Aerodynamic characteristics of a pitching airfoil with leading-edge morphing

Author:

WEN ChaoyuanORCID,DAI Yuting,XU Yuntao,YANG Chao

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Reference29 articles.

1. McCroskey WJ. The phenomenon of dynamic stall. Washington, D.C.: NASA; 1981. Report No.: NASA-TM-81264.

2. Piziali R. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall. Washington, D.C.: NASA; 1994. Report No.: NASA-TM-4632.

3. Investigation of flow over an oscillating airfoil;Lee;J Fluid Mech,2004

4. Bifurcation behavior of airfoil undergoing stall flutter oscillations in low-speed wind tunnel;Dimitriadis;AIAA J,2009

5. Yabili S, Smith M, Dimitriadis G. Unsteady Navier-Stokes simulation of low-Reynolds stall flutter. Proceedings of the 50th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition; Nashville, Tennessee. Reston: AIAA; 2012.

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