| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 7156102 | Computers & Fluids | 2018 | 34 Pages |
Abstract
The resulting model contains less parameter than existing ones and associates physical meaning to each of them. It is validated against experiments in two very different regimes: Shock to detonation transition, that typically happens in pressure ranges of 50Â kbar and shock propagation that involves pressure ranges 10 times higher.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
Richard Saurel, François Fraysse, Damien Furfaro, Emmanuel Lapebie,