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Aeromechanical stability of a bearingless composite rotor in forward flight
Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades
Aeroelastic response and blade loads ofa composite rotor in forward flight
Aeromechanical stability of rotorcraft with advanced geometry blades
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Multi-objective optimization of a composite helicopter rotor
Formulation of a rotor-system damage detection methodology
Dynamically tuned blade pitch links for vibration reduction