Development of an optically accessible continuous wave Rotating Detonation Engine
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4779
Reference6 articles.
1. Experimental Analogue of a Pre-Mixed Rotating Detonation Engine In Plane Flow
2. Self-Excited, Multi-kHz Dynamics in a Linear, Semi-Bounded Detonation Channel
3. Study of the Effects of Various Injection Geometries on the Operation of a Rotating Detonation Engine
4. Feedback into Mixture Plenums in Rotating Detonation Engines
5. Oblique detonation waves stabilized in rectangular-cross-section bent tubes
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