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Hubschrauber
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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
Prediction of helicopter component loads using neural networks
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
Formulation of a comprehensive aeroelastic analysis for tiltrotor aircraft
Detection of helicopter rotor system simulated faults using neural networks
Helicopter rotor system health monitoring using numerical simulation and neural networks
Air Vehicle Diagnostic System Technology Demonstration Program
Closed-loop hover test results with a neurocontroller on piezo-actuated smart rotor blades
Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades
Aeroelastic stability of smart trailing-edge flap helicopter rotors