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Large-Eddy Simulation of Flow and Heat Transfer Around a Low-Mach Number Turbine Blade

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Direct and Large-Eddy Simulation IX

Part of the book series: ERCOFTAC Series ((ERCO,volume 20))

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Abstract

If flowines has been In the ideal Brayton cycle, an increase of the pressure ratio directly leads to an increase of the thermodynamic efficiency and subsequently to a decrease of the specific fuel consumption. Unfortunately, this pressure ratio growth causes a direct increase of the temperature ratio through the turbine stages, which may impact the design of turbine blades.

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Acknowledgments

Computational time was provided by GENCI (Grand Equipement National de Calcul Intensif) under the allocation x2012026880 at IDRIS (CNRS) and by PRACE in the MS-COMB project at TGCC (CEA).

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Authors and Affiliations

  1. CORIA, CNRS UMR-6614, 76801, Saint Etienne du Rouvray, France

    N. Maheu, V. Moureau & P. Domingo

Authors
  1. N. Maheu
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  2. V. Moureau
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  3. P. Domingo
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Corresponding author

Correspondence to N. Maheu .

Editor information

Editors and Affiliations

  1. Institut für Strömungsmechanik, Technische Universität Dresden, Dresden, Germany

    Jochen Fröhlich

  2. Department of Mechanical Engineering, Eindhoven University of Technology, Eindhoven, The Netherlands

    Hans Kuerten

  3. Faculty EEMCS, Multiscale Modeling and Simulation, University of Twente, Enschede, The Netherlands

    Bernard J. Geurts

  4. Dipartimento di Ingegneria Civile ed Ambientale, Università di Trieste, Trieste, Italy

    Vincenzo Armenio

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Maheu, N., Moureau, V., Domingo, P. (2015). Large-Eddy Simulation of Flow and Heat Transfer Around a Low-Mach Number Turbine Blade. In: Fröhlich, J., Kuerten, H., Geurts, B., Armenio, V. (eds) Direct and Large-Eddy Simulation IX. ERCOFTAC Series, vol 20. Springer, Cham. https://doi.org/10.1007/978-3-319-14448-1_45

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  • DOI: https://doi.org/10.1007/978-3-319-14448-1_45

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-14447-4

  • Online ISBN: 978-3-319-14448-1

  • eBook Packages: EngineeringEngineering (R0)

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