Publisher
American Institute of Aeronautics and Astronautics
Reference8 articles.
1. E. Daniau, R. Zitoun, C. Couquet, D. Desbordes, Effetcs of Nozzles of Different Length and Shape on the Propulsion Performance of Pulsed Detonation Engines", High-Speed Deflagration and Detonation. Moscow: Elex-KMPublishers,(2000),pp.251-262.
2. E. Daniau, F. Falempin, S. Zhdan, F. Byokovskiy, Detonation Wave Propulsion Systems : First Step Toward Operational Engines , ISABE- 2005 -1302
3. E. Daniau, F. Falempin, F.A. Byokovskiy, S. Zhdan, Pulsed and Rotating Detonation Propulsion System : First StepTowardOperationalEngines,AIAA 2005-3233.
4. E. Daniau, F. Falempin, G. Zhang, H.S.Foo,M.S. Yip,T.Y.Jiang,D.B. Liu, Preliminarywork for apulseddetonation engine demonstrator -AIAA-2006-7957
5. G. Zhang, Y. T.Jiang, H. S. Foo, M. SinYip, F.Falempin, E. Daniau Firststeps for the development andtesting of a Pulse Detonation Engine for UAVapplication AIAA-2008-2681
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