Design of Active Flow Control at a Drooped Spoiler Configuration
Author:
Affiliation:
1. Technical University of Braunschweig
2. Swedish Defense Research Agency (FOI)
3. IBK Innovation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2518
Reference17 articles.
1. Dynamic vortex structures for flow-control applications
2. Experimental investigation of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3-element high-lift wing sections
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