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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
Air Vehicle Diagnostic System Technology Demonstration Program
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
Response and hub loads sensitivity analysis of a helicopter rotor
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
Development and flight test evaluation of a rotor system load monitoring technology
Effect of modeling techniques in the coupled rotor-body vibration analysis
Rotors with trailing edge flaps: Analysis and comparison with experimental data
Helicopter rotor system health monitoring using numerical simulation and neural networks
Prediction of helicopter component loads using neural networks
Detection of helicopter rotor system simulated faults using neural networks
Formulation of a comprehensive aeroelastic analysis for tiltrotor aircraft
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
Prediction of helicopter component loads using neural networks
Assessment of transient analysis techniques for rotor stability testing
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
Air and ground resonance of helicopters with elastically tailored composite rotor blades
Blade response calcultaions using three-dimensional aerodynamic modeling
Status of application of smart structures technology to rotorcraft systems
Hover test of a Mach-scale rotor model with active blade tips
Wind tunnel testing of a smart rotor model with trailing-edge flaps
Air resonance of hingeless helicopters in trimmed forward flight
Helicopter response to atmospheric turbulence in forward flight