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Hubschrauber
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Wind tunnel test of a smart rotor model with individual blade twist control
Wind tunnel testing of a smart rotor model with trailing-edge flaps
Trailing edge flap activated by a piezo-induced bending-torsion coupled beam
Torsional actuation with extension-torsion composite coupling and a magnetostrictive actuator
Status of application of smart structures technology to rotorcraft systems
Rotors with trailing edge flaps: Analysis and comparison with experimental data
Response and hub loads sensitivity analysis of a helicopter rotor
Prediction of tail rotor thrust and yaw control effectiveness
Hover test of a Mach-scale rotor model with active blade tips
Hover testing of smart rotor with induced-strain actuation of blade twist
Helicopter response to atmospheric turbulence in forward flight
Formulation of a helicopter rotor system damage detection methodology
Dynamic stability of a rotor blade using finite element 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