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Mach Number Influence on Vortex Breakdown in Compressible, Subsonic Swirling Nozzle-Jet Flows

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Direct and Large-Eddy Simulation IX

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

Abstract

The phenomenon of vortex breakdown is observed in a variety of technical (vortex burners, delta wing aircraft) and environmental flows (tornadoes, hurricanes).

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Acknowledgments

The present work was funded by an ETH research grant ETH-18 08-1 and supported by a grant from the Swiss National Supercomputing Centre (CSCS), Lugano, under project ID s52. We thank M. Gloor for comments on a draft of this paper.

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Authors and Affiliations

  1. Institute of Fluid Dynamics, ETH Zurich, 8092, Zurich, Switzerland

    Tobias Luginsland & Leonhard Kleiser

Authors
  1. Tobias Luginsland
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  2. Leonhard Kleiser
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Corresponding author

Correspondence to Tobias Luginsland .

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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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Luginsland, T., Kleiser, L. (2015). Mach Number Influence on Vortex Breakdown in Compressible, Subsonic Swirling Nozzle-Jet Flows. 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_39

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  • DOI: https://doi.org/10.1007/978-3-319-14448-1_39

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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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