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ANSYS Fluent Turbulence Modeling

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ANSYS Fluent Turbulence Modeling :: RANS, LES, DES, and Hybrid Approaches

ANSYS Fluent provides many turbulence models. They range from RANS (Reynolds-averaged) to DNS (direct numerical simulation). Hybrid RANS/LES (DES, SAS) bridges the gap between scale-resolving and scale-modeling approaches. This note catalogs all available turbulence models. It includes their governing equations, assumptions, recommended applications, and comparison with OpenFOAM equivalents.

RANS Turbulence Models

ModelEquationsClosed VariablesDefault DiffusionBest For
----------------------------------------------------------------
Spalart-Allmaras1ν̃PrandtExternal aerodynamics, boundary layers
Standard k-epsilon2 (k, epsilon)σₖ, σεStandardIndustrial, high-Re, attached flows
RNG k-epsilon2 (k, epsilon)Modified RNG theoryRNG enhancedModerate swirl, high strain
Realizable k-epsilon2 (k, epsilon)Modified CμModified turbulence diffusivityJet flows, boundary layers with pressure gradient
Reynolds Stress Model (RSM)7 (6 RNG + k)Full stress tensor transportFull differential pressureStrong swirl, rotating flows, secondary flow
v2-f5 (k, epsilon, v, f)Near-wall correctionNear-wall v²-f modelNear-wall attached flows with strong curvature
k-omega SST2 (k, omega)Blended k-epsilon/k-omegaShear stress transportGeneral engineering, adverse pressure gradients, separation

Spalart-Allmaras

The one-equation model targets external aerodynamics (aerofoil, aircraft). It solves a transport equation for a modified eddy viscosity ν̃ (related to actual turbulent viscosity νₜ):

where $P_{\tilde{\nu}}$ is production and $D_{\tilde{\nu}}$ is destruction/dissipation.

Turbulent viscosity comes from $\tilde{\nu}$:

with $f_{v1}$ a damping function. It vanishes near walls.

Fluent implementation: Spalart-Allmaras model. Skip low-Re correction. The model works on y₊ ≈ 1 walls. Users typically apply wall functions (y₊ ≈ 30–300).

RNG k-epsilon

The RNG $k$-$\epsilon$ model derives from Renormalization Group (RNG) theory. It modifies the standard $k$-$\epsilon$ equations. It incorporates small-scale turbulence effects analytically. Key differences from Standard $k$-$\epsilon$:

1. New term in the $\epsilon$-equation improves accuracy for high strain rates and moderate swirl 2. $C_\mu$ is no longer constant. It depends on the dimensionless strain rate:

Where $P_{ij}$ is production, $D_{ij}$ is diffusion, $\Pi_{ij}$ is pressure-strain correlation, and $\epsilon_{ij}$ is dissipation. A model handles the pressure-strain term (usually Rotta + Daly-Harlow closure).

Fluent RSM is the most complete RANS model (second-moment closure). It is also the most expensive (9 equations total: 7 transport + 2 for k and $\epsilon$). It converges significantly worse than two-equation models.

k-omega SST (Shear Stress Transport)

Use k-omega SST as the default RANS model for general engineering in Fluent. It blends the $k$-$\omega$ model near the wall with the $k$-$\epsilon$ model in the free stream. The $k$-$\omega$ model has correct near-wall asymptotic behavior. The $k$-$\epsilon$ model works better in the free stream (where $k$-$\omega$ is over-sensitive).

The blending function approaches 1 (pure $k$-$\omega$) near walls and 0 (pure $k$-$\epsilon$) in the free stream. The SST modification adds a limiter on eddy viscosity. This prevents over-prediction of turbulent shear stress:

where $\alpha$ is a blending function. This limiter makes k-omega SST superior to standard $k$-$\omega$ for adverse pressure gradient flows.

Fluent implementation: kOmegaSST model. Omega at walls defaults to $S\frac{\nu}{\beta_1 y^2}$, where $S$ is the specific rotation rate and $y$ is near-wall distance.

LES (Large Eddy Simulation)

Fluent's LES solves filtered Navier-Stokes equations with an SFS (SubFilter-Scale) model. Available SFS models:

ModelDescription
--------------------
SmagorinskyClassic eddy-viscosity model (constant Cs)
Dynamic SmagorinskyDynamically computed Cs via test-filter
WALE (Wall-Adapting Local Eddy-viscosity)Improved near-wall behavior; no damping needed
VremanSimilar to WALE, slightly different formulation

LES in Fluent needs:

Use the WALE model for LES with Fluent. It provides correct near-wall scaling. It needs no damping functions:

where $S_{ij}^d$ is the symmetric part of the squared velocity gradient.

DES / DDES / SAS (Hybrid RANS/LES)

Fluent supports these hybrid RANS/LES approaches:

ModelDescription
--------------------
SST-DESDelayed Eddy Simulation using SST-RANS away from wall, LES in separated regions
SST-DDESDelayed DES (avoids LES buffer layer issues near walls)
SST-SASScale-Adaptive Simulation (RANS model with SAS term for enhanced LES behavior in unsteady regions)
IDDESImproved DDES (includes near-wall modeling capability)

Summary (ANSYS vs OpenFOAM)

Model/ModelANSYS FluentOpenFOAM Equivalent
---------------------------------------------
k-omega SSTkOmegaSST (RANS)kOmegaSST, kOmegaSSTIDDES
k-epsilon (Standard)StandardKEpsilonkEpsilon
k-epsilon (RNG)RNGKEpsilonRNGkEpsilon (available via kEpsilon model selection)
k-epsilon (Realizable)RealizableKEpsilonRealizableKEpsilon
Reynolds Stress Model (RSM)ReynoldsStressModelRASModel with RSM
Spalart-AllmarasSpalartAllmarasSpalartAllmaras
Smagorinsky (LES)SmagorinskySmagorinsky
Dynamic Smagorinsky (LES)DynamicSmagorinskyDynamicSmagorinsky
WALE (LES)WALESWALES
SASSSTSASkOmegaSSTSAS
SST-DESSSTDESDES
SST-DDESSSTDDESDDES
SST-IDDESSSTIDDESIDDES

See Also