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Relations between heat capacities

In thermodynamics, the heat capacity at constant volume, , and the heat capacity at constant pressure, , are extensive properties that have the magnitude of energy divided by temperature.

Relations edit

The laws of thermodynamics imply the following relations between these two heat capacities (Gaskell 2003:23):

 
 

Here   is the thermal expansion coefficient:

 

  is the isothermal compressibility (the inverse of the bulk modulus):

 

and   is the isentropic compressibility:

 

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

 

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:

 

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.

Derivation edit

If an infinitesimally small amount of heat   is supplied to a system in a reversible way then, according to the second law of thermodynamics, the entropy change of the system is given by:

 

Since

 

where C is the heat capacity, it follows that:

 

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:

 

From this follows:

 

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

 

One can find the above expression for   by expressing dV in terms of dP and dT in the above expression for dS.

 

results in

 

and it follows:

 

Therefore,

 

The partial derivative   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:

 

It follows from this that the differential of the Helmholtz free energy   is:

 

This means that

 

and

 

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

 

allowing one to write:

 

The r.h.s. contains a derivative at constant volume, which can be difficult to measure. It can be rewritten as follows. In general,

 

Since the partial derivative   is just the ratio of dP and dT for dV = 0, one can obtain this by putting dV = 0 in the above equation and solving for this ratio:

 

which yields the expression:

 

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

 

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

 

we put   and solve for the ratio   we obtain  . Doing so gives:

 

One can similarly rewrite the partial derivative   by expressing dV in terms of dS and dT, putting dV equal to zero and solving for the ratio  . When one substitutes that expression in the heat capacity ratio expressed as the ratio of the partial derivatives of the entropy above, it follows:

 

Taking together the two derivatives at constant S:

 

Taking together the two derivatives at constant T:

 

From this one can write:

 

Ideal gas edit

This is a derivation to obtain an expression for   for an ideal gas.

An ideal gas has the equation of state:  

where

P = pressure
V = volume
n = number of moles
R = universal gas constant
T = temperature

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

  or  

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

 
 

The following simple expressions are obtained for thermal expansion coefficient  :

 
 

and for isothermal compressibility  :

 
 

One can now calculate   for ideal gases from the previously obtained general formula:

 

Substituting from the ideal gas equation gives finally:

 

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:

 

This result would be consistent if the specific difference were derived directly from the general expression for  .

See also edit

References edit

  • David R. Gaskell (2008), Introduction to the thermodynamics of materials, Fifth Edition, Taylor & Francis. ISBN 1-59169-043-9.

