Abstract
This study examines the dynamics of vortical interactions and their implications for mitigating thermoacoustic instability in a turbulent combustor. The regions of intense vortical interactions are identified as vortical communities in the network space of weighted directed vortical networks constructed from two-dimensional experimental velocity data. One can expect vortical interactions in the combustor to be strongest near the moment of vortex shedding, as the shed vortices gradually weaken due to dissipation while convecting downstream. However, we show that, during the state of thermoacoustic instability, there is a non-trivial consistent phase lag of approximately between the shedding of the coherent structures from the backward-facing step and the time instant when the vortical interactions attain their local maximum value. We explain this phase lag by investigating the correlation between acoustic pressure fluctuations, spatio-temporal dynamics of coherent structures and vortical interactions in the reaction field of the combustor. We also show the aperiodic variation of vortical interactions during the states of combustion noise and aperiodic epochs of intermittency. Furthermore, the spatio-temporal evolution of pairs of vortical communities with the maximum inter-community interactions provides insight into explaining the critical regions detected in the reaction field during the states of intermittency and thermoacoustic instability, also identified in previous studies. We further show that the most efficient suppression of thermoacoustic instability via air microjet injection is achieved when steady air jets are introduced to disrupt the maximum inter-community interactions present during the state of thermoacoustic instability.
| Original language | English |
|---|---|
| Article number | A25 |
| Journal | Journal of Fluid Mechanics |
| Volume | 1018 |
| DOIs | |
| State | Published - Sep 1 2025 |
Funding
R.I.S. is grateful for the funding from the Office of Naval Research Global (Grant No. N62909-18-1-2061; Funder ID: 10.13039/100007297), and the Institute of Eminence (IoE) initiative of IIT Madras (SB/2021/0845/AE/MHRD/002696). This research used resources of the Oak Ridge Leadership Computing Facility at the Oak Ridge National Laboratory, which is supported by the Office of Science of the US Department of Energy under Contract No. DE-AC05-00OR22725. We thank J.M. Dhadphale, S. Singh and G. Chopra for countless fruitful discussions. We acknowledge Thilagaraj S., A. Selvam, M. Raghunathan and A. Krishnan for providing the experimental data. A.S. is grateful to the Ministry of Education for the Half-Time Research Assistantship (HTRA). The authors are grateful to Professor K. Taira for fruitful discussions. R.I.S. is grateful for the funding from the Office of Naval Research Global (Grant No. N62909-18-1-2061; Funder ID: 10.13039/100007297), and the Institute of Eminence (IoE) initiative of IIT Madras (SB/2021/0845/AE/MHRD/002696). This research used resources of the Oak Ridge Leadership Computing Facility at the Oak Ridge National Laboratory, which is supported by the Office of Science of the US Department of Energy under Contract No. DE-AC05-00OR22725.
Keywords
- turbulent reacting flows
- vortex interactions
- vortex shedding