RNG K-Epsilon Turbulence

The RNG K-Epsilon model is a two-equation turbulence model that solves transport equations for the turbulent kinetic energy k and the turbulent dissipation rate ε to provide closure of the Reynolds-Averaged Navier-Stokes equations.

Yakhot and others [818] applied a statistical technique called Re-Normalisation Group (RNG) theory to the Navier-Stokes equations. The RNG theory accommodates the fact that eddies of different length scales contribute to turbulence. It accounts for these different scales in a global manner whilst calculating the dissipation rather than relying on a single turbulence scale.

The RNG model, as originally proposed, takes no explicit account of compressibility or buoyancy effects. In Simcenter STAR-CCM+, however, these effects are modeled as in the Standard K-Epsilon model.

Relation for Turbulent Viscosity

The turbulent eddy viscosity μ t is calculated as:

Figure 1. EQUATION_DISPLAY
μ t = ρ C μ k T
(4060)

where:

The turbulent time scale T is calculated as:

T T with Realizable Scale Option
Figure 2. EQUATION_DISPLAY
max ( T e , C t ν ε )
(4061)
Figure 3. EQUATION_DISPLAY
max ( min ( T e , C T C μ f μ S ) , C t ν ε )
(4062)

where:

Transport Equation

The transport equations for the kinetic energy k and the turbulent dissipation rate ε are:

Figure 4. EQUATION_DISPLAY
t ( ρ k ) + ∇⋅ ( ρ k v ¯ ) = ∇⋅ [ ( μ + μ t σ k ) k ] + P k ρ ( ε ε 0 ) + S k
(4063)
Figure 5. EQUATION_DISPLAY
t ( ρ ε ) + ∇⋅ ( ρ ε v ¯ ) = ∇⋅ [ ( μ + μ t σ ε ) ε ] + 1 T e C ε 1 P ε C ε 2 ρ ( ε T e ε 0 T 0 ) C ε 4 ρ ε ∇⋅ v ¯ + S R N G + S ε
(4064)

where:

  • v ¯ is the mean velocity.
  • μ is the dynamic viscosity.
  • σ k , σ ε , C ε 1 , C ε 2 , and C ε 4 are Model Coefficients.
  • ε 0 is the ambient turbulence value in the source terms that counteracts turbulence decay [316]. The possibility to impose an ambient source term also leads to the definition of a specific time-scale T 0 that is given by Eqn. (1170).
  • P k and P ε are Production Terms.
  • S k and S ε are the user-specified source terms.

S R N G in Eqn. (4064) represents the effect of mean flow distortion on turbulence and is defined as:

Figure 6. EQUATION_DISPLAY
S R N G = C μ η 3 ( 1 η / η 0 ) 1 + β η 3 ρ ε 2 k
(4065)

where:

Production Terms

The production terms P k and P ε are defined as:

Figure 7. EQUATION_DISPLAY
P k = G k + G n l + G b ϒ M
(4066)
Figure 8. EQUATION_DISPLAY
P ε = G k + G n l + C ε 3 G b
(4067)

where:

Model Coefficients

C M (Sarkar) C t C T C ε 1 C ε 2 C ε 4 C μ β σ ε σ k
2 1 0.6 1.42 1.68 0.387 0.085 0.012 0.719 0.719
C ε 3

The available literature is not clear as to the specification of this coefficient. By default, it is computed according to [305] as:

Figure 9. EQUATION_DISPLAY
C ε 3 = tanh | v b | | u b |
(4068)

where v b and u b are the velocity components parallel and perpendicular to the gravitational vector g .

This formulation tends to set the coefficient to zero outside natural convection boundary layers.

Alternatively, C ε 3 can be taken as constant everywhere, or specified depending on the buoyancy production term G b as follows:

Figure 10. EQUATION_DISPLAY
C ε 3 = { 1    for  G b 0 0    for  G b < 0
(4069)