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We use a linear non-reacting, linear rotating detonation engine model to investigate the pressure wave dynamics that are present within an operating RDE along with how the injector will recover after the passing of the detonation wave.
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This page is a summary of: Shock Propagation Through a Square Injector: Investigation into Rotating-Detonation Engine Injector Dynamics, AIAA Journal, March 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064217.
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