Using Controlled Unsteady Fluid Mass Addition
Author:
Affiliation:
1. NYMA Inc., Brook Park, Ohio 44142
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.185
Reference32 articles.
1. Controlled symmetric perturbation of the plane jet: an experimental study in the initial region
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4. Bifurcation of round air jets by dual-mode acoustic excitation
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