Rotating Detonation Rocket Engine Operability Under Varied Pressure Drop Injection
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Edwards Air Force Base, California 93524
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34763
Reference25 articles.
1. Continuous Spin Detonations
2. Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts
3. Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle
4. Progress of continuously rotating detonation engines
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