Abstract
Progress is reported on the modelling, via RANS closures, of two swirling turbulent flows important in aeronautics: the trailing wing-tip vortex and the flow in rotor-stator cavities. For the former the decay of the vortex is only well captured at second-moment level while, for the latter, an unsteady flow computation brings out large-scale organized structures, with the number of structures varying with cavity aspect ratio and Reynolds number, a result qualitatively in accord with experiment. © 2009 AFM EDP Sciences.
| Original language | English |
|---|---|
| Pages (from-to) | 171-174 |
| Number of pages | 3 |
| Journal | Mecanique et Industries |
| Volume | 10 |
| Issue number | 3-4 |
| DOIs | |
| Publication status | Published - May 2009 |
Keywords
- Fluids dynamics unsteady flows
- Large-scale organized structures
- Modelling
- RANS