Direct numerical simulations (DNS) were used to study the effects of periodic incoming wakes on the flow near the endwall in a linear turbine cascade T106. The moving cylindrical bars generating the wakes in the experiment were represented by means of appropriate unsteady turbulent inflow conditions. In the simulations, two cases, with and without incoming wakes, were conducted at a Reynolds number of 90,000 based on chord length and outlet velocity. The results were validated with experimental data. Due to constructive limitations of the experimental setup, the incoming boundary layer is very thin, so that some features of the secondary flow are absent or small. Employing phase-averaging, however, the periodic formation of vortical structures caused by the wakes can be identified in the vicinity of the endwall.
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ASME Turbo Expo 2014: Turbine Technical Conference and Exposition
June 16–20, 2014
Düsseldorf, Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4563-9
PROCEEDINGS PAPER
DNS of the Flow Near the Endwall in a Linear Low Pressure Turbine Cascade With Periodically Passing Wakes
Denis Koschichow,
Denis Koschichow
Technische Universität Dresden, Dresden, Germany
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Jochen Fröhlich,
Jochen Fröhlich
Technische Universität Dresden, Dresden, Germany
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Ilker Kirik,
Ilker Kirik
Universität der Bundeswehr München, Neubiberg, Germany
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Reinhard Niehuis
Reinhard Niehuis
Universität der Bundeswehr München, Neubiberg, Germany
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Denis Koschichow
Technische Universität Dresden, Dresden, Germany
Jochen Fröhlich
Technische Universität Dresden, Dresden, Germany
Ilker Kirik
Universität der Bundeswehr München, Neubiberg, Germany
Reinhard Niehuis
Universität der Bundeswehr München, Neubiberg, Germany
Paper No:
GT2014-25071, V02DT44A001; 12 pages
Published Online:
September 18, 2014
Citation
Koschichow, D, Fröhlich, J, Kirik, I, & Niehuis, R. "DNS of the Flow Near the Endwall in a Linear Low Pressure Turbine Cascade With Periodically Passing Wakes." Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Volume 2D: Turbomachinery. Düsseldorf, Germany. June 16–20, 2014. V02DT44A001. ASME. https://doi.org/10.1115/GT2014-25071
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