Vortex breakdown and its topologies in turbulent flows within a typical swirl combustor geometry
Nitesh Kumar Sahu, Anupam Dewan, Mayank Kumar

TL;DR
This study uses large-eddy simulations to analyze vortex breakdown and its topologies in turbulent swirl flows within a combustor, identifying key parameters and flow behaviors that influence vortex stability and dynamics.
Contribution
The paper introduces a detailed analysis of vortex breakdown topologies in turbulent swirl flows, including the use of a specific swirl-number formulation and topology mapping for flow prediction.
Findings
Single-helix vortex core dominates across vane-angles
Double-helix signatures appear at certain vane-angles
Vortex precession is driven by stable and marginally stable modes
Abstract
We investigate vortex breakdown (VB) and its dominant topologies in turbulent, non-reacting flows within a canonical swirl combustor using large-eddy simulations (LES). A baseline configuration and operating conditions are first used to validate the LES solver, then five additional cases differing only by swirler vane-angle are simulated. The onset of VB is quantified using the generic swirl-number formulation, SNg, by detecting an internal recirculation zone (IRZ) in the mean flow, excluding highly-intermittent VB cases. Analysis of the mean flow shows that SNg measured within 40 mm downstream of swirler best represents the flow's swirl-strength compared with commonly used alternatives. A stable-VB first appears in the flow with 25{\deg} vane-angle, SNg=0.35. Q-criterion iso-surfaces and velocity time-series at VC footprints show a single-helix VC to prevail across all investigated…
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Taxonomy
TopicsCombustion and flame dynamics · Cyclone Separators and Fluid Dynamics · Particle Dynamics in Fluid Flows
