Thermodynamic Performance Results for Rotating Detonation Rocket Engine with Distributed Heat Addition using Cantera
Author:
Affiliation:
1. Exquadrum, Inc.
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3682
Reference30 articles.
1. Fundamentals of rotating detonations
2. Numerical investigation of the physics of rotating-detonation-engines
3. Steady-State Analysis of Rotating Detonation Engine Flowfields with the Method of Characteristics
4. Continuous detonation combustion of an annular gas-mixture layer
5. Review of Propulsion Applications of Detonation Waves
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