Abstract
It is well known that explosive-based propellants are susceptible to detonation from the controlled deflagration mode of combustion. The work presented here represents an effort to analyze and numerically model the governing equations defining such a transient two-phase reactive flow process. Computer generated results will be presented showing the development of a steady state detonation wave from an accelerating deflagration wave.
| Original language | English (US) |
|---|---|
| Title of host publication | AGARD Conference Proceedings |
| Publisher | AGARD |
| Pages | 5. 1-5. 10 |
| Edition | 367 |
| ISBN (Print) | 9283503619 |
| State | Published - 1984 |
Publication series
| Name | AGARD Conference Proceedings |
|---|---|
| Number | 367 |
| ISSN (Print) | 0549-7191 |
ASJC Scopus subject areas
- General Engineering