SpectraSim Documentation
Parameter · 10 Results

Flow uniformity: plane

results.uniformity_plane Step 10 · Results

How the plane is defined.

Last updated

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 γ=0.5\gamma = 0.5 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, unu_n, gives the index and the maximum-to-mean ratio, the tangential part utu_t the swirl angle, weighted by the flux through each cell. Cells where unu_n 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

uˉn=1A∑iun,iAi,γ=1−12A∑i∣un,i−uˉn∣uˉnAi\bar u_n = \frac{1}{A}\sum_i u_{n,i} A_i, \qquad \gamma = 1 - \frac{1}{2A}\sum_i \frac{|u_{n,i} - \bar u_n|}{\bar u_n} A_i
(1)
wheremeaningunit
un,iu_{n,i}Velocity normal to the plane in cell iim/s
AiA_iArea of cell ii on the planem²
AAArea of the plane (or of the circle's cells)m²
γ\gammaUniformity index-
θ=∑iarctan⁡(∣ut,i∣/∣un,i∣) ∣un,i∣Ai∑i∣un,i∣Ai\theta = \frac{\sum_i \arctan(|u_{t,i}|/|u_{n,i}|)\,|u_{n,i}| A_i}{\sum_i |u_{n,i}| A_i}
(2)
wheremeaningunit
θ\thetaFlux-weighted mean swirl angle°
ut,iu_{t,i}Velocity component in the planem/s

Default and rule

Default
normal to an axis
Rule

Normal to an axis.

Source

Weltens et al. (1993), eqs. 1-4 (area-weighted for unequal cells).

Valid range axis | inlet / outlet face | point + normal

Post-processing

No solve: the plane is cut through the stored solution.

References 1

  1. Weltens, H., Bressler, H., Terres, F., Neumaier, H. and Rammoser, D. (1993). Optimisation of catalytic converter gas flow distribution by CFD prediction. SAE Technical Paper 930780. DOI 10.4271/930780