Abstract
Solid rocket motor flows depend strongly on alumina granulometry, which spreads up with coalescence. Solving droplet sizes in unsteady flows is a modeling and numerical challenge, specially when high loadings generate retrocoupling. As an alternative to Lagrangian approaches, the Eulerian Multi-Fluid model describes polydispersity with size-sorted droplet fluids called sections. A two size moment method, that spares sections, is implemented in the CEDRE code. A new transport and coupling method allows to capture moderately dense spray structures with low diffusion. The aim is threefold: compare CEDRE's Lagrangian and new Eulerian two-phase approaches, prove the feasibility of unsteady and complex motor flow simulations, and show the effect of coalescence on instabilities.
| Original language | English |
|---|---|
| Pages (from-to) | 44-54 |
| Number of pages | 11 |
| Journal | Comptes Rendus - Mecanique |
| Volume | 341 |
| Issue number | 1-2 |
| DOIs | |
| Publication status | Published - 1 Jan 2013 |
| Externally published | Yes |
Keywords
- Coalescence
- Combustion
- Eulerian multi-fluid
- Moderately dense spray
- Solid rocket motor