Experimental Investigation of the Axisymmetric Shear Layer between Coaxial Jets with Swirl

  • C. Nayeri
  • S. Béharelle
  • J. Delville
  • J. P. Bonnet
  • H. E. Fiedler
Part of the Fluid Mechanics and its Applications book series (FMIA, volume 36)

Abstract

Swirling motion is of practical interest as it can be found in a variety of industrial applications such as combustors, cyclonic separators or in trailing vortices of aircraft. Hence, the effect of swirl in various flow configurations has been studied intensively during the past two decades. The major interest was to determine its influence on mean flow quantities and the onset of the vortex breakdown.

Keywords

Wind Tunnel Shear Layer Proper Orthogonal Decomposition Vortex Breakdown Swirl Generator 
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.

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References

  1. [1]
    H. Gründet. Strukturen in symmetrischen und asymmetrischen scherschichten. Doc­toral thesis, Technische Universität Berlin.Google Scholar
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    F.C. Gouldin, J.S. Depsky, and S.-L. Lee. Velocity field characteristics of a swirling flow combuster. AIAA jounal, 23, no. 1:95–102, 1985.ADSCrossRefGoogle Scholar
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    J. Delville, S. Bellin, and J.P. Bonnet. Use of the proper orthogonal decomposition in a plane turbulent mixing layer. In M. Lesieur and O. Metáis, editors, Turbulence and Coherent Structures, pages 75–90. Kluwer Academic Publisher, 1990.Google Scholar

Copyright information

© Kluwer Academic Publishers 1996

Authors and Affiliations

  • C. Nayeri
    • 1
  • S. Béharelle
    • 2
  • J. Delville
    • 2
  • J. P. Bonnet
    • 2
  • H. E. Fiedler
    • 1
  1. 1.TU-BerlinHermann-Föttinger-Institut BerlinBerlinGermany
  2. 2.CEAT/LEAPoitiersFrance

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