Variation of Leading-Edge Suction at Stall for Steady and Unsteady Airfoil Motions
Author:
Affiliation:
1. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Reference56 articles.
1. Dynamic Stall in Pitching Airfoils: Aerodynamic Damping and Compressibility Effects
2. Unsteady aerodynamics associated with a horizontal-axis wind turbine
3. Leading-edge vortices in insect flight
4. The novel aerodynamics of insect flight: applications to micro-air vehicles
5. Review of Unsteady Vortex Flows over Slender Delta Wings
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