Lean premixed natural gas/air flames produced by an industrial gas turbine burner were analyzed using laser diagnostic methods. For this purpose, the burner was equipped with an optical combustion chamber and operated with preheated air at various thermal powers , equivalence ratios , and pressures up to . For the visualization of the flame emissions chemiluminescence imaging was applied. Absolute flow velocities were measured using particle image velocimetry (PIV), and the reaction zones as well as regions of burnt gas were characterized by planar laser-induced fluorescence (PLIF) of OH. Using these techniques, the combustion behavior was characterized in detail. The mean flow field could be divided into different regimes: the inflow, a central and an outer recirculation zone, and the outgoing exhaust flow. Single-shot PIV images demonstrated that the instantaneous flow field was composed of small and medium sized vortices, mainly located along the shear layers. The chemiluminescence images reflected the regions of heat release. From the PLIF images it was seen that the primary reactions are located in the shear layers between the inflow and the recirculation zones and that the appearance of the reaction zones changed with flame parameters.
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March 2009
Research Papers
Flow Field and Combustion Characterization of Premixed Gas Turbine Flames by Planar Laser Techniques
Ulrich Stopper,
Ulrich Stopper
German Aerospace Center,
e-mail: ulrich.stopper@dlr.de
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
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Manfred Aigner,
Manfred Aigner
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
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Wolfgang Meier,
Wolfgang Meier
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
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Rajesh Sadanandan,
Rajesh Sadanandan
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
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Michael Stöhr,
Michael Stöhr
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
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Ik Soo Kim
Ik Soo Kim
Siemens Industrial Turbomachinery Ltd.
, P.O. Box 1, Waterside South, Lincoln LN5 7FD, UK
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Ulrich Stopper
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germanye-mail: ulrich.stopper@dlr.de
Manfred Aigner
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
Wolfgang Meier
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
Rajesh Sadanandan
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
Michael Stöhr
German Aerospace Center,
Institute of Combustion Technology
, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany
Ik Soo Kim
Siemens Industrial Turbomachinery Ltd.
, P.O. Box 1, Waterside South, Lincoln LN5 7FD, UKJ. Eng. Gas Turbines Power. Mar 2009, 131(2): 021504 (8 pages)
Published Online: December 30, 2008
Article history
Received:
April 10, 2008
Revised:
April 14, 2008
Published:
December 30, 2008
Citation
Stopper, U., Aigner, M., Meier, W., Sadanandan, R., Stöhr, M., and Kim, I. S. (December 30, 2008). "Flow Field and Combustion Characterization of Premixed Gas Turbine Flames by Planar Laser Techniques." ASME. J. Eng. Gas Turbines Power. March 2009; 131(2): 021504. https://doi.org/10.1115/1.2969093
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