Standard

Time-resolved study of mixing and reaction in an aero-engine model combustor at increased pressure. / Litvinov, Ivan; Yoon, Jisu; Noren, Carrie et al.

In: Combustion and Flame, Vol. 231, 111474, 09.2021.

Research output: Contribution to journalArticlepeer-review

Harvard

APA

Litvinov, I., Yoon, J., Noren, C., Stöhr, M., Boxx, I., & Geigle, K. P. (2021). Time-resolved study of mixing and reaction in an aero-engine model combustor at increased pressure. Combustion and Flame, 231, [111474]. https://doi.org/10.1016/j.combustflame.2021.111474

Vancouver

Litvinov I, Yoon J, Noren C, Stöhr M, Boxx I, Geigle KP. Time-resolved study of mixing and reaction in an aero-engine model combustor at increased pressure. Combustion and Flame. 2021 Sept;231:111474. doi: 10.1016/j.combustflame.2021.111474

Author

Litvinov, Ivan ; Yoon, Jisu ; Noren, Carrie et al. / Time-resolved study of mixing and reaction in an aero-engine model combustor at increased pressure. In: Combustion and Flame. 2021 ; Vol. 231.

BibTeX

@article{e73f43d5b8ad4e419440d97ecbb39cc8,
title = "Time-resolved study of mixing and reaction in an aero-engine model combustor at increased pressure",
abstract = "In this study, we experimentally investigate large-scale vortex structures, fuel-air mixing and reaction processes, which occur in a partially premixed swirl-stabilized ethylene/air flame in a laboratory-scale gas turbine model combustor. Time-resolved stereo-PIV, OH-PLIF, and acetone/PAH-PLIF systems with a repetition rate of 10 kHz are used to investigate the flame behavior at 3 bar pressure and an equivalence ratio of Φ=1.2. For isothermal conditions, the results strongly indicate that vortex-induced roll-up of fuel is a main driver of the mixing process. For the reacting case, a precessing vortex core (PVC) and a double helical vortex (DHV), both co-rotating with the swirl direction and occurring simultaneously in the inner and outer shear layer, respectively, are identified by using proper orthogonal decomposition (POD) and phase-averaging techniques. Acetone-PLIF measurements show that the fuel exhibits a motion that resembles a strong axial flapping at the frequency of the DHV at reacting conditions when considering the measurement plane. The measurements show that the PVC and DHV cause a regular sequence of flame roll-up, mixture of burned and unburned gases, and the subsequent ignition of this mixture. The pockets of rich burned gas formed by mixing and reaction can eventually be oxidized by OH-rich lean burned gas regions that have the potential to prevent soot formation; however, this process strongly depends on intermittent motion within the inner recirculation zone. Based on the additional visualization of PAH-PLIF distributions, the present study further reveals for the first time the complete sequence of formation of rich burned gas, PAH and soot in a GT combustor. It is shown that soot forms only in certain regions of the high-PAH rich burned gas pockets. This indicates that other factors, such as the detailed composition of PAHs or local temperatures, which cannot be resolved here, likely also play an important role in soot formation.",
keywords = "Aero-engine combustor, Double helical vortex, High-speed laser measurements, Mixing, PAH, Precessing vortex core, PVC, Soot formation, Turbulent swirl flame",
author = "Ivan Litvinov and Jisu Yoon and Carrie Noren and Michael St{\"o}hr and Isaac Boxx and Geigle, {Klaus Peter}",
note = "Funding Information: I. Litvinov would especially acknowledge the financial support from the German Academic Exchange Service (DAAD) and the Ministry of Education and Science of the Russian Federation , project 13.12766.2018/12.2 . The experimental work at DLR was supported by the Air Force Office of Scientific Research, Air Force Material Command, USAF under Award No. FA9550-16-1-0044 and the European Union within the Horizon 2020 project SOPRANO, Soot Processes and Radiation in Aeronautical Innovative Combustors, # 690724. A fruitful discussion with M. Grader on the formation of the double helical vortex is much appreciated. We further gratefully acknowledge helpful suggestions by the anonymous reviewers. Publisher Copyright: {\textcopyright} 2021 Copyright: Copyright 2021 Elsevier B.V., All rights reserved.",
year = "2021",
month = sep,
doi = "10.1016/j.combustflame.2021.111474",
language = "English",
volume = "231",
journal = "Combustion and Flame",
issn = "0010-2180",
publisher = "Elsevier Science Inc.",

}

RIS

TY - JOUR

T1 - Time-resolved study of mixing and reaction in an aero-engine model combustor at increased pressure

AU - Litvinov, Ivan

AU - Yoon, Jisu

AU - Noren, Carrie

AU - Stöhr, Michael

AU - Boxx, Isaac

AU - Geigle, Klaus Peter

N1 - Funding Information: I. Litvinov would especially acknowledge the financial support from the German Academic Exchange Service (DAAD) and the Ministry of Education and Science of the Russian Federation , project 13.12766.2018/12.2 . The experimental work at DLR was supported by the Air Force Office of Scientific Research, Air Force Material Command, USAF under Award No. FA9550-16-1-0044 and the European Union within the Horizon 2020 project SOPRANO, Soot Processes and Radiation in Aeronautical Innovative Combustors, # 690724. A fruitful discussion with M. Grader on the formation of the double helical vortex is much appreciated. We further gratefully acknowledge helpful suggestions by the anonymous reviewers. Publisher Copyright: © 2021 Copyright: Copyright 2021 Elsevier B.V., All rights reserved.

