[1]
V. Animitsa, V. Golovin, M. Krainov, V. Novak, N. Tarasov, V. Shcheglova. Experiment-Calculated Investigations of Fields of Inductive Velocities Behind the Rotor on Aerodynamic Characteristics of the Antitorque Rotor at Small Flight Speeds at Lateral Wind. TSAGI. Moscow. The 4th Forum of the Russian Helicopter Society. February, 2004.
Google Scholar
[2]
J.C. Walchko, J. Kim, K. W. Wang, E.C. Smith, Hybrid Feed forward-Feedback Control for Active Helicopter Vibration Suppression. The Pennsylvania State University, University Park, PA 16802. AHS Forum Penn State Papers May 1-3, 2007.
Google Scholar
[3]
R.S. Turmanidze, L. Dadone, J.J. Philippe, B. Demaret, Investigation, Development and Tests Results of the Variable Geometry Rotor. 33rd European Rotorcraft Forum. Kazan, 10–14 September 2007, Pages 11.
Google Scholar
[4]
Dadone L.; Liu J.; Acree C. Proprotor Design Issues for High Speed Tiltrotors. Boeing Defense & Space Group, Helicopter Division. NASA Ames Research Center. Presented at the 50 th Annual Forum of the American Helicopter Society, Washington, DC, May 1994. p.21.
Google Scholar
[5]
R. Turmanidze, L. Dadone, G. Sanadze. Increase of Flight and Technical Characteristics of Flying Vehicles By Means of Application of the Variable Geometry Rotor. Materials of the 5th Forum of the Russian Helicopter Society. Moscow, 2002. p. VI39-VI48.
Google Scholar