Parameterization Objects Reference
The Parameterizations objects let you compute parameters for an axisymmetric solid of revolution, typically for turbomachinery applications, or for one or more turbomachine blades.
Specific nodes referenced here are:
Parameterizations Node Action
These are the pop-up menu items available when you right-click the Parameterizations node.
- New
- Adds an axisymmetric or blade geometry from the submenu.
[Axisymmetric node] Properties
This node contains direction parameter sub-nodes for an axisymmetric geometry: Meridional (from inlet to outlet), Spanwise (from hub to shroud), and Circumferential (the direction around the rotational axis).
- Cylindrical coordinate system
- Specifies the coordinate system aligned with the domain axis of revolution. See Coordinate Systems.
- Geometry
- Selects the geometry parts or regions that participate in the parameterization. In the parameter direction child nodes, you can only choose surfaces from the parts or regions chosen here.
- Computation mesh resolution
- Defines the resolution of the 2D regular mesh that is used for computing parameters. The resolution is defined in the meridional and spanwise directions (first and second values respectively) for a constant circumferential angle (theta). The resolution is defined per row; thus for domains with multiple rows in the meridional direction, the total resolution of the computational mesh in the meridional direction is the user-provided resolution multiplied by the number of rows.
[Blade node] Properties
This node contains the following properties for selecting connected surfaces for the parts of a blade, as well as the associated axisymmetric parameterization.
For post-processing, blade parameterization is only defined on those blade surfaces that you select as inputs to this object. If other surfaces or derived parts are shown that use the same region as the blade parameterization inputs, a value of 0 is shown.
- Pressure-side Blade Surfaces
- Suction-side Blade Surfaces
- Axisymmetric Parameterization
- Leading Edge
- Trailing Edge
Meridional Properties
For the meridional (or streamwise) direction, you select surfaces through which the flow passes from inlet to outlet.
- Min
- Identifies one or more bounding surfaces by which flow enters the parameterized domain.
- Max
- Identifies one or more bounding surfaces by which flow leaves the parameterized domain.
- Interfaces
- Selects one or more surfaces defining the interfaces between rows in a multi-row setup. Each interface is defined by the outlet surfaces of one row and the inlet surfaces of its neighboring row.
Spanwise Properties
For the spanwise (radial) direction, you select surfaces of the hub and the shroud.
- Min
- Identifies the surfaces that compose the hub.
- Max
- Identifies the surfaces that compose the shroud.
Circumferential Properties
Specifies the theta direction around the rotational axis.
In the current version of Simcenter STAR-CCM+, the geometry of a full 360-deg turbomachine is not yet supported. Therefore you specify this direction using periodic surfaces.
- Min
- Selects periodic surfaces that define the lower circumferential bound.
- Max
- Selects periodic surfaces that define the higher circumferential bound.
Parameterization Field Functions
Axisymmetric Parameterizations
This set of field functions is automatically generated for each axisymmetric parameterization. The object names are given as examples from an axisymmetric geometry node named Axisymmetric 1. When you rename an axisymmetric geometry node, the names of these field functions reflect that change automatically.
Function | Notation | Range | Description |
---|---|---|---|
Axisymmetric 1 M | Arclength from inlet to outlet. Dimensions: length. | ||
Axisymmetric 1 M Normalized |
Normalized arclength from inlet to outlet. Dimensionless. is the number of rows in the meridional direction. |
||
Axisymmetric 1 M Prime | Arclength from inlet to outlet scaled by the inverse radius (1/ ). Dimensionless. | ||
Axisymmetric 1 M Prime Normalized |
Arclength from inlet to outlet scaled by the inverse radius (1/ ) and normalized. Dimensionless. is the number of rows in the meridional direction. |
||
Axisymmetric 1 S | Arclength from hub to shroud. Dimensions: length. | ||
Axisymmetric 1 S Normalized | Normalized arclength from hub to shroud. Dimensionless. |
Blade Parameterizations
This set of field functions is automatically generated for each axisymmetric parameterization. The blade vertices are essentially mapped to a 2D rectangle that goes from -1 to 1 in one direction and 0 to 1 in the other. The object names are given as examples from a blade geometry node named Blade 1.
Function | Description |
---|---|
Blade 1 Leading-Trailing | From -1 at the trailing edge, across the suction side of the blade to the leading edge where the value is 0, and across the pressure side back to the trailing edge where the value is +1. |
Blade 1 Root-Tip | From 0 at the root of the blade to 1 at the tip of the blade. |