Dynamic Stall Control Using Deployable Leading-Edge Vortex Generators

Title
Dynamic Stall Control Using Deployable Leading-Edge Vortex Generators
Authors
Keywords
-
Journal
AIAA JOURNAL
Volume 50, Issue 10, Pages 2135-2145
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2012-09-13
DOI
10.2514/1.j051452

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