| Citation: | FAN Liangzhong, GUO Kangkang, SHU Chen, et al. Stability analysis of continuous rotating detonation in hollow combustor[J]. Journal of Aerospace Power, 2023, 38（5）：1090-1101 doi: 10.13224/j.cnki.jasp.20210548
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Rotating detonation experiments were conducted with various mass flow (i.e., 142.7−493.9 g/s) in a hollow combustor. The propagation velocity of the detonation wave was close to the Chapman-Jouguet (CJ) detonation speed when the mass flow reached 493.9 g/s. With the decrease of mass flow, the velocity and pressure of the detonation waves decreased. When it dropped to 142.7 g/s, the detonation waves evolved into a two-wave mode, accompanied by extinction and re-initiation phenomenon. Moreover, the pressure and velocity of the detonation waves fluctuated periodically, and the average propagation velocity was only 76.8% of CJ detonation velocity. Further, the nonlinear time-series analysis was adopted to reveal the stabilities of detonation waves. Results showed that when the mass flow was greater than 300 g/s, the attractor of the pressure time series in the phase space converged to the limit cycle mode. Decreasing the flow led to the disorder of the attractor. It indicated that the stability of the detonation wave decreased, and the system was prone to disorder. This study proved the effectiveness of nonlinear time-series analysis in studying the stabilities of rotating detonation, providing a methodological reference for the judgment of detonation wave stability under complex working conditions.
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