Real Gas Models Reference

Real Gas models allow you to take into account non-ideal behavior such as compressibility effects, variable specific heat, van der Waals forces, and non-equilibrium thermodynamic effects.

The following Real Gas models are available in STAR-CCM+:

  • Peng-Robinson—for use at high pressures and low temperatures
  • Redlich-Kwong—for use at high pressures and low temperatures
  • Soave-Redlich-Kwong—for more complex treatment of temperature
  • Modified Soave-Redlich-Kwong—designed to handle phase equilibrium calculations for non-polar molecules ([173], [174])
  • Van der Waals—designed to handle intermolecular attractive forces
  • Equilibrium Air—for high temperatures, to handle effects such as ionization. This model is useful for the simulation of hypersonic flows, such as nozzle flows or atmospheric re-entry.
  • IAPWS-IF97 Steam (for steam)—for this model, the material properties follow the IAPWS-IF97 specification [25], [26], [27].
Model Names and Abbreviations Peng-Robinson PR
Redlich-Kwong RK
Soave-Redlich-Kwong SRK
Modified Soave-Redlich-Kwong mSRK
Van der Waals VdW
Equilibrium Air EA
IAPWS-IF97 (Steam) IAPWS-s
Theory
Provided by Continua > [physics continuum] > Models > Real Gas Equation of State
Example Node Path Continua > Physics 1 > Models > Peng-Robinson
Requires Equation of State: Real Gas
Properties
Activates Model Controls (child nodes)
Materials See Real Gas Material Properties.
Monitors Vib. Energy
Field Functions See Field Functions.

Real Gas Material Properties

This table shows which material properties are used by which real gas models.

PR RK SRK mSRK VdW EA IAPWS-s
Acentric Factor ω
Critical Pressure p c
Critical Temperature T c
Fugacity Coefficient
Molecular Weight
Saturation Pressure
Saturation Temperature
Specific Heat
Speed of Sound
Acentric Factor
Critical Pressure
Displays the model constant p c (read-only).
Critical Temperature
Displays the model constant T c (read-only).
Fugacity Coefficient
The ratio of the fugacity and the partial pressure of gas mixture component i . ϕ i in Eqn. (81). The coefficient is 1 for ideal gases.
Molecular Weight
Specifies the molecular weight M .
Saturation Pressure
Specifies the saturation pressure.
Saturation Temperature
Specifies the temperature for the corresponding saturation pressure at which the liquid boils into its vapor phase.
Specific Heat
Specifies the fluid-specific heat capacity C p .
Method Corresponding Method Node
Constant (SRK, mSRK, PR, RK, VdW)
Constant
Specifies the specific heat using a scalar profile value.
Equilibrium Air (EA)
Equilibrium Air
This node provides no properties.
Fully Excited (TNEq)
Fully Excited
This node provides no properties.
Gas Kinetics (SRK, mSRK, PR, RK, VdW)

Uses the Gas Kinetics Method for Specific Heat.

Gas Kinetics
This node provides no properties.

Selecting the Gas Kinetics method adds the following material properties:

Electronic Partition Function
Specifies the partition function for electronic energy using a Number of Modes with Characteristic Temperatures θ i and Mode Degeneracies g i . See Q e l in Eqn. (163).
Molecule Type
Describes the molecular structure using the following values:
  • 0: atom
  • 1: linear molecule
  • 2: non-linear molecule
Standard State Temperature
Specifies the temperature at which the standard state of the fluid is defined. The Standard State Temperature is used to calculate enthalpy. The enthalpy value varies with Standard State Temperature, but in direct proportion, so differences in enthalpy remain the same for different values of Standard State.
Vibrational Partition Function
For polyatomic molecules, specifies the partition function for vibrational energy using a Number of Modes with Characteristic Temperatures θ i and Mode Degeneracies g i . See Q v i b in Eqn. (163).
IAPWS-IF97 (IAPWS-s)
IAPWS-IF97
This node provides no properties.
Polynomial in T (PR, RK, SRK, mSRK, VdW)
Polynomial in T
See Using Polynomial in T.

Selecting the Polynomial in T method adds the following material property:

Standard State Temperature
As for Gas Kinetics.
Table, Cp(T) (PR, RK, SRK, mSRK, VdW)

Tabulates specific heat as a function of temperature.

Table, Cp(T)
See Using Table(T).
Thermodynamic Polynomial Data (SRK, mSRK, PR, RK, VdW)
Thermodynamic Polynomial Data
See Using Thermodynamic Polynomial Data.
Speed of Sound
Specifies the rate of acoustic propagation in the medium using one of the following methods:
Method Corresponding Method Node
Equilibrium Air (EA)
Equilibrium Air
This node provides no properties.
IAPWS-IF97 (IAPWS-s)
IAPWS-IF97
This node provides no properties.

Field Functions

The following table shows which field functions become available for which real gas model:

PR RK SRK mSRK VdW EA IAPWS-s
Compressibility Factor
Critical Pressure
Critical Temperature
Entropy
Entropy Function
Gas Constant
IAPWS Region ID
Mach Number
Molecular Weight
Ratio of Specific Heats
Real Gas Specific Heat
Reduced Pressure
Reduced Temperature
Relative Mach Number
Saturation Pressure
Saturation Temperature
Speed of Sound
Compressibility Factor
Represents the amount of deviation of the real gas from an ideal gas, expressed as Z = p / ( ρ R T ) . This factor usually takes on values around 1.

For the Equilibrium Air model, the compressibility factor represents the degree of dissociation, which is non-ideal behavior, but has values that vary more widely (approximately between 1 and 6). A simplified formula that applies to the equilibrium air model is given as Eqn. (686).

Critical Pressure
Expressed as p c .
Critical Temperature
Expressed as T c .
Entropy
See Entropy.
Entropy Function
See Entropy Function.
Gas Constant
The specific gas constant.
IAPWS Region ID
Data that Simcenter STAR-CCM+ calculates for a particular IAPWS validity region.
Mach Number
The local Mach number.
Molecular Weight
The molecular weight as specified for the material.
Ratio of Specific Heats
Expressed as:

γ = C p C v = C p ( C p - R )

where C p is specific heat J/(kg K), and R is a specific gas constant J/(kg K).

Real Gas Specific Heat
The value of specific heat at constant pressure of the real gas. This field function accounts for the effects of variations in both temperature and pressure by including the departure from the ideal gas value. The last three terms on the right-hand side of Eqn. (192) give the departure from ideal:
Figure 1. EQUATION_DISPLAY
C p = C p 0 + T v ( 2 P T 2 ) v d ν T ( P T ) v 2 ( P v ) T - 1 - R
(192)
Reduced Pressure
Expressed as p r = p / p c .
Reduced Temperature
Expressed as T r = T / T c .
Relative Mach Number
Saturation Pressure
The saturation pressure as specified for the material.
Saturation Temperature
The saturation temperature as specified for the material.
Speed of Sound
The rate of acoustic propagation in the medium.