Thermodynamic Properties

Pure Component Constants

Pure component constants are tabulated by SuperPro Designer in databases, referred to as Physical Properties Databases. In particular, the following three sources of pure component constants are supported:

      the internal database (‘Designer’)

      the Design Institute for Physical Property Research (DIPPR) database

      a user specified database (‘User’)

At present, the following pure component constants:

      Molecular Weight

      Critical Properties (i.e., Critical Pressure, Critical Temperature, Critical Compressibility Factor and Pitzer’s Acentric Factor)

      Standard Gibbs Energy of Formation as an ideal gas at 298.15 K and 1 atm.

      Normal Boiling Point

      Normal Freezing Point

      Liquid density coefficients

      Antoine vapor pressure coefficients

      Ideal gas heat capacity coefficients

      Liquid/solid heat capacity at constant pressure

It is worth noting that the values of pure component constants may sometimes vary between sources as they might have been estimated by different methodologies (with significantly different accuracies) .

Pure component constants (e.g., critical parameters, activity coefficients, Antoine coefficients, enthalpies of vaporization etc.) consist the backbone of VLE modeling.They are essential parameters for the estimation of pure component as well as mixture properties (e.g., K-values, densities, enthalpies) by thermodynamic models (e.g, Raoult’s Law, EOS, etc.). For details, please see the following sections Thermodynamic Properties of Pure Components and Thermodynamic Properties of Mixtures

Thermodynamic Properties of Pure Components

Density

      Vapor Density

The density (molar volume) of a pure vapor component is calculated by the formula

PureComponentVaporDensityEOS.jpg 

eq. (D.1)

where P is the pressure, R is the gas constant, T is the temperature and Z is the compressibility factor. In the present version of SuperPro, Z=1, or any other words, the vapor is a assumed to behave as an ideal gas.

      Liquid Density

The density of a pure liquid component is calculated as a linear function of temperature

PureComponentLiquidDensityEOS.jpg 

eq. (D.2)

Heat Capacity

      Vapor Heat Capacity

The heat capacity of vapor components is calculated as an ideal gas heat capacity by the following third degree polynomial

PureCompIGHeatCapacity.jpg 

eq. (D.3)

where the values of the coefficients a, b, c and d are the pure component constants stored in the physical properties database.

      Liquid Heat Capacity

The liquid heat capacity of a pure component is considered tobe independent of the temperature, therefore:

PureCompLiquidHeatCapacity.jpg 

eq. (D.4)

where a is a constant stored in the physical properties database.

Enthalpy

      Vapor Enthalpy

The enthalpy of a pure component in the vapor phase is calculated (under the assumption of the ideal gas behavior) by the following integral:

PureCompVaporEnthalpy.jpg 

eq. (D.5)

where TREF is the reference temperature for enthalpy calculations (i.e., the temperature where the enthalpy value is assumed to be zero). The reference temperature is considered a variable of the process file and can be edited by right clicking anywhere in a process file and selecting Ambient, Standard and Enthalpy Ref. Conditions.

      Liquid Enthalpy

The enthalpy of a pure component in the liquid phase is calculated by:

PureCompLiquidEnthalpy.jpg 

eq. (D.6)

Notice that the effect of pressure on the enthalpy (i.e., the residual enthalpy) of vapor and liquid components is not currently taken into account in the calculations. This feature will be implemented in a future release of SuperPro.

Enthalpy OF Vaporization

SuperPro calculates the enthalpy of vaporization of a component at a given temperature, T, by the following empirical correlation:

PureCompVaporizationEnthalpy.jpg 

eq. (D.7)

where a is:

EnthalpyofVaporization_aTerm.jpg 

 

 

eq. (D.8)

EnthalpyofVaporization_bTerm.jpg 

eq. (D.9)

and b is calculated by the generalized Watson correlation (Viswanath and Kuloor, 1967):

Finally ,the enthalpy of vaporization at the normal boiling point of the component is calculated by Chen’s correlation (Chen, 1965)

ChensCorrelation.jpg 

eq. (D.10)

where Tb is the boiling point of the component, Tbr=Tb/Tc is the reduced boiling point and Tc, Pc are the critical temperature and pressure, respectively.

Saturation Vapor Pressure

The saturation vapor pressure of a component at temperature T, is calculated by the Antoine equation:

PureCompVaporSatPressAntoine.jpg 

eq. (D.11)

where A, B and C are the Antoine coefficients stored in the SuperPro database.

Fugacity

By definition, the fugacity, f, of a pure component is equal to the product of pressure times the species fugacity coefficient, φ:

PureCompFugacity.jpg 

eq. (D.12)

where φ is calculated by the following integral:

PureCompFugacityCoeff.jpg 

eq. (D.13)

The term Z in the above equation denotes the compressibility factor which is calculated by the solution of an appropriate cubic EOS. Notice that for most EOS the integral part can be analytically evaluated and so there is no need to apply a numerical integration rule.

Thermodynamic Properties of Mixtures

Density

      Vapor Density

The density (molar volume) of a vapor mixture is calculated by the formula:

MixtureVaporDensityEOS.jpg 

eq. (D.14)

where Z is the compressibility factor. In the present version of SuperPro, Z=1 (ideal gas assumption).

      Liquid Density

The liquid density of mixtures is calculated by the ideal mixture model as:

MixtureLiquidDensity.jpg 

eq. (D.15)

where nc is the number of components in the mixture, λi are weight factors (volumetric contribution coefficients) and ρL,i are the pure component liquid densities.

