Development of Powered Resonance-Tube Actuators for Aircraft Flow Control Applications
Author:
Affiliation:
1. Illinois Institute of Technology, Chicago, Illinois 60616
2. The Boeing Company, St. Louis, Missouri 63166
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.144
Reference22 articles.
1. On a New Method for the Generation of Sound-Waves
2. LXXVII.On the production of acoustic waves by means of an air-jet of a velocity exceeding that of sound
3. A study of the Hartmann-Sprenger tube using the hydraulic analogy
4. Experimental Study of Flow Oscillation in a Rectangular Jet-Driven Tube
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