Tip Vortex Behind a Wing Undergoing Deep-Stall Oscillation
Author:
Affiliation:
1. McGill University, Montreal, Quebec H3A 2K6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.13139
Reference17 articles.
1. Dynamic Stall Experiments on Oscillating Airfoils
2. Unsteady Airfoils
3. Fluid mechanics of dynamic stall part I. Unsteady flow concepts
4. Measurement of unsteady boundary layer developed on an oscillating airfoil using multiple hot-film sensors
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