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Published on: May 26, 2014
Lagrangian coherent structures during combustion instability in a premixed-flame backward-step combustor.
Ramgopal Sampath1,2, Manikandan Mathur1, Satyanarayanan R Chakravarthy1,2
1Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India.
Lagrangian coherent structures, identified by finite-time Lyapunov exponent (FTLE) ridges, reveal large-scale vortices during combustion instability. These structures also act as surrogate flame boundaries, guiding flame propagation.
Area of Science:
- Fluid Dynamics
- Combustion Science
- Acoustics
Background:
- Combustion instability is a critical phenomenon in various engineering applications, often linked to complex flow dynamics.
- Understanding the interplay between flow structures, flame behavior, and acoustic oscillations is crucial for controlling combustion processes.
- Lagrangian coherent structures (LCS) offer a powerful framework for analyzing fluid transport and identifying dynamically significant flow features.
Purpose of the Study:
- To quantitatively compare large-scale coherent structures in unstable versus stable combustion flow fields.
- To investigate the role of Lagrangian coherent structures in characterizing flow dynamics and flame behavior during combustion instability.
- To determine if LCS can serve as surrogate boundaries for flame structures.
Main Methods:
- Experimental investigation of a confined flow past a backward-facing step at a Reynolds number of 18600 and equivalence ratio of 0.9.
- Utilized time-resolved particle image velocimetry (PIV) for velocity field measurements and CH* chemiluminescence for flame visualization.
- Calculated finite-time Lyapunov exponent (FTLE) fields to extract LCS ridges and analyze flow structures.
Main Results:
- FTLE ridges effectively delineated large-scale vortical structures and their modulation in the unstable (long combustor) case, contrasting with small-scale vortices in the stable (short combustor) case.
- Saddle-type flow features, identified by FTLE, separated distinct flow structures in both stable and unstable configurations.
- FTLE ridges aligned with flame boundaries upstream, acting as surrogate flame boundaries, and captured flame curl-up phenomena.
Conclusions:
- Lagrangian coherent structures, particularly FTLE ridges, are effective in identifying and characterizing large-scale flow structures associated with combustion instability.
- The study demonstrates that FTLE ridges can serve as dynamic surrogate boundaries for flames, encompassing flame curl-up.
- Flame propagation was observed to follow backward-time FTLE ridges, linking successive vortex roll-up events.
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