High-Fidelity Simulations of Transitional Flow Over Pitching Airfoils
Author:
Affiliation:
1. U.S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-3693
Reference20 articles.
1. Progress in analysis and prediction of dynamic stall
2. Investigation of the flow structure around a rapidly pitching airfoil
3. Dynamic stall of a constant-rate pitching airfoil
4. Two-dimensional unsteady leading-edge separation on a pitching airfoil
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