Active Flow Control Using High-Frequency Compliant Structures
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2125
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.111
Reference16 articles.
1. The delay of turbulent boundary layer separation by oscillatory active control
2. Oscillatory Control of Separation at High Reynolds Numbers
3. Control of dynamic stall using pulsed vortex generator jets
4. Enhancement of transonic airfoil performance using pulsed jets for separation control
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