Computational Investigation of Turbulent Swirling Flows in Gas Turbine Combustors

Benim, A.C.; Escudier, M.P.; Stopford, P.J.; Buchanan, E.; Syed, K.J.

doi:http://dx.doi.org/10.5293/IJFMS.2008.1.1.001

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자료유형: 학술저널

저자정보: Benim, A.C. Escudier, M.P. Stopford, P.J. Buchanan, E. Syed, K.J.

저널정보: 한국유체기계학회 International Journal of Fluid Machinery and Systems International Journal of Fluid Machinery and Systems Vol.1 No.1

발행연도: 2008.8

수록면: 1 - 9 (9page)

DOI: http://dx.doi.org/10.5293/IJFMS.2008.1.1.001

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In the first part of the paper, Computational Fluid Dynamics analysis of the combusting flow within a high-swirl lean premixed gas turbine combustor and over the row nozzle guide vanes is presented. In this analysis, the focus of the investigation is the fluid dynamics at the combustor/turbine interface and its impact on the turbine. The predictions show the existence of a highly-rotating vortex core in the combustor, which is in strong interaction with the turbine nozzle guide vanes. This has been observed to be in agreement with the temperature indicated by thermal paint observations. The results suggest that swirling flow vortex core transition phenomena play a very important role in gas turbine combustors with modern lean-premixed dry low emissions technology. As the predictability of vortex core transition phenomena has not yet been investigated sufficiently, a fundamental validation study has been initiated, with the aim of validating the predictive capability of currently-available modelling procedures for turbulent swirling flows near the sub/supercritical vortex core transition. In the second part of the paper, results are presented which analyse such transitional turbulent swirling flows in two different laboratory water test rigs. It has been observed that turbulent swirling flows of interest are dominated by low-frequency transient motion of coherent structures, which cannot be adequately simulated within the framework of steady-state RANS turbulence modelling approaches. It has been found that useful results can be obtained only by modelling strategies which resolve the three-dimensional, transient motion of coherent structures, and do not assume a scalar turbulent viscosity at all scales. These models include RSM based URANS procedures as well as LES and DES approaches.

#LES #URANS #DES #gas turbine combustors #RSM #Turbulent swirling flows

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