Wall Treatment Models Reference

The Wall Treatment models allow you to set near-wall modeling assumptions for turbulence models.

Models Overview

Model Names and Abbreviations High y+ Wall Treatment High y+
Low y+ Wall Treatment Low y+
All y+ Wall Treatment* All y+
Two-Layer All y+ Wall Treatment* 2L All y+
Theory See Theory Guide—Wall Treatment for Turbulence.
Provided By
  • [physics continuum] > Models > Wall Treatment
Example Node Path Continua > Physics 1 > Models > All y+ Wall Treatment
Requires
  • Space: Axisymmetric, Two Dimensional, or Three Dimensional
  • Material: Gas, Liquid, Multiphase, Multi-Component Gas, or Multi-Component Liquid
  • Viscous Regime: Turbulent
  • Turbulence: See Turbulence Models Lookup.
Properties See Properties Lookup.
Activates Boundary Inputs See Boundary Settings.
Region Inputs See Region Settings.
Field Functions
  • Ustar
  • Virtual Local Heat Transfer Coefficient
  • Wall y+
See Field Functions.

Turbulence Models Lookup

High y+ Low y+ All y+ 2L All y+
Detached Eddy Simulation EB K-Epsilon Detached Eddy
SST (Menter) K-Omega Detached Eddy
Spalart-Allmaras Detached Eddy
Large Eddy Simulation Dynamic Smagorinsky Subgrid Scale
Smagorinsky Subgrid Scale
WALE Subgrid Scale
Reynolds-Averaged Navier-Stokes K-Epsilon Turbulence EB K-Epsilon
Lag EB K-Epsilon
Realizable K-Epsilon
Realizable K-Epsilon Two-Layer
Standard K-Epsilon
Standard K-Epsilon Low-Re
Standard K-Epsilon Two-Layer
K-Omega Turbulence SST (Menter) K-Omega
Standard (Wilcox) K-Omega
Reynolds Stress Turbulence Elliptic Blending
Linear Pressure Strain
Linear Pressure Strain Two-Layer
Quadratic Pressure Strain
Spalart-Allmaras Turbulence Standard Spalart-Allmaras

Properties Lookup

High y+ Low y+ All y+ 2L All y+
Iterative Ustar
When On, this property allows iterative computation of the reference velocity u * from the wall law. When this property is Off, the reference velocity u * is computed according to the specific turbulence model.

Boundary Settings

NoteBoundary types that do not require setting any conditions or values are not listed.
Domain Boundaries

The following boundary conditions and values are equal to all boundaries of type:

  • Wall
  • Baffle Boundary
  • Porous Baffle Boundary
  • Contact Interface Boundary
  • Mapped Contact Boundary
Blended Wall Function (All y+, 2L All y+)
Added to the Values node on no-slip walls when the all-y+ or the two-layer all-y+ wall treatment is selected. You need to specify two scalar values:
  • E: The log law offset.
  • Kappa: The von Karman constant.
Standard Wall Function (High y+)
Added to the Values node on no-slip walls when the high-y+ wall treatment is selected. The values you need to specify are equal to the Blended Wall Function.
Wall Surface Specification
Controls whether the boundary is smooth or rough.
MethodCorresponding Value Nodes
Smooth

Regular wall treatment without modification for wall roughness.

None.
Rough

Modification of wall treatment to incorporate roughness using data correlation.

Calculates a roughness function f , which modifies the log law offset E using Eqn. (1604). f is calculated from the specified equivalent sand-grain roughness height r and wall roughness parameters using Eqn. (1639) and Eqn. (1640).

NoteThis method limits the roughness height by the wall distance of the wall-adjacent cell. Simcenter STAR-CCM+ returns the number of faces on which the roughness height is limited in the Output window.
Roughness Height
Scalar profile value to specify r.

