Turbulence Chapter 1: Review of RANS-Boussinesq Models & Statistical Turbulence Description

This chapter introduces turbulence from a statistical and modeling perspective, establishing why turbulence must be modeled rather than resolved in most engineering flows. The chapter explains the decomposition of turbulent motion into mean and fluctuating components, introduces Reynolds averaging, and motivates the Reynolds-Averaged Navier–Stokes (RANS) framework. The physical meaning and limitations of the Boussinesq hypothesis are discussed, followed by an overview of advanced options commonly used to improve two-equation RANS model robustness in industrial CFD.

 

Why Turbulence Requires Modeling

Turbulent flows are characterized by:

  • Strong unsteadiness

  • Three-dimensionality

  • A wide range of interacting length and time scales

Directly resolving all turbulent scales (DNS) is:

  • Computationally prohibitive for engineering Reynolds numbers

  • Infeasible for design and industrial workflows

As a result:

  • Turbulence is treated statistically

  • Only averaged effects of turbulence are modeled

This motivates the RANS approach.


Statistical Description of Turbulence

3.1 Instantaneous vs Mean Flow

In turbulent flow:

  • Velocity, pressure, and scalar fields fluctuate randomly in time

  • These fluctuations are superimposed on an underlying mean motion

Key idea:

  • Engineering interest is usually in mean quantities

  • Fluctuations matter only through their averaged effect on transport

3.2 Reynolds Decomposition

Any instantaneous flow variable is decomposed into:

  • A time-averaged (mean) component

  • A fluctuating component with zero mean

Physical interpretation:

  • The mean represents the large-scale, organized motion

  • Fluctuations represent turbulent eddies transporting momentum and energy

This decomposition is the foundation of all RANS models.


Reynolds Averaging and Its Consequences

4.1 Reynolds-Averaged Equations

Applying averaging to the Navier–Stokes equations:

  • Removes explicit time dependence of turbulence

  • Introduces new terms representing the effect of fluctuations

These new terms are the Reynolds stresses, which:

  • Act like additional stresses in the momentum equations

  • Represent turbulent momentum transport

4.2 Closure Problem

The Reynolds stresses are unknowns:

  • They depend on fluctuating velocities

  • No new equations are automatically available

This creates the closure problem:

More unknowns than equations

All turbulence models are essentially closure models for these stresses.


Physical Meaning of Reynolds Stresses

Reynolds stresses:

  • Are not material stresses

  • Represent momentum flux caused by turbulent motion

Physically:

  • Large eddies transport high-momentum fluid into low-momentum regions

  • This enhances mixing and increases effective momentum diffusion

Turbulence therefore behaves like:

  • An additional, flow-dependent viscosity

  • But one that is anisotropic and history-dependent


The Boussinesq Hypothesis

6.1 Core Assumption

The Boussinesq hypothesis assumes:

  • Reynolds stresses are proportional to mean strain rate

  • Turbulence behaves like an isotropic eddy viscosity

This allows:

  • Reynolds stresses to be modeled using a scalar turbulent viscosity

  • Closure of the RANS equations with relatively low cost

6.2 Why It Works (and Why It Fails)

It works well when:

  • Turbulence is approximately isotropic

  • Flow curvature and rotation are weak

  • Separation is mild

It fails when:

  • Strong anisotropy exists

  • Swirl, curvature, or rotation dominate

  • Secondary flows are important

These limitations motivate advanced RANS options and higher-fidelity models.


Two-Equation RANS Models (Context)

Two-equation models:

  • Solve transport equations for two turbulence quantities

  • Use them to compute turbulent viscosity

Their popularity comes from:

  • Robustness

  • Reasonable accuracy

  • Low computational cost

This chapter does not focus on individual models, but on how they are modified and extended in practice.


Advanced Options for Two-Equation RANS Models

8.1 Why Advanced Options Are Needed

Standard RANS models:

  • Are calibrated for simple benchmark flows

  • Often fail in complex industrial geometries

Advanced options act as:

  • Corrections

  • Limiters

  • Stabilization mechanisms

They do not change the core model, but constrain or adapt it.

8.2 Production Limiters

Purpose:

  • Prevent excessive turbulence production

  • Stabilize simulations in stagnation regions or strong strain

Physical meaning:

  • Turbulence cannot grow arbitrarily fast

  • Real flows exhibit saturation mechanisms

Production limiters are especially important in:

  • High-speed flows

  • Strong acceleration or deceleration zones

8.3 Curvature and Rotation Corrections

Standard RANS models:

  • Cannot distinguish between strain and rotation

  • Mis-predict turbulence levels in curved flows

Curvature correction:

  • Reduces turbulence production in stabilizing curvature

  • Increases it in destabilizing curvature

Important for:

  • Cyclones

  • Turbomachinery

  • Strongly swirling flows

8.4 Near-Wall Damping and Low-Re Effects

Near walls:

  • Turbulence is suppressed by viscosity

  • Length scales collapse

Low-Re and damping functions:

  • Reduce turbulent viscosity near walls

  • Allow resolution of viscous sublayer

These options require:

  • Fine near-wall mesh

  • Careful y⁺ control

8.5 Model Blending and Adaptivity

Modern RANS approaches increasingly rely on:

  • Blending between formulations

  • Context-dependent behavior

This philosophy aims to:

  • Retain robustness of simple models

  • Improve accuracy in complex flows

This is a precursor to later hybrid and adaptive models.


Engineering Intuition

  • RANS models predict average turbulence effects, not turbulence itself

  • Reynolds stresses represent momentum transport by eddies

  • The Boussinesq hypothesis is a powerful but restrictive assumption

  • Advanced options exist to prevent unphysical behavior, not to “fix” turbulence

  • Most industrial success comes from judicious constraint, not model complexity

Rule of thumb:

If a RANS solution looks unstable or unphysical, the issue is often excessive turbulence production.


Study Priorities

If short on time, focus on:

  1. Reynolds decomposition and averaging

  2. Physical meaning of Reynolds stresses

  3. Closure problem in turbulence modeling

  4. Boussinesq hypothesis and its limits

  5. Purpose of production limiters and corrections


Key Takeaways

  • Turbulence is treated statistically in engineering CFD.

  • Reynolds averaging introduces unknown stress terms.

  • RANS models are closure models for turbulent momentum transport.

  • The Boussinesq hypothesis enables practical modeling but limits accuracy.

  • Advanced RANS options constrain turbulence behavior in complex flows.

  • This chapter sets the foundation for more detailed turbulence models.

Previous
Previous

Turbulence Chapter 2: Turbulence Anisotropy in RANS

Next
Next

Exploring SQL: Building a Foundation in Data