Publications by authors named "Abin Krishnan"

Article Synopsis
  • The study introduces a framework using Lagrangian Coherent Structures (LCSs) for controlling tonal sounds caused by thermoacoustic instability in a turbulent combustor.
  • Researchers performed experiments to identify dynamic flow regions where dominant acoustic frequencies occur, revealing critical interactions between shear layers and vortices in the combustor.
  • A passive control strategy was developed by injecting secondary air to influence the shear layer's behavior, effectively reducing sound amplitude by preventing vortex impingement on the combustor walls.
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Thermoacoustic instability in turbulent combustion systems emerges from the complex interplay among the flame, flow, and acoustic subsystems. While the onset of thermoacoustic instability exhibits a global order, the characteristics of local interactions between subsystems responsible for this order are not well understood. Here, we utilize the framework of synchronization to elucidate the spatiotemporal interactions among heat release rate fluctuations in the flame, velocity fluctuations in the flow, and acoustic pressure fluctuations in a turbulent combustor, across the bluff-body stabilized flame.

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Many complex systems exhibit periodic oscillations comprising slow-fast timescales. In such slow-fast systems, the slow and fast timescales compete to determine the dynamics. In this study, we perform a recurrence analysis on simulated signals from paradigmatic model systems as well as signals obtained from experiments, each of which exhibit slow-fast oscillations.

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We use complex network theory to investigate the dynamical transition from stable operation to thermoacoustic instability via intermittency in a turbulent combustor with a bluff body stabilized flame. A spatial network is constructed, representing each of these three dynamical regimes of combustor operation, based on the correlation between time series of local velocity obtained from particle image velocimetry. Network centrality measures enable us to identify critical regions of the flow field during combustion noise, intermittency, and thermoacoustic instability.

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