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Aeroelastic response and blade loads ofa composite rotor in forward flight
Aeroelastic optimization of an advanced geometry helicopter rotor
Aeromechanical stability of a bearingless composite rotor in forward flight
Aeromechanical stability of rotorcraft with advanced geometry blades
Effect of modeling techniques in the coupled rotor-body vibration analysis
Dynamically tuned blade pitch links for vibration reduction
Multi-objective optimization of a composite helicopter rotor
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Formulation of a rotor-system damage detection methodology
Helicopter vibration reduction with trailing edge flaps