Effect of a Coanda Extension on the Performance of a Sweeping-Jet Actuator
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054448
Reference16 articles.
1. Actuators for Active Flow Control
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3. Flow Separation Control Over a Ramp Using Sweeping Jet Actuators
4. MeltonL. P. “Active Flow Separation Control on a NACA 0015 Wing Using Fluidic Actuators,” AIAA Paper 2014-2364, June 2014.
5. Discrete Sweeping Jets as Tools for Improving the Performance of the V-22
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