This paper presents a numerical investigation of a generic lab scale combustor with focus on the ignition characteristics. The test case has been examined thoroughly in a comprehensive measurement campaign to provide a detailed set of boundary conditions and a profound data base of results. The experimental setup comprises five parallel-aligned mono-disperse droplet chains which are ignited, using a focused laser beam. One aspect of the experimental study is the ignitability with respect to the imposed boundary conditions. The second covers the growth and the propagation of the flame after the establishment of an initial kernel. The outcome of the numerical simulations is compared to the experimental results which allows an in-depth assessment of the employed numerical models. The chemistry and, thus, the flame propagation behavior is captured by a turbulent flame speed closure approach with an adaptation to render the model suitable to multiphase flows. For the dispersed phase a Lagrangian particle tracking scheme is employed in combination with a continuous thermodynamics fuel model for the evaporation. The overall good agreement demonstrates the capability of a multiphase flow CFD solver in the field of ignition modeling.
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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
Validation of an Ignition and Flame Propagation Model for Multiphase Flows
J. M. Boyde,
J. M. Boyde
German Aerospace Center (DLR), Stuttgart, Germany
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P. Le Clercq,
P. Le Clercq
German Aerospace Center (DLR), Stuttgart, Germany
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M. Di Domenico,
M. Di Domenico
German Aerospace Center (DLR), Stuttgart, Germany
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M. Rachner,
M. Rachner
German Aerospace Center (DLR), Stuttgart, Germany
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G. C. Gebel,
G. C. Gebel
German Aerospace Center (DLR), Stuttgart, Germany
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T. Mosbach,
T. Mosbach
German Aerospace Center (DLR), Stuttgart, Germany
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M. Aigner
M. Aigner
German Aerospace Center (DLR), Stuttgart, Germany
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J. M. Boyde
German Aerospace Center (DLR), Stuttgart, Germany
P. Le Clercq
German Aerospace Center (DLR), Stuttgart, Germany
M. Di Domenico
German Aerospace Center (DLR), Stuttgart, Germany
M. Rachner
German Aerospace Center (DLR), Stuttgart, Germany
G. C. Gebel
German Aerospace Center (DLR), Stuttgart, Germany
T. Mosbach
German Aerospace Center (DLR), Stuttgart, Germany
M. Aigner
German Aerospace Center (DLR), Stuttgart, Germany
Paper No:
GT2011-45104, pp. 91-104; 14 pages
Published Online:
May 3, 2012
Citation
Boyde, JM, Le Clercq, P, Di Domenico, M, Rachner, M, Gebel, GC, Mosbach, T, & Aigner, M. "Validation of an Ignition and Flame Propagation Model for Multiphase Flows." 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. 91-104. ASME. https://doi.org/10.1115/GT2011-45104
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