Experimental Characterization of a Supersonic Flow Control Actuator
Author:
Affiliation:
1. Johns Hopkins University Applied Physics Laboratory
2. Johns Hopkins University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-478
Reference28 articles.
1. Combustion-driven jet actuators for flow control
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