Visual experimental research on the propagation instabilities in a plane-radial rotating detonation engine
Author:
Funder
National Natural Science Foundation of China
China Postdoctoral Science Foundation
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference52 articles.
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1. Impact of the Nozzle Guide Vanes on the Pressure Fields Inside a Rotating Detonation Combustor;AIAA SCITECH 2024 Forum;2024-01-04
2. Effects of the perturbation inlet on the evolution and oscillation characteristics of multiple rotating detonation waves;Aerospace Science and Technology;2023-10
3. Effect of Combustor Outlet Geometry on Operating Characteristics of Disk-Shaped Rotating Detonation Engine;Aerospace;2023-08-20
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