1. Friedmann, P.P.: Rotary-wing aeroelasticity: current status and future trends. AIAA J. 42(10), 1953–1972 (2004)
2. Cambridge aerospace series;JG Leishman,2000
3. Pitt, D.M., Peters, D.A.: Theoretical predictions of dynamic inflow derivatives. Vertica 5, 21–34 (1981)
4. Pitt, D.M., Peters, D.A.: Rotor dynamic inflow derivatives and time constants from various inflow models. In: 15th European Rotorcraft Forum, Stresa, Italy (1983)
5. Pitt, D.M., Peters, D.A.: Comparison of measured induced velocities with results from a closed-form finite state wake model in forward flight. In: 45th Annual Forum of the American Helicopter Society, Boston, MA (1989)