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Hubschrauber
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Dynamic stability of a rotor blade using finite element analysis
Response and hub loads sensitivity analysis of a helicopter rotor
Assessment of transient analysis techniques for rotor stability testing
Application of higher harmonic control to rotors operating at high speed and thrust
Helicopter response to atmospheric turbulence in forward flight
Blade response calcultaions using three-dimensional aerodynamic modeling
Aeroelastic response and blade loads ofa composite rotor in forward flight
Aeroelastic optimization of an advanced geometry helicopter rotor
Aerolastic analysis of swept, anhedral, and tapered tip rotor blades
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
Air and ground resonance of helicopters with elastically tailored composite rotor blades
Prediction of helicopter component loads using neural networks
Dynamically tuned blade pitch links for vibration reduction
Multi-objective optimization of a composite helicopter rotor
Air resonance of hingeless helicopters in trimmed forward flight
Prediction of Helicopter Component Loads Using Neural Networks
Prediction of helicopter component loads using neural networks
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Formulation of a rotor-system damage detection methodology
Helicopter vibration reduction with trailing edge flaps
Prediction of tail rotor thrust and yaw control effectiveness
Torsional actuation with extension-torsion composite coupling and a magnetostrictive actuator
Formulation of a comprehensive aeroelastic analysis for tiltrotor aircraft
Detection of helicopter rotor system simulated faults using neural networks
Formulation of a helicopter rotor system damage detection methodology
Aerolastic optimization of an advanced geometry helicopter rotor
Helicopter rotor system health monitoring using numerical simulation and neural networks
Detection of helicopter rotor system simulated faults using neural networks
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
Actuation of trailing edge flap in a wing model using piezostack device
Rotors with trailing edge flaps: Analysis and comparison with experimental data
A parametric design study for actively controlled trailing edge flaps
An aeroelastic analysis methodology for bearingless main rotor helicopters
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Air Vehicle Diagnostic System Technology Demonstration Program
Trailing edge flap activated by a piezo-induced bending-torsion coupled beam
Closed-loop hover test results with a neurocontroller on piezo-actuated smart rotor blades
Development and flight test evaluation of a rotor system load monitoring technology
Status of application of smart structures technology to rotorcraft systems
Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades