In RWIND Simulation, each model surface in the wind flow is treated as a "smooth" wall. As of RWIND Simulation version 1.26, it is possible to define the roughness parameters. This definition results in a boundary layer in the areas around the flow close to the walls, which has an influence on the velocity profile perpendicular to the wall depending on the air viscosity. This boundary layer is created in RWIND Simulation according to the "wall law". This law describes the velocity profile perpendicular to the wall and can be represented by the dimensionless variables u+ and y+.
Dimensionless variable u+:
U | Velocity on the wall |
uτ | Frictional velocity |
Dimensionless variable y+:
y | Wall distance |
uτ | Frictional velocity |
ν | Kinematic viscosity of the air |
Using the frictional velocity uτ (Formula 03), the boundary layer model describes the following velocity distribution in the viscous partial layer directly next to the wall (Formula 04) and in the adjacent logarithmic layer (Formula 05).
τw | Shear stress |
ρ | Air density |
κ | Kármán constant |
C | Constant |
Here is:
- κ = 0.41 for the simulation of a smooth wall)
- C = 5 for the simulation of a smooth wall
If the roughness parameters are defined, the nutkRoughWallFunction is used with the parameters Ks and Cs. The formula of the nutkRoughWallFunction can be found here:
Formula of nutkRoughWallFunction
KS | Equivalent sand roughness |
Cs | Roughness constant |
To ensure that the solution process is relatively fast and robust, the program specifies the corresponding boundary layer model directly in the first cell next to the model surface. The remaining part of the boundary layer results from the solution of the globally applied Navier-Stokes equations.