A lean partially premixed swirling combustor with synthesis gases is studied using large-eddy simulation (LES). The simulation used the linear-eddy mixing (LEM) model to close the unclosed subgrid scalar flux. Several terms resulting from the LES filter are not modelled but directly resolved considering their unique length and time scales, such as the molecular diffusion, scalar mixing and chemical reaction processes. The validation results show that the code and the chemical mechanism used in the present work do have reliable accuracy. With this model, the effects of preferential diffusion process on lean partially premixed swirling combustion are investigated and the results show that the characteristics of flow and combustion dynamics can be profoundly affected. The obtained results are expected to provide helpful information for the design and operation of syngas gas turbine combustor systems.
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ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
June 13–17, 2016
Seoul, South Korea
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4976-7
PROCEEDINGS PAPER
A LES-LEM Study of Preferential Diffusion Processes in a Partially Premixed Swirling Combustor With Synthesis Gases
Shaoshuai Li,
Shaoshuai Li
Tsinghua University, Beijing, China
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Yunzhe Zheng,
Yunzhe Zheng
Tsinghua University, Beijing, China
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Daniel Mira Martinez,
Daniel Mira Martinez
Barcelona Supercomputing Center, Barcelona, Spain
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Xi Jiang
Xi Jiang
Lancaster University, Lancaster, UK
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Shaoshuai Li
Tsinghua University, Beijing, China
Yunzhe Zheng
Tsinghua University, Beijing, China
Daniel Mira Martinez
Barcelona Supercomputing Center, Barcelona, Spain
Suhui Li
Tsinghua University, Beijing, China
Min Zhu
Tsinghua University, Beijing, China
Xi Jiang
Lancaster University, Lancaster, UK
Paper No:
GT2016-57146, V04BT04A001; 13 pages
Published Online:
September 20, 2016
Citation
Li, S, Zheng, Y, Martinez, DM, Li, S, Zhu, M, & Jiang, X. "A LES-LEM Study of Preferential Diffusion Processes in a Partially Premixed Swirling Combustor With Synthesis Gases." Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. Volume 4B: Combustion, Fuels and Emissions. Seoul, South Korea. June 13–17, 2016. V04BT04A001. ASME. https://doi.org/10.1115/GT2016-57146
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