Experimental Aerodynamics of Mesoscale Trailing-Edge Actuators
Author:
Affiliation:
1. Stanford University, Stanford,California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1600
Reference7 articles.
1. Aerodynamic concepts for future aircraft
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5. Load control for turbine blades - A non-traditional microtab approach
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1. Particle image velocimetry investigation of flow over unsteady airfoil with trailing-edge strip;Experiments in Fluids;2007-10-26
2. Wake Vortex Control Using Static Segmented Gurney Flaps;AIAA Journal;2007-02
3. Gurney Flaps on Slender and Non-Slender Delta Wings;24th AIAA Applied Aerodynamics Conference;2006-06-05
4. Two Dimensional Unsteady Aerodynamics of Miniature Trailing Edge Effectors;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
5. Wake Vortex Control Using Rapidly Actuated Segmented Gurney Flaps;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
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