You obtain the roughness height that is appropriate for your model either from the literature or empirically. To determine r from an experiment:

  • Measure the friction factor for the Reynolds number of your case in the experiment.
  • Plot your measurements on a Moody diagram.
  • Deduce the equivalent sand-grain roughness height from the Moody diagram curve.
Roughness Model Parameters
Scalar values to specify:
  • B: Coefficient B in roughness function.
  • C: Coefficient C in roughness function.
  • RplusSmooth: Roughness parameter R s m o o t h + in roughness function corresponding to a fully smooth surface.
  • RplusRough: Roughness parameter R r o u g h + in roughness function corresponding to a fully rough surface.
Rough Displaced Origin

Modification of wall treatment to incorporate roughness using displacement of origin.

Applies modified wall functions for velocity u + , Temperature T + , turbulent dissipation rate ε + , and specific dissipation rate ω + using Eqn. (1642), Eqn. (1645), Eqn. (1648), Eqn. (1650), Eqn. (1652), and Eqn. (1653), respectively.

This method does not limit the roughness height by the wall distance of the wall-adjacent cell and is therefore less sensitive to the mesh resolution. You are advised to use this method over the Rough method in case both are available.

Roughness Height
As for Rough.
Roughness Model Parameters
Scalar values to specify:
  • RplusSmooth: As for Rough.
  • RplusRough: As for Rough.

The methods Rough (R) and Rough Displaced Origin (RDO) are available depending on the selected turbulence and wall treatment models as follows:

High y+ Low y+ All y+ 2L All y+
Large Eddy Simulation Dynamic Smagorinsky Subgrid Scale - - RDO -
Smagorinsky Subgrid Scale - - RDO -
WALE Subgrid Scale - - RDO -
Reynolds-Averaged Navier-Stokes K-Epsilon Turbulence EB K-Epsilon R, RDO - R, RDO -
Lag EB K-Epsilon - - R, RDO -
Realizable K-Epsilon R, RDO - - -
Realizable K-Epsilon Two-Layer - - - R
Standard K-Epsilon R, RDO - - -
Standard K-Epsilon Low-Re - - R, RDO -
Standard K-Epsilon Two-Layer - - - R
K-Omega Turbulence SST (Menter) K-Omega R, RDO RDO R, RDO -
Standard (Wilcox) K-Omega R, RDO RDO R, RDO -
Reynolds Stress Turbulence Elliptic Blending - - R, RDO -
Linear Pressure Strain R, RDO - - -
Linear Pressure Strain Two-Layer - - - R
Quadratic Pressure Strain R, RDO - - -
Spalart-Allmaras Turbulence Standard Spalart-Allmaras - - R, RDO -

Region Settings

Wall Treatment Option (All y+ for Large Eddy Simulations)
Specifies which reference cell is used for the calculation of the wall shear stress as given by Eqn. (1638).
For Reference Location, the following options are available:
  • Off-Wall Cell: Uses the second cell away from wall for the calculation of the wall shear stress. This option reduces the effect of log-layer mismatch for wall-modeled large eddy simulations (WMLES) and is the default setting for Simcenter STAR-CCM+ 2022.1 and newer.
  • Near-Wall Cell: Uses the near-wall cell for the calculation of the wall shear stress. Use this option for backward compatibility purposes.

Field Functions

Ustar
Scalar field that represents the reference velocity u*, computed according to the selected wall treatment.
Virtual Local Heat Transfer Coefficient
Scalar field that represents an approximation to the true Local Heat Transfer Coefficient. It does not require an energy model to be activated and is defined as h=ρCpu*/T+ where T+ is computed according to the selected wall treatment. Since thermal material properties are not available, the specific heat Cp and the molecular and turbulent Prandtl numbers are specified as reference values. The fluid density ρ is obtained locally from the simulation.
Wall Roughness R+ (for walls with Wall Surface Specification set to Rough or Rough Displaced Origin)
Scalar field that represents the roughness parameter R + , as defined in Eqn. (1639).
Wall Y+
Scalar field that represents the non-dimensional wall distance. It is defined as y+=u*y/ν where u* is the reference velocity, y is the normal distance from the centroid to the wall in wall-adjacent cells and ν is the kinematic viscosity.