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HUBSCHRAUBER
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Dynamic stability of a rotor blade using finite element analysis
Actuation of trailing edge flap in a wing model using piezostack device
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
Active-passive hybrid optimization of rotor blades with trailing edge flaps
Aeromechanical stability of rotorcraft with advanced geometry blades
Response and hub loads sensitivity analysis of a helicopter rotor
Induced-shear piezoelectric actuators for active twist rotor blades
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Dynamically tuned blade pitch links for vibration reduction
Formulation of a rotor-system damage detection methodology
Multi-objective optimization of a composite helicopter rotor
Aeroelastic optimization of an advanced geometry helicopter rotor
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Closed-loop hover test results with a neurocontroller on piezo-actuated smart rotor blades
Helicopter vibration reduction with trailing edge flaps
Aeroelastic stability of smart trailing-edge flap helicopter rotors
Rotors with trailing edge flaps: Analysis and comparison with experimental data
Effect of modeling techniques in the coupled rotor-body vibration analysis
Helicopter rotor system health monitoring using numerical simulation and neural networks
Assessment of transient analysis techniques for rotor stability testing
Detection of helicopter rotor system simulated faults using neural networks
Formulation of a comprehensive aeroelastic analysis for tiltrotor aircraft
Air and ground resonance of helicopters with elastically tailored composite rotor blades
Wind tunnel test of a smart rotor model with individual blade twist control
Hover testing of smart rotor with induced-strain actuation of blade twist
Trailing edge flap activated by a piezo-induced bending-torsion coupled beam
A parametric design study for actively controlled trailing edge flaps
Formulation of a helicopter rotor system damage detection methodology
Detection of helicopter rotor system simulated faults using neural networks
Prediction of tail rotor thrust and yaw control effectiveness
Hover test of a Mach-scale rotor model with active blade tips
Blade response calcultaions using three-dimensional aerodynamic modeling
An optimal actuator placement methodology for active control of helicopter airframe vibrations
Application of higher harmonic control to rotors operating at high speed and thrust
Status of application of smart structures technology to rotorcraft systems
Formulation, validation, and application of a finite element model for elastomeric lag dampers