Flow Dynamics of a Pitching Foil by Eulerian and Lagrangian Viewpoints
Author:
Affiliation:
1. National Sun Yat-Sen University, Kaohsiung 80424, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053619
Reference69 articles.
1. ShyyW.LianY.TangJ.ViieruD.LiuH., Aerodynamics of Low Reynolds Number Flyers, Cambridge Univ. Press, New York, 2011, pp. 1–158.
2. Investigation of the unsteady flow velocity field above an airfoil pitching under deep dynamic stall conditions
3. Demonstration by PIV of the non-reproducibility of the flow field around an airfoil pitching under deep dynamic stall conditions and consequences thereof
4. Velocity Measurements over a Pitching Airfoil
5. Dynamic stall on a fully equipped helicopter model
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