Jet Mixing Enhancement by High-Amplitude Fluidic Actuation
Author:
Affiliation:
1. University of California, Los Angeles, Los Angeles, California 90095
2. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.839
Reference19 articles.
1. Effect of tabs on the flow and noise field of an axisymmetric jet
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5. Effect of slotting on the noise of an axisymmetric supersonic jet
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