Thrust Augmentation Measurements for a Pulse Detonation Engine Driven Ejector-Reference-Cited by-同舟云学术

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Thrust Augmentation Measurements for a Pulse Detonation Engine Driven Ejector

Published:2004-06-26 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Shehadeh Rafat¹,Saretto Silvano¹,Lee Seong-Young¹,Santoro Robert¹

Affiliation:

1. Pennsylvania State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3398

Reference13 articles.

1. 1Bratkovich,T.,andBussing,T."APulseDetonationEnginePerformanceModel,"AIAA-95-3155,1995.

2. Thermodynamic Cycle Analysis of Pulse Detonation Engines

3. 3Roy,G.,Frolov,S.,Santoro,R.,andTsyganov,(editors),ConfinedDetonationsandPulseDetonationEngines,TorusPress, Moscow, 2003.

4. Experimental Study of a Pulse Detonation Engine Driven Ejector

Cited by 10 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. Unsteady Thrust Measurement for Pulse Detonation Engines;Journal of Propulsion and Power;2016-01

2. Gas Flow in Ejector of Pulse Detonation Engine;29th International Symposium on Shock Waves 2;2015

3. Thrust measurement method verification and analytical studies on a liquid-fueled pulse detonation engine;Chinese Journal of Aeronautics;2014-06

4. Numerical Investigations on the Thrust Augmentation Mechanisms of Ejectors Driven by Pulse Detonation Engines;Combustion Science and Technology;2011-10

5. Experimental study of an air-breathing pulse detonation engine ejector;Experimental Thermal and Fluid Science;2011-09

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