In SimScale, a wall boundary condition is assigned to a face by primarily defining the behavior of the flow velocity at that face. In a CFD simulation, a wall can be an internal surface or an external surface.
Following is a snap of Wall boundary condition settings panel from the SimScale Workbench:
There are four ways to define the flow velocity at the surface assigned with a Wall boundary condition. These are:
Moving Wall: Used for surfaces in motion, where the tangential velocity component is specified.
No-slip: Recommended for viscous flow and real-world surfaces where velocity is zero at the wall. If any surfaces in the CAD model are left unassigned, then a No-slip wall boundary condition gets automatically assigned to them.
Rotating Wall: Used to specify the rotation of a wall surface about an axis. A point on the axis, the axis of rotation, and angular velocity of the rotation must be specified. The latter could be specified as a constant, or as a time-dependent variable by either uploading a CSV file or directly entering the values in the table. For general information on how to use the table feature in SimScale, refer to this document.
Slip: With Slip, a friction-less surface can be modeled. Mathematically speaking, it erases the normal component of the velocity and keeps the tangential components untouched at the assigned surface.
Additionally, to generate the boundary layer profile near the wall regions, two approaches are available. These can be defined under Turbulence wall as:
Wall Function: Appropriate functions are used to model the velocity profile. Thus, the boundary layer profile is not completely calculated and a relatively coarse mesh can be used in the near-wall regions.
To achieve a good accuracy with wall functions place the first cell of the mesh in the logarithmic region (30 < \(y^+\) < 300).
Full Resolution: In this case, the mesh has to fulfill certain criteria and should be particularly of high resolution in the near-wall regions. This boundary condition provides modelling for the viscous and inertial sublayers
For explicit resolution near the wall region, the first cell should lie in the laminar sub-layer region (\(y^+\) < 1). Such a wall is referred to as fully resolved.
The best example to understand the different wall types is that of a moving car. For simulation, the car is stationary and the air is blown at it through the inlet face (red).
Here, the car body (grey) is assigned no-slip, tires (black) are rotating walls, ground (light blue) is a moving wall (since no relative motion between air and ground), and the top along with the outer face (not seen) are slip walls.
For certain analysis types, the temperature needs to be defined too. The assignment of temperature on the surfaces of your flow domain is again done through Wall boundary condition:
All the details about the available choices and their implementation are described here without radiation and here with radiation.
Unassigned Boundary condition
Faces which are left unassigned without any boundary condition type automatically get assigned as no-slip walls with temperature being adiabatic (zero-gradient).
Last updated: November 9th, 2021
Did this article solve your issue?
How can we do better?
We appreciate and value your feedback.
Strictly Necessary Cookies
Strictly Necessary Cookie should be enabled at all times so that we can save your preferences for cookie settings.
If you disable this cookie, we will not be able to save your preferences. This means that every time you visit this website you will need to enable or disable cookies again.