Is this page helpful?
35x
000309
2025-02-18

VE0309 | Atmospheric Boundary Layer Test

Description

This example is based on the Atmospheric Boundary Layer (ABL) test from the document of German WTG: Fact Sheet of Committee 3 - Numerical simulation of wind flows, chapter 9.1 (see references). Before each numerical simulation, it should be checked whether the atmospheric boundary layer defined at the inflow reaches the structure by testing its development in an empty tunnel. This affects not only the distribution of the velocities, but also the turbulent quantities. The test must be carried out for both steady (RANS) and transient (URANS, LES) calculations. In the following article, the development of a velocity field, turbulence kinetic energy field and turbulence dissipation rate field is shown for the four terrain categories I to IV defined in the EN 1991-1-4. A vertically anisotropic turbulence acc. to chapter 6.3.1 and RANS k-ω SST turbulence model is used.

Fluid Properties Kinematic Viscosity ν 1.500e-5 m2/s
Density ρ 1.250 kg/m3
Wind Tunnel Length Dx 800.000 m
Width Dy 80.000 m
Height Dz 300.000 m
Calculation Parameters Reference Velocity uref 20.000 m/s
Reference Height zref 10.000 m
von Kármán Constant κ 0.410
Turbulence Viscosity Constant Cμ 0.090

Analytical Solution

Analytical solution is not available. The example provides an overview of the chosen quantity field development in an empty wind tunnel.

Wind speed profile is calculated from the following equation:

where u* is friction velocity, defined as:

Turbulence k profile is defined according following equation:

Turbulence ω profile is defined calculated according following equation:

RWIND Simulation Settings

  • Modelled in RWIND 3.03.0220
  • Steady flow simulation type
  • Mesh density is 28 %: 2 482 465 cells
  • Number of tunnel boundary layers is 10
  • The height of the first cell at the bottom is 0.046 m
  • y+ ranges from 800 to 1000
  • RANS k-ω SST turbulence model
  • Inlet boundary condition - ABL v, k, ω; zero pressure gradient
  • Tunnel bottom - no-slip boundary condition
  • Tunnel walls and top - slip boundary condition
  • Outlet boundary condition - zero pressure; zero velocity gradient

Results

Terrain category I

Terrain category II

Terrain category III

Terrain category IV


References
  1. Windtechnological Society WTG eV (2023). WTG Code of Practice M3 - Numerical Simulation of Wind Flows. Aachen: Sgt.