Effect of Sweep on Dynamic Stall of a Pitching Finite-Aspect-Ratio Wing
Author:
Affiliation:
1. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058206
Reference45 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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