ANALYTICAL MODEL OF SHOCK DYNAMICS IN PULSE DETONATION ENGINE NOZZLES (AIAA 2016-4878)
Joint propulsion conference
01.01.2016
17 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1939
Compressor Integration Study for a Pulse Detonation Engine (AIAA 2016-0397)
British Library Conference Proceedings | 2016
|Detonation Reignition within a Rotating Detonation Engine (AIAA 2016-1202)
British Library Conference Proceedings | 2016
|A review of research on pulse detonation engine nozzles
AIAA | 2001
|