Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades
Multi-objective optimization of a composite helicopter rotor
Helicopter vibration reduction with trailing edge flaps
Helicopter rotor system health monitoring using numerical simulation and neural networks
Formulation of a rotor-system damage detection methodology
Formulation of a comprehensive aeroelastic analysis for tiltrotor aircraft
Effect of modeling techniques in the coupled rotor-body vibration analysis
Dynamically tuned blade pitch links for vibration reduction
Detection of helicopter rotor system simulated faults using neural networks
Closed-loop hover test results with a neurocontroller on piezo-actuated smart rotor blades
Aeromechanical stability of rotorcraft with advanced geometry blades
Aeromechanical stability of a bearingless composite rotor in forward flight
Aeroelastic stability of smart trailing-edge flap helicopter rotors
Aeroelastic response and blade loads ofa composite rotor in forward flight
Aeroelastic optimization of an advanced geometry helicopter rotor
Aeroelastic analysis of advanced geometry tiltrotor aircraft