Han D, Wang H W, Gao Z. Aeroelastic analysis of a shipboard helicopter rotor with ship motions during engagement and disengagement operations. Aerospace Science and Technology, 2012, 16(1): 1-9.
[2]
Prouty R W. Should we consider variable rotor speeds. Vertiflite, 2004, 50(4): 24-27.
[3]
Diottavio J, Friedmann D. Operational benefits of an optimal widely variable speed rotor. 66th Annual Forum Proceedings of the American Helicopter Society, 2010: 1011-1017.
[4]
Maisel M D, Giulianetti D, Dugan D. The history of the XV-15 tilt rotor research aircraft: from concept to flight. NASA SP-2000-4517, 2000.
[5]
Johnson W, Yamauchi G K. NASA heavy lift rotorcraft systems investigations. NASA TP-2005-213467, 2005.
[6]
Germanowski P J, Stille B L, Strauss M P. Technology assessment for large vertical-lift transport tiltrotors. NASA CR-2010-216484, 2010.
[7]
Blackwell R, Millott T. Dynamics design of the sikorsky X2 technologyTM demonstrator aircraft. 64th Annual Forum Proceedings of the American Helicopter Society, 2008: 886-898.
[8]
Bagai A. Aerodynamic design of the X2 technology demonstratorTM main rotor blade. 64th Annual Forum Proceedings of the American Helicopter Society, 2008: 29-44.
[9]
Steiner J, Gandhi F, Yoshizaki Y. An investigation of variable rotor RPM on performance and trim. 64th Annual Forum Proceedings of the American Helicopter Society, 2008: 697-705.
[10]
Berry B, Chopra I. Wind tunnel testing for performance and vibratory loads of a variable-speed Mach-scale rotor. 67th Annual Forum Proceedings of the American Helicopter Society, 2011: 1227-1240.
[11]
Datta A, Yeo H, Norman T R. Experimental investigation and fundamental understanding of a slowed UH-60A rotor at high advanced ratios. 67th Annual Forum Proceedings of the American Helicopter Society, 2011: 1105-1130.
[12]
Kang H, Saberi H, Grandhi F. Dynamic blade shape for improved helicopter rotor performance. 65th Annual Forum Proceedings of the American Helicopter Society, 2009: 677-688.
[13]
Han D, Smith E C. Lagwise loads analysis of a rotor blade with an embedded chordwise absorber. Journal of Aircraft, 2009, 46(4): 1280-1290.
