Aspect Ratio Effect on Finite Wing Dynamic Stall
Author:
Affiliation:
1. Ohio Aerospace Institute
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Reference52 articles.
1. Unsteady Airfoils
2. Progress in analysis and prediction of dynamic stall
3. Fluid dynamics of unsteady separated flow. Part II. Lifting surfaces
4. Computational prediction of airfoil dynamic stall
5. Compressibility effects on dynamic stall
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