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      Effect of tabs on the flow and noise field of an axisymmetric jet

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      AIAA Journal
      American Institute of Aeronautics and Astronautics (AIAA)

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          Most cited references26

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          The compressible turbulent shear layer: an experimental study

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            Motion of particles with inertia in a compressible free shear layer

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              • Abstract: not found
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              A study of hairpin vortices in a laminar boundary layer. Part 1. Hairpin vortices generated by a hemisphere protuberance

                Author and article information

                Journal
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics (AIAA)
                0001-1452
                1533-385X
                April 1993
                April 1993
                : 31
                : 4
                : 609-619
                Article
                10.2514/3.11594
                aae31168-0005-4e57-b6eb-ed4801847461
                © 1993
                History

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