Propulsive Performance of a Continuously Rotating Detonation Engine
Author:
Affiliation:
1. Institute of High Performance Computing, Institute of High Performance Computing
2. Pusan National University, Busan 609-735, Republic of Korea
3. Warsaw University of Technology, 00-665 Warsaw, Poland.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.46686
Reference31 articles.
1. Pulse detonation propulsion: challenges, current status, and future perspective
2. Pressure Measurements and Attenuation in a Hybrid Multitube Pulse Detonation Turbine System
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