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Exploring Soot Pathways: High-Fidelity LES Investigation of Soot Formation and Oxidation in RQL Combustion Systems Under Real Conditions

Koob, Philipp and Ferraro, Federica and Magens, Eggert and Heinze, Johannes and Soworka, Thomas and Behrendt, Thomas and Eggels, Ruud and Hasse, Christian (2025) Exploring Soot Pathways: High-Fidelity LES Investigation of Soot Formation and Oxidation in RQL Combustion Systems Under Real Conditions. Journal of Engineering for Gas Turbines and Power, 148 (1). American Society of Mechanical Engineers (ASME). doi: 10.1115/1.4069469. ISSN 0742-4795.

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Official URL: https://asmedigitalcollection.asme.org/gasturbinespower/article/148/1/011017/1221107/Exploring-Soot-Pathways-High-Fidelity-Large-Eddy

Abstract

Developing low-emission aero-engines presents a critical step in meeting near-term climate goals. A particular challenge is accurate soot predictions with computational fluid dynamics (CFD), where the integration of advanced thermochemical interaction models is required. The extreme conditions typical of aero-engines—characterized by high temperatures, elevated pressures, and strong transients—demand reliable and accurate modeling to capture the complex pathways of soot formation and oxidation. This study focuses on the soot formation, evolution, and oxidation in a single-sector rich–quench–lean (RQL) aero-engine model combustor, employing high-fidelity numerical simulations validated against experimental data obtained as part of this investigation. Based on the validated simulation results, the high-fidelity large eddy simulations (LESs) coupled with the split-based extended quadrature method of moments (S-EQMOM) soot model are used to examine soot dynamics within the combustor. The LES predictions accurately reproduce experimental trends across a range of operating conditions. By categorizing the combustor flow field into distinct zones—flame, mixing, recirculation, and a transition between flame and mixing—the study provides a detailed quantification of soot behavior. Soot formation and growth are predominantly confined to the flame zone, while oxidation occurs throughout the chamber, reducing the soot volume fraction. High mixing rates corresponding to very low local residence times prevent complete soot oxidation, increasing the probability of soot breakthrough into the lean region. These findings provide critical insights for developing reduced-order models that efficiently predict soot formation. Such models are essential for reducing computational costs and advancing the design of future low-emission aero-engines.

Item URL in elib:https://elib.dlr.de/218151/
Document Type:Article
Title:Exploring Soot Pathways: High-Fidelity LES Investigation of Soot Formation and Oxidation in RQL Combustion Systems Under Real Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Koob, PhilippTechnical University of Darmstadt, Department of Mechanical Engineering, Simulation of reactive Thermo-Fluid Systems, Darmstadt, GermanyUNSPECIFIEDUNSPECIFIED
Ferraro, FedericaTechnische Universität Braunschweig, Institute of Jet Propulsion and Turbomachinery, Braunschweig, GermanyUNSPECIFIEDUNSPECIFIED
Magens, EggertUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Heinze, JohannesUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Soworka, ThomasUNSPECIFIEDhttps://orcid.org/0009-0005-8443-8847UNSPECIFIED
Behrendt, ThomasUNSPECIFIEDhttps://orcid.org/0000-0002-4154-3277UNSPECIFIED
Eggels, RuudRolls-Royce Deutschland Ltd & Co KGUNSPECIFIEDUNSPECIFIED
Hasse, ChristianTechnical University of Darmstadt, Department of Mechanical Engineering, Simulation of reactive Thermo-Fluid Systems, Darmstadt, GermanyUNSPECIFIEDUNSPECIFIED
Date:8 October 2025
Journal or Publication Title:Journal of Engineering for Gas Turbines and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:148
DOI:10.1115/1.4069469
Publisher:American Society of Mechanical Engineers (ASME)
ISSN:0742-4795
Status:Published
Keywords:emissions, computational fluid dynamics (CFD), combustion, LES, combustor validation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Components and Emissions, L - Future Engines and Engine Integration, E - Combustion and Power Plant Systems, E - Gas Turbine
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine Measurement Systems
Institute of Propulsion Technology > Combustor
Deposited By: Soworka, Thomas
Deposited On:13 Dec 2025 00:38
Last Modified:13 Dec 2025 00:38

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