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|
|Pages||5. 1-5. 10|
|State||Published - 1984|
|Name||AGARD Conference Proceedings|
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