Heat Capacity

      Vapor Heat Capacity

The heat capacity of a vapor mixture is calculated, under the ideal mixture assumption, as the molar fraction weighted average of pure component ideal gas heat capacities:

MixtureIGHeatCapacity.jpg 

eq. (D.16)

where yi are their molar fractions of the mixture components and inset_0.jpg are the pure-component heat capacities.

      Liquid Heat Capacity

The heat capacity of a liquid mixture is calculated as the molar fraction weighted average of pure component liquid heat capacities:

MixtureLiquidHeatCapacity.jpg 

eq. (D.17)

Enthalpy

      Vapor Enthalpy

The enthalpy of a vapor mixture is calculated as the molar fraction weighted average of pure component vapor enthalpies.

MixtureVaporEnthalpy.jpg 

eq. (D.18)

where nc is the number of components in the mixture, yi are the molar fractions of the mixture components and hV,i(T) are the pure species vapor enthalpies. Currently, the effect of the pressure on the enthalpy is neglected. The contribution of residual enthalpy will be implemented in a future release of SuperPro.

 

      Liquid Enthalpy

The enthalpy of a liquid mixture is calculated as the molar fraction weighted average of pure component liquid enthalpies.

MixtureLiquidEnthalpy.jpg 

eq. (D.19)

where nc is the number of components in the mixture, xi are the molar fractions of the mixture components and hL,i(T) are the pure species liquid enthalpies.

Partial Fugacity

      Vapor Partial Fugacity

The vapor partial fugacity of species i in a mixture, inset_1.jpg, is defined as:

ComponentVaporPartialFugacity.jpg 

eq. (D.20)

where yi is the molar fraction of species i in the mixture and inset_2.jpg is the partial fugacity coefficient, calculated by the integral:

ComponentVaporPartialFugCoeff.jpg 

eq. (D.21)

 

      Liquid Partial Fugacity

The liquid partial fugacity of species i in a mixture, inset_3.jpg, of a vapor mixture is defined as:

ComponentLiquidPartialFugacity.jpg 

eq. (D.22)

where xi is the molar fraction of species i in the mixture and inset_4.jpg is the partial fugacity coefficient, calculated by the integral:

ComponentLiquidPartialFugCoeff.jpg 

eq. (D.23)

The term Z in and is the compressibility factor, calculated by the solution of an appropriate cubic EOS: the maximum of the three roots obtained is used in while the minimum root is used for . Notice that for most EOS the integral part can be analytically evaluated and so there is no need to apply a numerical integration rule.

Phase Equilibrium Ratio (K-Value)

A phase-equilibrium ratio is the ratio of molar fractions of a species in the two phases at equilibrium at a given temperature and pressure. For vapor/liquid systems, the constant is referred to as the K-value or vapor/liquid equilibrium ratio:

PhaseEquilibriumRatio.jpg 

eq. (D.24)

where xi and yi are the molar fractions of component i in the liquid and vapor phase, respectively.

SuperPro supports the following thermodynamic models for the calculation of the K-value.

 

 

      Raoult’s Law

The Raoult’s Law assumes ideal behavior for the vapor and liquid phase of the mixture. Under this assumption, the K-value of component i is given by:

ComponentKvalueRaoultLaw.jpg 

eq. (D.25)

where inset_5.jpg is the saturation vapor pressure of the pure component i (see Saturation Vapor Pressure), calculated by the Antoine correlation. Notice that with Raoult’s Law, the K-values are independent of the composition of the vapor and liquid phase (i.e., the molar fractions xi and yi). In the case that Antoine coefficients are not available for certain components, SuperPro Designer offers the possibility to bypass the calculation of their K-values by directly setting an expected vapor fraction for them (i.e., the fraction of the component that is expected to be in the vapor phase). This form of hybrid model is only available with Raoult’s Law.

      Modified Raoult’s Law

The Modified Raoult’s Law assumes an ideal vapor phase and a non-ideal liquid phase. The K-value of component i is given by:

ComponentKvalueModRaoultLaw.jpg 

eq. (D.26)

where inset_6.jpg is the saturation vapor pressure and γL,i is the liquid activity coefficient of component i. Activity coefficients are calculated by an appropriate activity coefficient model (see Activity Coefficient Models).

      Equation of State (EOS)

The EOS expression of the K-value is:

ComponentKvalueEOS.jpg 

eq. (D.27)

where inset_7.jpg and inset_8.jpg are the partial fugacity coefficients of species i in the liquid and in the vapor phase, respectively. As explained previously, the partial fugacity coefficients are calculated according to a selected EOS model (see Equations Of State (EOS)).

The employment EOS of state models is a thermodynamically consistent way of calculating the fugacity coefficients of components in the vapor and liquid phase. For example, EOS models have been traditionally used for non-polar mixtures (i.e. hydrocarbons and light gases) at all pressure ranges and for polar mixtures at low pressures only. However, simple EOS models are accurate only in cases of mixtures without strong, special interactions between the molecules of their constituent components. EOS models are known to produce inaccurate results for the liquid phase of mixtures with polar compounds (e.g., acetone+ methanol). This problem is dealt with by the employment of gamma-phi (activity coefficient) models.

      Gamma-Phi Model

The gamma-phi expression of the K-value combines an EOS for the estimation of the vapor phase partial fugacity coefficient and an activity coefficient model for the estimation of the liquid phase partial fugacity coefficient in the liquid phase:

ComponentKvalueGammaPhi.jpg 

eq. (D.28)

where γi is the activity coefficient of component i and inset_9.jpg is the liquid fugacity coefficient of the pure component. The activity coefficients are calculated by an appropriate activity coefficient model (see Activity Coefficient Models).