| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 864809 | Procedia IUTAM | 2015 | 10 Pages |
Abstract
Laminar-turbulent transition of an experimental configuration representative of the flow in Solid Rocket Motors is investigated using Large Eddy Simulation. The specific instability of this flow is reproduced and a turbulent region is recovered, using a spatial perturbation model built upon an analysis of the noise related to injection. The results show the axial natural growth of instabilities until the laminar-turbulent transition occurs near the end of the channel. Comparisons to measurements are made to validate the numerical procedure.
Related Topics
Physical Sciences and Engineering
Engineering
Engineering (General)
