Theory
The uniformity index of Weltens et al. (1993) measures how evenly the flow passes through a cross-section, for example the inlet face of a catalyst, a filter, a fuel-cell stack or a liner: 1 when the normal velocity is the same everywhere, 0 in the worst case. Their definition averages over equal elements; the cells of a plane cut through a mesh are not equal, so every mean is weighted by the cell area, which is the same for equal elements. For example means that half the section carries twice the mean velocity and the other half none.
The plane is cut through the solved volume (the same conversion as the section plots); the velocity normal to it, , gives the index and the maximum-to-mean ratio, the tangential part the swirl angle, weighted by the flux through each cell. Cells where points against the mean flow make up the back-flow area. An inlet or outlet face uses the solution on that face. With "only inside a circle" just the cells whose centre lies within the circle count, e.g. a monolith face smaller than the duct.
Equations
| where | meaning | unit |
|---|---|---|
| Velocity normal to the plane in cell | m/s | |
| Area of cell on the plane | m² | |
| Area of the plane (or of the circle's cells) | m² | |
| Uniformity index | - |
| where | meaning | unit |
|---|---|---|
| Flux-weighted mean swirl angle | ° | |
| Velocity component in the plane | m/s |
Default and rule
- Default
- the first inlet
- Rule
The first inlet.
- Source
Weltens et al. (1993), eqs. 1-4 (area-weighted for unequal cells).
Valid range an inlet or outlet of the model
Post-processing
No solve: the plane is cut through the stored solution.