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

  • Tobias LuginslandEmail author
  • Leonhard Kleiser
Conference paper
Part of the ERCOFTAC Series book 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).

Keywords

Mach Number Recirculation Zone Recirculation Region Vortex Breakdown Nozzle Flow 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Notes

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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Copyright information

© Springer International Publishing Switzerland 2015

Authors and Affiliations

  1. 1.Institute of Fluid DynamicsZurichSwitzerland

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