STAR-CCM+ / TURBULENCE & WALLS

STAR-CCM+ Turbulence Model Selection

Select the turbulence model from flow physics, near-wall resolution and the quantity of interest rather than habit.

SHORT ANSWER

Select the turbulence model from flow physics, near-wall resolution and the quantity of interest rather than habit.

01

Start from the engineering decision, not the menu option

Select the turbulence model from flow physics, near-wall resolution and the quantity of interest rather than habit. In STAR-CCM+, the relevant setting only becomes meaningful when it is tied to a measurable output, a physical scale and a stated modelling assumption.

This guide deliberately avoids a release-specific click sequence. Interface names and solver options can change between releases, while the engineering checks remain stable. Use the Siemens documentation for your installed release to confirm exact menu names after the physical decision is clear.

Practical rule:

Record the baseline value and the reason for choosing it. If the result changes materially when that assumption is varied within a defensible range, the assumption belongs in the uncertainty discussion.

02

Inputs and definitions to verify first

Before changing solver controls, confirm the quantities that actually define this problem. The most important checks for this topic are:

  • separation and adverse pressure gradients: confirm the value, definition, units and spatial location before using it to justify the setup.
  • free shear layers and jets: confirm the value, definition, units and spatial location before using it to justify the setup.
  • near-wall treatment and y+: confirm the value, definition, units and spatial location before using it to justify the setup.
  • steady versus strongly unsteady physics: confirm the value, definition, units and spatial location before using it to justify the setup.
03

Recommended STAR-CCM+ workflow

  1. Define the engineering output.

    Write down the quantity that will determine success before changing STAR-CCM+ Turbulence Model Selection. This prevents a software setting from becoming the objective itself.

  2. Verify the physical inputs.

    Check separation and adverse pressure gradients and free shear layers and jets first. Then confirm near-wall treatment and y+ and steady versus strongly unsteady physics are consistent with the real operating condition.

  3. Create a documented baseline.

    Run one traceable baseline with the model, mesh, boundary conditions and reference values recorded before tuning secondary options.

  4. Monitor solution evidence.

    Track forces and pressure drop, separation location and wall shear or heat-transfer stability. A stable residual history alone is not enough if the engineering evidence is still drifting.

  5. Run one targeted sensitivity.

    Change the parameter that most directly controls the uncertainty and confirm that the engineering conclusion does not depend on one arbitrary setting.

04

What evidence should support the final setup?

The setup is credible when the engineering outputs are stable for the right reason—not merely because the solver stopped changing quickly. Build the evidence around:

  • forces and pressure drop: compare the baseline with at least one targeted sensitivity or independent physical expectation.
  • separation location: compare the baseline with at least one targeted sensitivity or independent physical expectation.
  • wall shear or heat-transfer stability: compare the baseline with at least one targeted sensitivity or independent physical expectation.

Where possible, compare these signals with a hand calculation, correlation, test value, conservation balance or a deliberately simplified CFD case. Independent checks are especially useful before increasing model complexity.

05

Common failure modes

  • using one model for every application.
  • changing models before fixing mesh/BC errors.
  • comparing models with inconsistent wall resolution.

If one of these appears, return to the physical definition before tuning relaxation, discretization or convergence controls. Numerical tuning should not compensate for an inconsistent model.

06

Turn the guide into an engineering check

Calculate / structure

Use the related Abecator engineering tool or workflow to quantify the governing scale or setup assumption.

Wall Treatment Advisor →

Model-specific review

Use engineering support when the answer depends on your geometry, operating point, measurements or acceptance criteria.

CFD Model Review →

07

Related STAR-CCM+ guides

Editorial and independence note

This is original Abecator CFD engineering guidance. It is written around modelling decisions, dimensional consistency, conservation and verification. STAR-CCM+ is a Siemens product name; Abecator is independent and does not reproduce Siemens documentation or third-party tutorial text. For release-specific menus and supported-model details, verify against official Siemens documentation for your installed version.

AUTHORITY

Turbulence model selection: start with flow regime and required output

This section turns the workflow into a quantitative engineering check and an original visual model that can be reused during setup review.

boundary-layer / separation behavior
There is no best turbulence model in isolation; there is a model whose assumptions and cost fit the flow and decision.
ENGINEERING RELATION

Re = UL / ν

  • Re = Reynolds number
  • U = characteristic velocity
  • L = characteristic length
  • ν = kinematic viscosity
Worked example:

For air at U = 30 m/s, L = 1 m and ν = 1.5×10⁻⁵ m²/s, Re ≈ 2.0×10⁶. That establishes a turbulent-scale problem, but it does not by itself choose SST, k-ε, SA, DES or LES; separation, curvature, unsteadiness and the output still matter.

Decision table

Robust industrial baseline

Choose a RANS model matched to known flow features.

Compare pressure, forces, wall quantities and separation.
Strong separation/unsteadiness

Consider whether scale-resolving physics is required.

Check time/mesh resolution and averaging convergence.
Model uncertainty matters

Run at least one reasonable alternate model where practical.

Report whether the engineering decision changes.

Primary / official references

Exact model names and menu locations can change by STAR-CCM+ release; use the official documentation for the installed version when reproducing software steps.

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