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Keywords: gas turbine model combustor
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Proceedings Papers

Proc. ASME. GT2020, Volume 4B: Combustion, Fuels, and Emissions, V04BT04A050, September 21–25, 2020
Paper No: GT2020-16107
... appears to be an integration of those local instabilities. Keywords: 4D measurements; tomography; gas turbine model combustor; heat release rate. INTRODUCTION Heat release rate distribution in a swirl-stabilized model gas turbine combustor and its fluctuation behavior associated with the surrounding...
Proceedings Papers

Proc. ASME. GT2013, Volume 1B: Combustion, Fuels and Emissions, V01BT04A024, June 3–7, 2013
Paper No: GT2013-95316
... injector whose two flow rates were controlled separately. The split of those air flows provided an additional parameter variation. Nominal power of the operating points was approximately 10 kW/bar leading to a maximum power of roughly 50 kW, not including oxidation air. gas turbine model combustor...
Proceedings Papers

Proc. ASME. GT2011, Volume 2: Combustion, Fuels and Emissions, Parts A and B, 591-600, June 6–10, 2011
Paper No: GT2011-45611
... 07 05 2012 Sooting ethylene/air flames were investigated experimentally in a dual swirl gas turbine model combustor with good optical access at atmospheric pressure. The goals of the investigations were a detailed characterization of the soot formation and oxidation processes under gas...
Proceedings Papers

Proc. ASME. GT2009, Volume 2: Combustion, Fuels and Emissions, 11-23, June 8–12, 2009
Paper No: GT2009-59038
... In this contribution the three-dimensional reacting turbulent flow field of a swirl-stabilized gas turbine model combustor is analyzed numerically. The investigated partially premixed and lifted CH4/air flame has a thermal power load of P th = 35kW and a global equivalence ratio of φ = 0.65...
Proceedings Papers

Proc. ASME. GT2006, Volume 1: Combustion and Fuels, Education, 303-309, May 8–11, 2006
Paper No: GT2006-90344
... and form a part of a co-operative EC project aiming at the development of highly efficient gas turbines for IGCC (Integrated Gasification Combined Cycle) power plants. gas turbine model combustor syngas combustion laser techniques validation measurements experimental results constitute a data...
Proceedings Papers

Proc. ASME. GT2006, Volume 1: Combustion and Fuels, Education, 237-245, May 8–11, 2006
Paper No: GT2006-90300
... 11 09 2008 Non-intrusive laser-based and optical measurements were performed in a gas turbine model combustor with a lean premixed swirl-stabilized CH 4 -air flame at atmospheric pressure. The main objective was to gain spatially and temporally resolved experimental data to enable...