Koob, Philipp and Nicolai, Hendrik and Lindenthal, Andreas and Hirth, Frederic Aaron Witkind and Bürkle, Niklas and Soworka, Thomas and Eggels, Ruud and Clemen, Carsten and Koch, Rainer and Behrendt, Thomas and Schroll, Michael and Hasse, Christian (2025) Comprehensive Modeling of the Cause-and-Effect Chain in Aero-Engine Combustor Simulations: from Primary Breakup to Soot Formation. In: 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, GT 2025. ASME Turbo Expo 2025 Turbomachinery Technical Conference & Exposition, 2025-06-16 - 2025-06-20, Memphis, Tennessee. doi: 10.1115/GT2025-151330. ISBN 978-0-7918-8878-0.
Full text not available from this repository.
Official URL: https://asmedigitalcollection.asme.org/GT/proceedings/GT2025/88780/V03AT04A005/1220205?searchresult=1
Abstract
Due to the significant environmental and health impacts, minimizing pollutant emissions, especially soot, is a critical challenge in developing next-generation aero-engines. While predictive soot models in CFD are essential for reducing development time and cost, the full simulation of the entire process—from fuel injection and atomization to soot formation and evolution—remains challenging and often involves strong modeling assumptions. To address this challenge, this study combines smoothed particle hydrodynamics (SPH), used to predict liquid fuel atomization, with finite volume method (FVM) large eddy simulations (LES) with advanced combustion and soot models. This approach allows for consistent simulations from fuel breakup to soot formation and enables a detailed investigation of the complex interactions between spray dynamics and soot under enginelike conditions. To accurately capture the primary breakup, the fuel spray particle size distribution (PSD) is sampled from SPH simulations and used to initialize Lagrangian spray particles in the LES, where secondary breakup and evaporation are predicted. The objective of this work is to apply these methods to a single-sector aero-engine combustion chamber operated at elevated pressure and high preheating temperatures, with an aeroengine fuel injector geometry, and to investigate the influence of spray dynamics on soot formation. Comparison with experimental data demonstrates that the applied methods accurately capture the overall flow and combustion characteristics. Spray characteristics sampled from SPH simulations significantly improve the accuracy of mixing and soot formation predictions compared to conventional spray representation approaches. Furthermore, an extended analysis across various operating ranges demonstrates that spray initializations tailored to the respective conditions are essential for achieving accurate pollutant predictions.
| Item URL in elib: | https://elib.dlr.de/218117/ | ||||||||||||||||||||||||||||||||||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Title: | Comprehensive Modeling of the Cause-and-Effect Chain in Aero-Engine Combustor Simulations: from Primary Breakup to Soot Formation | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | 11 August 2025 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Journal or Publication Title: | 70th ASME Turbo Expo 2025: Turbomachinery Technical Conference and Exposition, GT 2025 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| DOI: | 10.1115/GT2025-151330 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| ISBN: | 978-0-7918-8878-0 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Keywords: | CFD simulations, combustor, primary breakup, spray, soot formation, LII experiments, | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Event Title: | ASME Turbo Expo 2025 Turbomachinery Technical Conference & Exposition | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Event Location: | Memphis, Tennessee | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Event Start Date: | 16 June 2025 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Event End Date: | 20 June 2025 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Organizer: | ASME | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| 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 > Combustor Institute of Propulsion Technology > Engine Measurement Systems | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Deposited By: | Soworka, Thomas | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Deposited On: | 01 Dec 2025 11:35 | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Last Modified: | 01 Dec 2025 11:35 |
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