What is it about?
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.
Featured Image
Read the Original
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.
You can read the full text:
Contributors
The following have contributed to this page