The Turbo Slicing Tool
In turbomachinery simulations, the repeat periodic nature of the geometry allows you to model flow through a single blade passage only. To create the fluid volume for a single blade passage, you must cut the blade passage out of the whole domain volume using surfaces that pass between adjacent blades. The Turbo Slicing tool computes these neutral surfaces for you.
When preparing the geometry for a turbomachinery simulation, your aim is to form a fluid domain around a single blade in each row. When simulating a single blade passage, you can use a much finer mesh which affords you a more detailed look at the flow near the blade.
For axial geometries, to achieve the goal, you can create a fluid domain for the entire geometry, then proceed to slice out a single blade passage. Although the Turbo Slicing tool is designed to operate on one blade row at a time, you can use the tool multiple times to create slice features for multi-row machines.
For radial geometries that have different types of blades, such as full blades and splitter blades, you can create a periodic fluid domain by including these two types of blades in the fluid domain. If the radial geometry only contains one type of blade, then you can create a periodic fluid domain that contains a single blade.
- Blade Faces - allows you to generate a neutral sheet using the faces of a blade.
- Blade Sketches - allows you to generate a neutral sheet using the sketch profiles of a blade.

Typically, you start with the raw CAD geometry of the turbomachinery. The Turbo Slicing tool is suited for axial geometries (axial-flow turbomachinery, propellers, fans), as well as radial geometries (radial compressors, radial diffusers).

