First steps for the Development and testing of a Pulse Detonation Engine for UAV application-Reference-Cited by-同舟云学术

First steps for the Development and testing of a Pulse Detonation Engine for UAV application

Published:2008-04-28 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Zhang Gui Tian¹,Jiang Yi Tsann¹,Foo Hee Suan¹,Yip Mee Sin¹,Falempin François¹,Daniau Emeric¹

Affiliation:

1. MBDA Missile Systems

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2681

Reference17 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-KM Publishers, (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 Step Toward OperationalEngines, AIAA 2005-3233.

4. E. Daniau, F. Falempin, G. Zhang, H.S.Foo, M.S. Yip, T.Y.Jiang, D.B. Liu, Preliminary work for a pulsed detonation engine demonstrator-AIAA-2006-7957

5. Shchelkin, K.I.(1949) «Fast combustionandspinning detonation of gases », Moscow: Voenizdat 44-73

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental investigations on pulse detonation rocket engine with various injectors and nozzles;Acta Astronautica;2011-07

2. R&T Effort on Pulsed and Continuous Detonation Wave Engines;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14

3. Research on Pulse Detonation Combustion Systems: A Status Report;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

4. A Contribution to the Development of Actual Continuous Detonation Wave Engine;15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2008-04-28