A nonlinear full-wheel time-domain simulation of a two-stage low pressure turbine is presented, analyzed, and compared with the available experimental data. Recent improvements to the computational fluid dynamics (CFD) solver TRACE that lead to significantly reduced wall-clock times for such large scale simulations are described in brief. Since the configuration is characterized by significant unsteady turbulence and transition effects, it is well suited for the validation and benchmarking of frequency-domain methods. 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 frequency-domain-based simulation methods.
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On the Simulation and Spectral Analysis of Unsteady Turbulence and Transition Effects in a Multistage Low Pressure Turbine
Georg Geiser,
Georg Geiser
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
e-mail: Georg.Geiser@dlr.de
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
e-mail: Georg.Geiser@dlr.de
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Jens Wellner,
Jens Wellner
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
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Edmund Kügeler,
Edmund Kügeler
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
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Anton Weber,
Anton Weber
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
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Anselm Moors
Anselm Moors
MTU Aero Engines AG,
Dachauer Straße 665,
Munich 80995, Germany
Dachauer Straße 665,
Munich 80995, Germany
Search for other works by this author on:
Georg Geiser
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
e-mail: Georg.Geiser@dlr.de
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
e-mail: Georg.Geiser@dlr.de
Jens Wellner
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
Edmund Kügeler
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
Anton Weber
Institute of Propulsion Technology,
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
German Aerospace Center (DLR),
Linder Höhe,
Cologne 51147, Germany
Anselm Moors
MTU Aero Engines AG,
Dachauer Straße 665,
Munich 80995, Germany
Dachauer Straße 665,
Munich 80995, Germany
1Corresponding author.
2Present address: Exa GmbH, Landshuter Allee 8, Munich 80637, Germany.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received October 5, 2018; final manuscript received October 19, 2018; published online January 25, 2019. Editor: Kenneth Hall.
J. Turbomach. May 2019, 141(5): 051012 (9 pages)
Published Online: January 25, 2019
Article history
Received:
October 5, 2018
Revised:
October 19, 2018
Citation
Geiser, G., Wellner, J., Kügeler, E., Weber, A., and Moors, A. (January 25, 2019). "On the Simulation and Spectral Analysis of Unsteady Turbulence and Transition Effects in a Multistage Low Pressure Turbine." ASME. J. Turbomach. May 2019; 141(5): 051012. https://doi.org/10.1115/1.4041820
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