Attenuation of Low-Speed Flow-Induced Cavity Tones Using Plasma Actuators
Author:
Affiliation:
1. University of Southampton, Southampton, SO17 1BJ England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.26645
Reference45 articles.
1. Fundamental investigations of airframe noise
2. Development of an adaptive weapons-bay suppression system
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