Performance Estimations of a Pulse Detonation Engine with Exit Nozzle
42nd, Joint propulsion conference & exhibit ; 2006 ; Sacramento, CA
2006-01-01
AIAA Paper 2006-4792
Paper numbers 2006-4300 to 2006-5277 with gaps held.; HELD ON CD-ROM
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Effects of injection nozzle exit width on rotating detonation engine
Elsevier | 2017
|Performance Estimations for Subsonic-to-Subsonic Flight Conditions of a Pulse Detonation Engine
British Library Conference Proceedings | 2008
|