Thermodynamic Modeling of a Rotating Detonation Engine Through a Reduced-Order Approach
Author:
Affiliation:
1. Innovative Scientific Solutions, Inc., Dayton, Ohio 45459
2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36237
Reference26 articles.
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4. Numerical investigation of the physics of rotating-detonation-engines
5. SchwerD. A.KailasanathK. “Numerical Investigation of Rotating Detonation Engines,” 46th Joint Propulsion Conference and Exhibit, AIAA Paper 2010-6880, 2010. doi:10.2514/6.2010-6880
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