Abstr:Premixed Methane-Air Swirl Burner (TECFLAM): Difference between revisions
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Validation data is available for the reacting and non-reacting cases using the same velocity boundary conditions to allow for a separate assessment of the applied turbulence model and combustion model. A total of four cases are considered in this AC consisting of a 30 kW and 150 kW flame and their corresponding isothermal cases. | Validation data is available for the reacting and non-reacting cases using the same velocity boundary conditions to allow for a separate assessment of the applied turbulence model and combustion model. A total of four cases are considered in this AC consisting of a 30 kW and 150 kW flame and their corresponding isothermal cases. | ||
[[Image:nozzle_only.png|left|frame|The Tecflam swirl burner. 2-D cut of the experimental setup]] | |||
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[[Image:photo_flamme.png|left|frame|Photograph of the flame including laser beams for the measurements. For illustration purpose a large amount of seeding material has been added (orange region). Under normal operating conditions only the blue flame is present]] | [[Image:photo_flamme.png|left|frame|Photograph of the flame including laser beams for the measurements. For illustration purpose a large amount of seeding material has been added (orange region). Under normal operating conditions only the blue flame is present]] |
Revision as of 09:58, 11 January 2011
Application Area 2: Combustion
Application Challenge AC2-08
Abstract
The TECFLAM configuration is a lean premixed methane-air burner with a high swirl intensity where the flame is stabilized by the recirculation of hot products. It is designed to investigate essential features found in industrial lean premixed combustors. An extensive set of measurements obtained by advanced laser-diagnostics exists to:
- Give insight into the underlying physics to gain a deeper understanding of the relevant phenomena
- Build a database well suited for CFD validation
Validation data is available for the reacting and non-reacting cases using the same velocity boundary conditions to allow for a separate assessment of the applied turbulence model and combustion model. A total of four cases are considered in this AC consisting of a 30 kW and 150 kW flame and their corresponding isothermal cases.
Contributors: Johannes Janicka (EKT), Guido Kuenne (EKT), Andreas Dreizler (RSM)
© copyright ERCOFTAC 2011