Time-History Statistics of Soot Formation in A Model Gas Turbine CombustorSoot formation is a complex dynamic and intermittent process determined by properties of the fuel, combustor design, and combustor operation. Although the major steps in soot formation (i.e., formation of precursors, inception, growth and evolution) are similar for a variety of carbonaceous fuels, applications, and operating conditions, it remains unclear when the temporal transition between these steps occurs. An engineering prediction tool coupled with computational fluid physics (CFD), therefore needs to accurately model all these complex steps. To develop such a model, we propose the time-history concept for understanding the time dependency of soot formation as a function of local properties (i.e., temperature, velocity, local fuel air ratio, etc.). We continue our previous work with modeling the DLR aero-combustor [1] with our updated in-house CFD code, Open National Combustion Code (OpenNCC), that now includes a Multiple Time-Scale Flamelet Progress Variable approach and a the semi-empirical two-equation soot model. We injected massless tracer particles upstream of the injector region of the combustor to collect time-history statistics of the solution variables. The correlations between the collected statistics with respect to the experimental soot volume fraction data showed that time-history effect of certain flow variables, including turbulent kinetic energy (TKE), and multiple species is indeed important for soot formation. We then conducted a time-history based correlation analysis to determine the key species and the concentration ranges critical for soot formation (C6H5-based nucleation, acetylene-based surface growth, and oxidation with OH and O2). Based on the time-history correlation coefficient (THCC) analysis, we propose possible modifications to improve the current two-equation model.
Document ID
20260004729
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Kenji Miki (Glenn Research Center Cleveland, United States)
Francisco J Guzman (Glenn Research Center Cleveland, United States)
Kumud Ajmani (HX5, LLC)
Date Acquired
May 26, 2026
Subject Category
Aircraft Propulsion and PowerAerodynamics
Report/Patent Number
GT2026-176156
Meeting Information
Meeting: Turbomachinery Technical Conference and Exposition (Turbo Expo 2026)
Location: Milan
Country: IT
Start Date: June 15, 2026
End Date: June 19, 2026
Sponsors: American Society of Mechancial Engineers (ASME)