1. Theory of Wing Sections;Abbott,1959
2. Simulation of dynamic stall for a NACA 0012 airfoil using a vortex method;Akbari;Journal of Fluids and Structures,2003
3. Observations and hypothesis of double stall;Bak;Wind Energy,1999
4. Beddoes, T.S., 1978. Onset of leading edge separation effects under dynamic conditions and low Mach numbers. In: Proceedings of the 34th Annual Forum of the American Helicopter Society.
5. Aeroelasticity;Bisplinghoff,1996