Near-field flow of supersonic swirling jets-Reference-Cited by-同舟云学术

Near-field flow of supersonic swirling jets

Published:1995-05 Issue:5 Volume:33 Page:876-881
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Cutler Andrew D.¹,Levey Brian S.¹,Kraus Donna K.¹

Affiliation:

1. George Washington University/NASA/Joint Institute for Advancement of Flight Sciences, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.12362

Reference18 articles.

1. The compressible turbulent shear layer: an experimental study

2. Time evolution of the shear layer of a supersonic axisymmetric jet

3. 4Naughton, J, W. "The Enhancement of Compressible Turbulent Mixing via Streamwise Vorticity," Ph.D. Thesis, Dept. of Mechanical Engineering,Pennsylvania StateUniv.University Park, PA,May 1993.

4. A theoretical framework for mixing layers surrounding compressible turbulent swirling jets

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