Quasi-Two-Dimensional Simulation of a Rotating Detonation Engine Combustor and Injector
Author:
Affiliation:
1. Royal Military College, Kingston, Ontario K7K 7B4, Canada
2. University of Ottawa, Ottawa, Ontario K1N 6N5, Canada
3. National Research Council, Ottawa, Ontario K1A 0R6, Canada
Abstract
Funder
Aerospace Research Centre of the National Research Council of Canada
Office of Energy Research and Development of the Natural Resources Canada
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.B39214
Reference28 articles.
1. Feedback into Mixture Plenums in Rotating Detonation Engines
2. Three-dimensional numerical investigations of the rotating detonation engine with a hollow combustor
3. Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor
4. Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor
5. Thermodynamic Cycle Analysis of Pulse Detonation Engines
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1. Numerical Study of the Effects of Injection Conditions on Rotating Detonation Engine Propulsive Performance;Aerospace;2023-10-12
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