Revisiting Conventional Flaps at High Deflection-Rate: Separation Control
Author:
Affiliation:
1. Air Force Research Laboratory
2. University of Maryland, College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3945
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2. The control of flow separation by periodic excitation
3. Nguyen, L., Golubev, V., Dudley, J., and Visbal, M. "High-Fidelity Simulations of Transitional Airfoil Interacting with Canonical Upstream Flow Disturbances". AIAA 2012-2696.
4. Williams, D.R., and Grimaud, L. "Scaling Vehicle Dynamics and Fluid Dynamics in Gusting Flows". AIAA 2014-1456.
5. Orlov, D., Apker, T., He, C., Othman, H., and Corke, T. "Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators". AIAA 2007-0877
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3. Singularity Methods for Modeling Airfoil Flows with Dynamic Stall and Fast Flap Deflections;55th AIAA Aerospace Sciences Meeting;2017-01-05
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