Further Experimentation of a Premixed Rotating Detonation Engine
Author:
Affiliation:
1. Air Force Research Laboratory
2. Air Force Institute of Technology
3. Innovative Scientific Solutions, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0786
Reference28 articles.
1. Thermodynamic Cycle Analysis of Pulse Detonation Engines
2. The Thermodynamic Basis of Pulsed Detonation Engine Thrust Production
3. Thermodynamic Modeling of a Rotating Detonation Engine Through a Reduced Order Approach
4. Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle
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