relations, between, heat, capacities, this, article, needs, additional, citations, verification, please, help, improve, this, article, adding, citations, reliable, sources, unsourced, material, challenged, removed, find, sources, news, newspapers, books, schol. This article needs additional citations for verification Please help improve this article by adding citations to reliable sources Unsourced material may be challenged and removed Find sources Relations between heat capacities news newspapers books scholar JSTOR May 2013 Learn how and when to remove this template message In thermodynamics the heat capacity at constant volume C V displaystyle C V and the heat capacity at constant pressure C P displaystyle C P are extensive properties that have the magnitude of energy divided by temperature Contents 1 Relations 2 Derivation 3 Ideal gas 4 See also 5 ReferencesRelations editThe laws of thermodynamics imply the following relations between these two heat capacities Gaskell 2003 23 C P C V V T a 2 b T displaystyle C P C V VT frac alpha 2 beta T nbsp C P C V b T b S displaystyle frac C P C V frac beta T beta S nbsp Here a displaystyle alpha nbsp is the thermal expansion coefficient a 1 V V T P displaystyle alpha frac 1 V left frac partial V partial T right P nbsp b T displaystyle beta T nbsp is the isothermal compressibility the inverse of the bulk modulus b T 1 V V P T displaystyle beta T frac 1 V left frac partial V partial P right T nbsp and b S displaystyle beta S nbsp is the isentropic compressibility b S 1 V V P S displaystyle beta S frac 1 V left frac partial V partial P right S nbsp A corresponding expression for the difference in specific heat capacities intensive properties at constant volume and constant pressure is c p c v T a 2 r b T displaystyle c p c v frac T alpha 2 rho beta T nbsp where r 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 c p c v b T b S displaystyle frac c p c v frac beta T beta S nbsp 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 Derivation editIf an infinitesimally small amount of heat d Q displaystyle delta Q nbsp is supplied to a system in a reversible way then according to the second law of thermodynamics the entropy change of the system is given by d S d Q T displaystyle dS frac delta Q T nbsp Since d Q C d T displaystyle delta Q CdT nbsp where C is the heat capacity it follows that T d S C d T displaystyle TdS CdT nbsp 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 d S S T V d T S V T d V displaystyle dS left frac partial S partial T right V dT left frac partial S partial V right T dV nbsp From this follows C V T S T V displaystyle C V T left frac partial S partial T right V nbsp Expressing dS in terms of dT and dP similarly as above leads to the expression C P T S T P displaystyle C P T left frac partial S partial T right P nbsp One can find the above expression for C P C V displaystyle C P C V nbsp by expressing dV in terms of dP and dT in the above expression for dS d V V T P d T V P T d P displaystyle dV left frac partial V partial T right P dT left frac partial V partial P right T dP nbsp results in d S S T V S V T V T P d T S V T V P T d P displaystyle 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 nbsp and it follows S T P S T V S V T V T P displaystyle left frac partial S partial T right P left frac partial S partial T right V left frac partial S partial V right T left frac partial V partial T right P nbsp Therefore C P C V T S V T V T P V T a S V T displaystyle 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 nbsp The partial derivative S V T displaystyle left frac partial S partial V right T nbsp 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 d E T d S P d V displaystyle dE TdS PdV nbsp It follows from this that the differential of the Helmholtz free energy F E T S displaystyle F E TS nbsp is d F S d T P d V displaystyle dF SdT PdV nbsp This means that S F T V displaystyle S left frac partial F partial T right V nbsp and P F V T displaystyle P left frac partial F partial V right T nbsp The symmetry of second derivatives of F with respect to T and V then implies S V T P T V displaystyle left frac partial S partial V right T left frac partial P partial T right V nbsp allowing one to write C P C V V T a P T V displaystyle C P C V VT alpha left frac partial P partial T right V nbsp The r h s contains a derivative at constant volume which can be difficult to measure It can be rewritten as follows In general d V V P T d P V T P d T displaystyle dV left frac partial V partial P right T dP left frac partial V partial T right P dT nbsp Since the partial derivative P T V displaystyle left frac partial P partial T right V nbsp is just the ratio of dP and dT for dV 0 one can obtain this by putting dV 0 in the above equation and solving for this ratio P T V V T P V P T a b T displaystyle 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 nbsp which yields the expression C P C V V T a 2 b T displaystyle C P C V VT frac alpha 2 beta T nbsp The expression for the ratio of the heat capacities can be obtained as follows C P C V S T P S T V displaystyle frac C P C V frac left frac partial S partial T right P left frac partial S partial T right V nbsp 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 d P P S T d S P T S d T displaystyle dP left frac partial P partial S right T dS left frac partial P partial T right S dT nbsp we put d P 0 displaystyle dP 0 nbsp and solve for the ratio d S d T displaystyle frac dS dT nbsp we obtain S T P displaystyle left frac partial S partial T right P nbsp Doing so gives S T P P T S P S T displaystyle 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 nbsp One can similarly rewrite the partial derivative S T V displaystyle left frac partial S partial T right V nbsp by expressing dV in terms of dS and dT putting dV equal to zero and solving for the ratio d S d T displaystyle frac dS dT nbsp When one substitutes that expression in the heat capacity ratio expressed as the ratio of the partial derivatives of the entropy above it follows C P C V P T S P S T V S T V T S displaystyle 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 nbsp Taking together the two derivatives at constant S P T S V T S P T S T V S P V S displaystyle 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 nbsp Taking together the two derivatives at constant T V S T P S T V S T S P T V P T displaystyle 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 nbsp From this one can write C P C V P V S V P T b T b S displaystyle 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 nbsp Ideal gas editThis is a derivation to obtain an expression for C P C V displaystyle C P C V nbsp for an ideal gas An ideal gas has the equation of state P V n R T displaystyle PV nRT nbsp where P pressure V volume n number of moles R universal gas constant T temperatureThe ideal gas equation of state can be arranged to give V n R T P displaystyle V nRT P nbsp or n R P V T displaystyle nR PV T nbsp The following partial derivatives are obtained from the above equation of state V T P n R P V P T 1 P V T displaystyle left frac partial V partial T right P frac nR P left frac VP T right left frac 1 P right frac V T nbsp V P T n R T P 2 P V P 2 V P displaystyle left frac partial V partial P right T frac nRT P 2 frac PV P 2 frac V P nbsp The following simple expressions are obtained for thermal expansion coefficient a displaystyle alpha nbsp a 1 V V T P 1 V V T displaystyle alpha frac 1 V left frac partial V partial T right P frac 1 V left frac V T right nbsp a 1 T displaystyle alpha 1 T nbsp and for isothermal compressibility b T displaystyle beta T nbsp b T 1 V V P T 1 V V P displaystyle beta T frac 1 V left frac partial V partial P right T frac 1 V left frac V P right nbsp b T 1 P displaystyle beta T 1 P nbsp One can now calculate C P C V displaystyle C P C V nbsp for ideal gases from the previously obtained general formula C P C V V T a 2 b T V T 1 T 2 1 P V P T displaystyle C P C V VT frac alpha 2 beta T VT frac 1 T 2 1 P frac VP T nbsp Substituting from the ideal gas equation gives finally C P C V n R displaystyle C P C V nR nbsp 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 C P C V n n R n R displaystyle C P m C V m frac C P C V n frac nR n R nbsp This result would be consistent if the specific difference were derived directly from the general expression for c p c v displaystyle c p c v nbsp See also editHeat capacity ratioReferences editDavid R Gaskell 2008 Introduction to the thermodynamics of materials Fifth Edition Taylor amp Francis ISBN 1 59169 043 9 Retrieved from https en wikipedia org w index php title Relations between heat capacities amp oldid 1173198590, wikipedia, wiki, book, books, library,

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