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Soot Prediction in a Model Aero-Engine Combustor using a Quadrature-based Method of Moments

Çokuslu, Ömer H. ; Hasse, Christian ; Geigle, Klaus-Peter ; Ferraro, Federica (2022)
Soot Prediction in a Model Aero-Engine Combustor using a Quadrature-based Method of Moments.
Enabling Sustainability Through Aerospace Technology. San Diego, USA and virtual (03.-07.01.2022)
doi: 10.26083/tuprints-00022571
Conference or Workshop Item, Secondary publication, Postprint

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Item Type: Conference or Workshop Item
Type of entry: Secondary publication
Title: Soot Prediction in a Model Aero-Engine Combustor using a Quadrature-based Method of Moments
Language: English
Date: 2022
Place of Publication: Darmstadt
Year of primary publication: 2022
Publisher: American Institute of Aeronautics and Astronautics, Inc.
Book Title: AIAA SCITECH 2022 Forum
Collation: 12 Seiten
Event Title: Enabling Sustainability Through Aerospace Technology
Event Location: San Diego, USA and virtual
Event Dates: 03.-07.01.2022
DOI: 10.26083/tuprints-00022571
Corresponding Links:
Origin: Secondary publication

Numerical simulations of aero-engine combustors are extremely challenging due to the complex multiscale and multiphysics phenomena involved. Currently, reliable modeling and prediction of soot particle formation produced during incomplete hydrocarbon combustion is one of the major issues in combustion research. The next generation of gas turbines for more sustainable aircraft engines must meet strict limitations for soot particle mass and size distribution. Therefore, a comprehensive understanding of the processes leading to soot particle formation and its precise prediction in practical combustion systems is crucial. In this work, a recently developed detailed soot model, the Split-based Extended Quadrature Method of Moments (S-EQMOM), is applied to simulate a model aero-engine combustor, experimentally investigated by the German Aerospace Center (DLR). In previous studies, the S-EQMOM demonstrated good prediction capability in predicting soot particle oxidation, important to account for the reduction of soot particles. Here, the model is evaluated at elevated pressure conditions. Large eddy simulations are performed using flamelet-based tabulated chemistry with artificially thickened flame (ATF) approach coupled with the S-EQMOM. The simulation results are analyzed for both the gas phase and soot solid phase and compared with the experimental data. Velocity and temperature fields are well predicted. Soot formation is underestimated by the simulation, but qualitatively in good agreement with the experimental data.

Uncontrolled Keywords: Soot formation, Split-based Extended Quadrature Method of Moments, Large Eddy Simulation, model aero-engine combustor
Status: Postprint
URN: urn:nbn:de:tuda-tuprints-225719
Additional Information:

Correction: https://doi.org/10.2514/6.2022-1446.c1

View Video Presentation: https://doi.org/10.2514/6.2022-1446.vid

Classification DDC: 600 Technology, medicine, applied sciences > 620 Engineering and machine engineering
Divisions: 16 Department of Mechanical Engineering > Simulation of reactive Thermo-Fluid Systems (STFS)
TU-Projects: EC/H2020|821418|ESTiMatE
Date Deposited: 31 Oct 2022 13:38
Last Modified: 03 Mar 2023 10:43
URI: https://tuprints.ulb.tu-darmstadt.de/id/eprint/22571
PPN: 502426357
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