Funder
National Natural Science Foundation of China
Reference28 articles.
1. Modern helicopter rotor aerodynamics;Conlisk;Prog. Aerosp. Sci.,2002
2. An evaluation of dynamic stall onset prediction methods for rotorcraft airfoil design;Vieira,2013
3. Dynamic stall simulation of a pitching airfoil under unsteady freestream velocity;Gharali;J. Fluids Struct.,2013
4. An insight into the dynamic stall lift characteristics;Choudhry;Exp. Therm. Fluid Sci.,2014
5. H. Nagib, D. Greenblatt, J. Kiedaisch, Effective flow control for rotorcraft applications at flight Mach numbers, in: 31st AIAA Fluid Dynamics Conference & Exhibit, Anaheim, CA, June 11–14, 2001. AIAA Paper 2001-2974.
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