\alpha}{\beta_{T}}\,$

which yields the expression:

$C_{P} - C_{V}= V T\frac{\alpha^{2}}{\beta_{T}}\,$

The expression for the ratio of the heat capacities can be obtained as follows. We have:

$\frac{C_{P}}{C_{V}} = \frac{\left(\frac{\partial S}{\partial T}\right)_{P}}{\left(\frac{\partial S}{\partial T}\right)_{V}}\,$

The partial derivative in the numerator can be expressed as a ratio of partial derivatives of the pressure w.r.t. temperature and entropy. If in the relation

$dP = \left(\frac{\partial P}{\partial S}\right)_{T}dS+\left(\frac{\partial P}{\partial T}\right)_{S}dT\,$

we put $d P = 0$ and solve for the ratio $\frac{dS}{dT}$ we obtain $\left(\frac{\partial S}{\partial T}\right)_{P}$ . Doing so gives:

$\left(\frac{\partial S}{\partial T}\right)_{P}=-\frac{\left(\frac{\partial P}{\partial T}\right)_{S}}{\left(\frac{\partial P}{\partial S}\right)_{T}}\,$

We can similarly rewrite the partial derivative $\left(\frac{\partial S}{\partial T}\right)_{V}$ by expressing dV in terms of dS and dT, putting dV equal to zero and solving for the ratio $\frac{dS}{dT}$ . If we substitute that expression in the heat capacity ratio expressed as the ratio of the partial derivatives of the entropy above, we obtain:

$\frac{C_{P}}{C_{V}}=\frac{\left(\frac{\partial P}{\partial T}\right)_{S}}{\left(\frac{\partial P}{\partial S}\right)_{T}} \frac{\left(\frac{\partial V}{\partial S}\right)_{T}}{\left(\frac{\partial V}{\partial T}\right)_{S}}\,$

Taking together the two derivatives at constant S:

$\frac{\left(\frac{\partial P}{\partial T}\right)_{S}}{\left(\frac{\partial V}{\partial T}\right)_{S}} = \left(\frac{\partial P}{\partial T}\right)_{S}\left(\frac{\partial T}{\partial V}\right)_{S}=\left(\frac{\partial P}{\partial V}\right)_{S}\,$

Taking together the two derivatives at constant T:

$\frac{\left(\frac{\partial V}{\partial S}\right)_{T}}{\left(\frac{\partial P}{\partial S}\right)_{T}}=\left(\frac{\partial V}{\partial S}\right)_{T}\left(\frac{\partial S}{\partial P}\right)_{T}=\left(\frac{\partial V}{\partial P}\right)_{T}\,$

We can thus write

$\frac{C_{P}}{C_{V}}=\left(\frac{\partial P}{\partial V}\right)_{S}\left(\frac{\partial V}{\partial P}\right)_{T}=\frac{\beta_{T}}{\beta_{S}}\,$

[edit] Ideal gas

We now try to obtain an expression for $C_{P} - C_{V}\,$ for an ideal gas.

An ideal gas has the equation of state: $P V = n R T\,$

where

P = pressure

V = volume

n = number of moles

R = universal gas constant

T = temperature

The ideal gas equation of state can be easily arranged to give:

$V = n R T / P\,$ or $\, n R = V P / T$

The following partial derivatives are easily obtained from the above equation of state:

$\left(\frac{\partial V}{\partial T}\right)_{P}\ = \frac {n R}{P}\ = \left(\frac{V P}{T}\right)\left(\frac{1}{P}\right) = \frac{V}{T}$

$\left(\frac{\partial V}{\partial P}\right)_{T}\ = - \frac {n R T}{P^2}\ = - \frac {P V}{P^2}\ = - \frac{V}{P}$

The following simple expressions are obtained for thermal expansion coefficient $α$ :

$\alpha=\frac{1}{V}\left(\frac{\partial V}{\partial T}\right)_{P}\ = \frac{1}{V}\left(\frac{V}{T}\right)$

$\alpha= 1 / T \,$

and for isothermal compressibility $β T$ :

$\beta_{T}= - \frac{1}{V}\left(\frac{\partial V}{\partial P}\right)_{T}\ = - \frac{1}{V}\left( - \frac{V}{P}\right)$

$\beta_{T}= 1 / P \,$

We now calculate $C_{P} - C_{V}\,$ for ideal gases from the previously-obtained general formula:

$C_{P} - C_{V}= V T\frac{\alpha^{2}}{\beta_{T}}\ = V T\frac{(1 / T)^2}{1 / P} = \frac{V P}{T}$

Substituting from the ideal gas equation gives finally:

$C_{P} - C_{V} = n R\,$

where n = number of moles of gas in the thermodynamic system under consideration and R = universal gas constant. On a per mole basis, the expression for difference in molar heat capacities becomes simply R for ideal gases as follows:

$C_{P,m} - C_{V,m} = \frac{C_{P} - C_{V}}{n} = \frac{n R}{n} = R$

This result would be consistent if the specific difference were derived directly from the general expression for $c_p - c_v\,$ .

[edit] See also

Heat capacity ratio

[edit] References

David R. Gaskell (2003), Introduction to the thermodynamics of materials, Taylor & Francis. ISBN 1560329920

Contents

[edit] Derivation

[edit] Ideal gas

[edit] See also

[edit] References