PY - 2021/9

Y1 - 2021/9

N2 - In this study, we experimentally investigate large-scale vortex structures, fuel-air mixing and reaction processes, which occur in a partially premixed swirl-stabilized ethylene/air flame in a laboratory-scale gas turbine model combustor. Time-resolved stereo-PIV, OH-PLIF, and acetone/PAH-PLIF systems with a repetition rate of 10 kHz are used to investigate the flame behavior at 3 bar pressure and an equivalence ratio of Φ=1.2. For isothermal conditions, the results strongly indicate that vortex-induced roll-up of fuel is a main driver of the mixing process. For the reacting case, a precessing vortex core (PVC) and a double helical vortex (DHV), both co-rotating with the swirl direction and occurring simultaneously in the inner and outer shear layer, respectively, are identified by using proper orthogonal decomposition (POD) and phase-averaging techniques. Acetone-PLIF measurements show that the fuel exhibits a motion that resembles a strong axial flapping at the frequency of the DHV at reacting conditions when considering the measurement plane. The measurements show that the PVC and DHV cause a regular sequence of flame roll-up, mixture of burned and unburned gases, and the subsequent ignition of this mixture. The pockets of rich burned gas formed by mixing and reaction can eventually be oxidized by OH-rich lean burned gas regions that have the potential to prevent soot formation; however, this process strongly depends on intermittent motion within the inner recirculation zone. Based on the additional visualization of PAH-PLIF distributions, the present study further reveals for the first time the complete sequence of formation of rich burned gas, PAH and soot in a GT combustor. It is shown that soot forms only in certain regions of the high-PAH rich burned gas pockets. This indicates that other factors, such as the detailed composition of PAHs or local temperatures, which cannot be resolved here, likely also play an important role in soot formation.

AB - In this study, we experimentally investigate large-scale vortex structures, fuel-air mixing and reaction processes, which occur in a partially premixed swirl-stabilized ethylene/air flame in a laboratory-scale gas turbine model combustor. Time-resolved stereo-PIV, OH-PLIF, and acetone/PAH-PLIF systems with a repetition rate of 10 kHz are used to investigate the flame behavior at 3 bar pressure and an equivalence ratio of Φ=1.2. For isothermal conditions, the results strongly indicate that vortex-induced roll-up of fuel is a main driver of the mixing process. For the reacting case, a precessing vortex core (PVC) and a double helical vortex (DHV), both co-rotating with the swirl direction and occurring simultaneously in the inner and outer shear layer, respectively, are identified by using proper orthogonal decomposition (POD) and phase-averaging techniques. Acetone-PLIF measurements show that the fuel exhibits a motion that resembles a strong axial flapping at the frequency of the DHV at reacting conditions when considering the measurement plane. The measurements show that the PVC and DHV cause a regular sequence of flame roll-up, mixture of burned and unburned gases, and the subsequent ignition of this mixture. The pockets of rich burned gas formed by mixing and reaction can eventually be oxidized by OH-rich lean burned gas regions that have the potential to prevent soot formation; however, this process strongly depends on intermittent motion within the inner recirculation zone. Based on the additional visualization of PAH-PLIF distributions, the present study further reveals for the first time the complete sequence of formation of rich burned gas, PAH and soot in a GT combustor. It is shown that soot forms only in certain regions of the high-PAH rich burned gas pockets. This indicates that other factors, such as the detailed composition of PAHs or local temperatures, which cannot be resolved here, likely also play an important role in soot formation.

KW - Aero-engine combustor

KW - Double helical vortex

KW - High-speed laser measurements

KW - Mixing

KW - PAH

KW - Precessing vortex core

KW - PVC

KW - Soot formation

KW - Turbulent swirl flame

UR - http://www.scopus.com/inward/record.url?scp=85099263274&partnerID=8YFLogxK

U2 - 10.1016/j.combustflame.2021.111474

DO - 10.1016/j.combustflame.2021.111474

M3 - Article

AN - SCOPUS:85099263274

VL - 231

JO - Combustion and Flame

JF - Combustion and Flame

SN - 0010-2180

M1 - 111474

ER -

ID: 28874542