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    Experimental study on effects of nozzles and combustors on the rotating detonation rocket engine in pulse operation

    Experimental study on effects of nozzles and combustors on the rotating detonation rocket engine in pulse operation door Guining Liu, Zixuan Wang, Yingying Ruan, Zewen Zhong, Rui Wang, Shengbing Zhou, Ning Hu

    Gepubliceerd in 2025-09-01

    The rotating detonation engine (RDE) is an innovative pressure-gain combustion device that harnesses detonation waves for efficient fuel combustion. This paper examines the impact of various nozzle and combustor configurations on the operating characteristics of a rotating detonation rocket engine (...

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