Numerical Investigation of Fuel Distribution Effect on Flow and Temperature Field in a Heavy Duty Gas Turbine Combustor
Author:
Affiliation:
1. Electric Power Research Institute of Guangdong Power Grid Corporation , Guangzhou , Guangdong Province, P.R. China
2. School of Power and Energy, Northwestern Polytechnical University , Xi’an , P.R. China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2016-0021/pdf
Reference22 articles.
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2. Cross C, Fricker A, Shcherbik D, Lubarsky E, Zinn BT, Lovett J. Dynamics of non-premixed bluff-body stabilized flames in heated air flow. ASME Paper No.GT 2010–23059.
3. Davis LB, Black SH. Dry low NOX combustion systems for GE heavy-duty gas turbines. GE Power Systems, GER-3568G, 1999.
4. Feigl M, Setzer F, Varela RF, Myers G, Sweet B. Field test validation of the DLN 2.5H combustion system on the 9H gas turbine at Balgan bay power station. Proceedings of ASME Turbo Expo 2005, ASME paper No.GT2005–68843.
5. Gruschka U, Janus B, Meisl J, Huth M, Wasif S. ULN system for the new SGT5-8000H gas turbine: design and high pressure rig test results. Proceedings of ASME Turbo Expo, 2008, No.GT2008–51208.
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