Study on shock train oscillations in a rectangular diverging isolator based on large eddy simulation

In the article, the unsteady flow phenomenon of self-excited and forced oscillations in a rectangular diverging isolator is studied by using large eddy simulation, and the shock train region is analysed particularly. Self-excited oscillations are analysed under four pressure ratios, with pressure statistically processed to reveal shock train oscillation characteristics. The interference factors of the external environment on the unsteady flow in the isolator are investigated, and the function of upstream disturbance and downstream disturbance on the shock train oscillation is studied. Both disturbance types show that pressure amplitude increases oscillation amplitude, while frequency variations have opposing effects. Due to mismatched response speeds, low-frequency disturbances intensify oscillations, whereas high-frequency ones suppress them. The difference is that the pressure frequency excitation upstream is transmitted along the flow direction and directly acts on the shock train in the trough period of each unsteady pressure transformation, which intensifies the negative effect on shock train oscillations. The downstream disturbance arrives at the shock train region after passing through the complex flow coupling in the mixing region. The superposition of the external pressure excitation frequency and the mixing region makes the response of the shock train slower leading to a weakening effect of the shock train oscillation. Moreover, the unsteady flow develops in the mixing district and transmits upstream, and the inhibition effect is stronger than that of upstream pressure frequency excitation.

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Publication Details

Journal
Journal of Fluid Mechanics
Published
2026-02-24
DOI
https://doi.org/10.1017/jfm.2026.11140
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
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article

Study on shock train oscillations in a rectangular diverging isolator based on large eddy simulation

Vignesh Ram Petha Sethuraman, S. C. Fu, Xinyi Fan, Ajith Kumar S et al.
Journal of Fluid Mechanics
Computational Fluid Dynamics and Aerodynamics
article

Study on shock train oscillations in a rectangular diverging isolator based on large eddy simulation

Vignesh Ram Petha Sethuraman, S. C. Fu, Xinyi Fan, Ajith Kumar S, Kexin Wu, Heuy Dong Kim
article en

Abstract

In the article, the unsteady flow phenomenon of self-excited and forced oscillations in a rectangular diverging isolator is studied by using large eddy simulation, and the shock train region is analysed particularly. Self-excited oscillations are analysed under four pressure ratios, with pressure statistically processed to reveal shock train oscillation characteristics. The interference factors of the external environment on the unsteady flow in the isolator are investigated, and the function of upstream disturbance and downstream disturbance on the shock train oscillation is studied. Both disturbance types show that pressure amplitude increases oscillation amplitude, while frequency variations have opposing effects. Due to mismatched response speeds, low-frequency disturbances intensify oscillations, whereas high-frequency ones suppress them. The difference is that the pressure frequency excitation upstream is transmitted along the flow direction and directly acts on the shock train in the trough period of each unsteady pressure transformation, which intensifies the negative effect on shock train oscillations. The downstream disturbance arrives at the shock train region after passing through the complex flow coupling in the mixing region. The superposition of the external pressure excitation frequency and the mixing region makes the response of the shock train slower leading to a weakening effect of the shock train oscillation. Moreover, the unsteady flow develops in the mixing district and transmits upstream, and the inhibition effect is stronger than that of upstream pressure frequency excitation.

Journal of Fluid MechanicsVol. 1030
Zhejiang Sci-Tech University (CN), Sejong University (KR), Amrita Vishwa Vidyapeetham (IN), Tsinghua University (CN)
Openalex Percentile: Top 42%
Computational Fluid Dynamics and Aerodynamics
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