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ACTA AERONAUTICAET ASTRONAUTICA SINICA > 2014, Vol. 35 Issue (4): 986-994   doi: 10.7527/S1000-6893.2013.0399
Numerical Calculation Effects of Deforming Leading Edge on Airfoil Dynamic Stall Control
LU Tianyu, WU Xiaosheng
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China