On the spatial structure and intermittency of soot in a lab-scale gas turbine combustor: Insights from large-eddy simulations

TL;DR

This study uses large-eddy simulations to analyze soot formation, distribution, and intermittency in a lab-scale gas turbine combustor, revealing flow recirculation as a key factor and comparing two soot modeling approaches.

Contribution

It provides detailed insights into soot spatial structure and intermittency mechanisms, and evaluates two different soot modeling methods in LES of a swirl-stabilized flame.

Findings

Soot peaks near the bluff body and correlates with flow recirculation.

Flow fluctuations cause soot intermittency through flame-front and vortex interactions.

Comparison shows trade-offs between on-the-fly and pre-tabulated soot models.

Abstract

This work presents a numerical investigation of soot formation in the Cambridge lab-scale gas turbine combustor. Large-eddy simulations (LES) of a swirl-stabilized ethylene flame are performed using the flamelet generated manifold method coupled with a discrete sectional model to account for soot formation, growth, and oxidation. The study aims to elucidate the mechanism governing the spatial structure and intermittency of soot, supported by comparisons with experimental data. The predicted soot distribution agrees well with measurements, with peak concentrations near the bluff body. Flow recirculation is identified as the key mechanism driving soot accumulation in fuel-rich regions, where surface reactions dominate soot mass growth. Soot intermittency arises from fluctuations in the flow field driven by interactions between the flame front and the recirculation vortex. Two soot modeling approaches are evaluated, differing in their treatment of soot model quantities: the first approach employs on-the-fly computation of source terms (FGM-C), while the second uses fully pre-tabulated source terms (FGM-T). Their predictive performance and computational cost are compared in the context of unsteady, sooting flames in swirl-stabilized combustors.