Front Cellular Structure and Thrust Performance on Hydrogen–Oxygen Rotating Detonation Engine
Author:
Affiliation:
1. Kyushu Institute of Technology, Kitakyushu, Fukuoka 804-8550, Japan
2. Aoyama Gakuin University, Sagamihara, Kanagawa 252-5258, Japan
3. Japan Aerospace Exploration Agency, Chofu, Tokyo 182-8522, Japan
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.B36095
Reference29 articles.
1. Feasibility studies of a rotating detonation wave rocket motor.
2. Experimental research on the rotating detonation in gaseous fuels–oxygen mixtures
3. Airbreathing rotating detonation wave engine cycle analysis
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