High-Lift Performance Investigation of a Two-Element Configuration with a Two-Stage Actuator System
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Technical University of Berlin, 10623 Berlin, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052639
Reference19 articles.
1. High-Lift Aerodynamics
2. Active Control of Flow Separation from Supercritical Airfoil Leading-Edge Flap Shoulder
3. MeltonL.SchaefflerN.LinJ. “High-Lift System for a Supercritical Airfoil: Simplified by Active Flow Control,” AIAA Paper 2007-0707, 2007.
4. Active Control of Leading Edge Separation Within the German Flow Control Network
5. High Mach Number Leading-Edge Flow Separation Control Using AC DBD Plasma Actuators
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