Term of Award
Fall 2025
Degree Name
Master of Science, Mechanical Engineering
Document Type and Release Option
Thesis (open access)
Copyright Statement / License for Reuse

This work is licensed under a Creative Commons Attribution 4.0 License.
Department
Department of Mechanical Engineering
Committee Chair
Marcel Ilie
Committee Member 1
Prakashbhai Bhoi
Committee Member 2
Mosfequr Rahman
Abstract
Advances in computational resources are making computational fluid dynamics (CFD) increasingly accessible for a variety of engineering applications. However, certain complex problems, such as simulating detailed flame kinetics, remain computationally prohibitive for many users. Developing cost-effective methods to simulate these challenges would greatly benefit applications involving flame dynamics, such as turbine engines or industrial burners. This study investigates the effect of main stage swirler intensity on near lean blow-off characteristics in a multi-staged swirl combustor using Ansys Fluent. The hybrid RANS-LES turbulence model, Stress Blended Eddy Simulation (SBES) coupled with Flamelet Generated Manifold (FGM) combustion model was selected to model the turbulence fluctuations. A reduction in swirl intensity prevented the formation of swirl-stabilized flame while excess swirl negatively affects the emission characteristics. In the baseline (S2) and high swirl (S3) cases, liftoff height increased by an average of 21.0% and 11.96% respectively, for each 0.1 decrease in equivalence ratio. The S3 case also showed reduced combustion efficiency with 156.4% increase in CO compared to S2. Local flame extinction was also captured, with the flame exhibiting increased susceptibility to quenching in regions of droplet-flame interaction.
Recommended Citation
O'Brien, Brandon, "Hybrid RANS-LES Analysis of Turbulent Flame under Near Blow-off Condition in a Multi-Stage Swirl Combustor" (2025). College of Graduate Studies: Theses & Dissertations. 3064.
https://digitalcommons.georgiasouthern.edu/etd/3064
Research Data and Supplementary Material
No
Included in
Aerodynamics and Fluid Mechanics Commons, Computational Engineering Commons, Propulsion and Power Commons, Thermodynamics Commons