This is the second part of a series of three papers on the simulation of turbulence and transition effects in a multistage low pressure turbine. In this second part, the investigated two-stage low pressure turbine is described and results of a nonlinear full-wheel time-domain simulation are presented, analyzed and compared with the available experimental data. Furthermore, recent improvements to the CFD solver TRACE are described in brief that lead to significantly reduced wall-clock times for such large scale simulations. The utilized models match those used in the Harmonic Balance (HB) based simulations that are presented in the third paper of this series, such that the full-wheel result can be utilized to validate the HB result. Transition, flow separation and wall pressure fluctuations on the stator blades of the second stage are analyzed in detail. A strong azimuthal π-periodicity is observed, manifesting in a significantly varying stability of the midspan trailing edge flow with a quasi-steady closed separation bubble on certain blades and highly dynamic partially open separation bubbles with recurring transition and turbulent reattachment on other blades. The energy spectrum of fluctuating wall quantities in that regime shows a high bandwidth and considerable disharmonic content, which is challenging for the HB based simulations.
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ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition
June 11–15, 2018
Oslo, Norway
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5101-2
PROCEEDINGS PAPER
On the Simulation of Unsteady Turbulence and Transition Effects in a Multistage Low Pressure Turbine: Part II — Full-Wheel Simulation
Georg Geiser,
Georg Geiser
German Aerospace Center (DLR), Cologne, Germany
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Jens Wellner,
Jens Wellner
German Aerospace Center (DLR), Cologne, Germany
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Edmund Kügeler,
Edmund Kügeler
German Aerospace Center (DLR), Cologne, Germany
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Anton Weber,
Anton Weber
German Aerospace Center (DLR), Cologne, Germany
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Anselm Moors
Anselm Moors
MTU Aero Engines AG, Munich, Germany
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Georg Geiser
German Aerospace Center (DLR), Cologne, Germany
Jens Wellner
German Aerospace Center (DLR), Cologne, Germany
Edmund Kügeler
German Aerospace Center (DLR), Cologne, Germany
Anton Weber
German Aerospace Center (DLR), Cologne, Germany
Anselm Moors
MTU Aero Engines AG, Munich, Germany
Paper No:
GT2018-76764, V02CT42A043; 11 pages
Published Online:
August 30, 2018
Citation
Geiser, G, Wellner, J, Kügeler, E, Weber, A, & Moors, A. "On the Simulation of Unsteady Turbulence and Transition Effects in a Multistage Low Pressure Turbine: Part II — Full-Wheel Simulation." Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. Volume 2C: Turbomachinery. Oslo, Norway. June 11–15, 2018. V02CT42A043. ASME. https://doi.org/10.1115/GT2018-76764
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