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Hubschrauber
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Trailing edge flap activated by a piezo-induced bending-torsion coupled beam
Response and hub loads sensitivity analysis of a helicopter rotor
Prediction of tail rotor thrust and yaw control effectiveness
Prediction of helicopter component loads using neural networks
Helicopter vibration reduction with trailing edge flaps
Helicopter rotor system health monitoring using numerical simulation and neural networks
Helicopter response to atmospheric turbulence in forward flight
Formulation of a rotor-system damage detection methodology
Formulation of a helicopter 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
Detection of helicopter rotor system simulated faults using neural networks
Blade response calcultaions using three-dimensional aerodynamic modeling
Assessment of transient analysis techniques for rotor stability testing
Application of higher harmonic control to rotors operating at high speed and thrust
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
A parametric design study for actively controlled trailing edge flaps
An aeroelastic analysis methodology for bearingless main rotor helicopters