In this paper numerical simulations of a confined, high strained jet flame employing a detailed chemistry combustion model are presented. Unlike other configurations available in literature, the geometry under investigation presents the jet axis shifted one side of the confining chamber in order to get non-symmetric recirculation zones and a flame stabilization mechanism based on the recirculation of a high percentage of hot combustion products. Fully three-dimensional unsteady simulations are carried out with finite-rate chemistry effects included by means of a detailed reaction scheme. Turbulence-chemistry interaction is taken into account by employing a presumed PDF approach, which is able to close species source terms by solving two additional transport equations. The use of the hybrid RANS/LES SST-SAS turbulence model is able to include large unsteady turbulent structures according to the local grid size and flow conditions. The approach presented here allows an in-depth investigation of flame stabilization mechanisms, ignition phenomena and influence of recirculation regions on flame stability. Additional simulations adopting simpler combustion models (i.e. Eddy-dissipation Concept) are also presented in order to assess the prediction capabilities of methods widely used in design environments. The paper also includes experimental data while comparison in terms of radial profiles at different heights above the burner are provided.
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ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition
June 6–10, 2011
Vancouver, British Columbia, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5462-4
PROCEEDINGS PAPER
Numerical Simulations of Confined, Turbulent, Lean, Premixed Flames Using a Detailed Chemistry Combustion Model
Massimiliano Di Domenico,
Massimiliano Di Domenico
German Aerospace Center (DLR), Stuttgart, Germany
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Peter Gerlinger,
Peter Gerlinger
German Aerospace Center (DLR), Stuttgart, Germany
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Berthold Noll
Berthold Noll
German Aerospace Center (DLR), Stuttgart, Germany
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Massimiliano Di Domenico
German Aerospace Center (DLR), Stuttgart, Germany
Peter Gerlinger
German Aerospace Center (DLR), Stuttgart, Germany
Berthold Noll
German Aerospace Center (DLR), Stuttgart, Germany
Paper No:
GT2011-45520, pp. 519-530; 12 pages
Published Online:
May 3, 2012
Citation
Di Domenico, M, Gerlinger, P, & Noll, B. "Numerical Simulations of Confined, Turbulent, Lean, Premixed Flames Using a Detailed Chemistry Combustion Model." Proceedings of the ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. Volume 2: Combustion, Fuels and Emissions, Parts A and B. Vancouver, British Columbia, Canada. June 6–10, 2011. pp. 519-530. ASME. https://doi.org/10.1115/GT2011-45520
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