The Combustion Dynamics group in the Rocket Propulsion Department at the German Aerospace Center (DLR), Lampoldshausen, strives to advance the understanding of dynamic processes in cryogenic rocket engines. Leveraging the test facilities and experimental expertise at DLR Lampoldshausen, the group has taken a primarily experimental approach to investigating transient flows, ignition, and combustion instabilities for over one and a half decades. This article provides a summary of recent achievements, and an overview of current and planned research activities.
|Original language||English (US)|
|Number of pages||8|
|State||Published - Jun 1 2018|
Bibliographical noteGenerated from Scopus record by KAUST IRTS on 2022-09-12
ASJC Scopus subject areas
- Aerospace Engineering