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The objective of the experiment was to achieve a coupled cylindrical rotating detonation engine (RDE) with two cylindrical RDEs synchronized initiation with a single igniter. Experiments were conducted on the inner wall of the combustor with different connecting hole diameters and wall heights to evaluate the ignition mechanism, combustion mode, and propulsion performance.

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This page is a summary of: Synchronized Initiation of Two Cylindrical Rotating Detonation Engines, Journal of Propulsion and Power, June 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b39459.
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