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Hubschrauber
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Prediction of Helicopter Component Loads Using Neural Networks
Prediction of helicopter component loads using neural networks
Dynamic stability of a rotor blade using finite element analysis
Actuation of trailing edge flap in a wing model using piezostack device
Response and hub loads sensitivity analysis of a helicopter rotor
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Development and flight test evaluation of a rotor system load monitoring technology
Rotors with trailing edge flaps: Analysis and comparison with experimental data
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
Assessment of transient analysis techniques for rotor stability testing
A parametric design study for actively controlled trailing edge flaps
Trailing edge flap activated by a piezo-induced bending-torsion coupled beam
Formulation of a helicopter rotor system damage detection methodology
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
Helicopter response to atmospheric turbulence in forward flight
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
Torsional actuation with extension-torsion composite coupling and a magnetostrictive actuator
Application of higher harmonic control to rotors operating at high speed and thrust
Aerolastic optimization of an advanced geometry helicopter rotor
An aeroelastic analysis methodology for bearingless main rotor helicopters
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Aerolastic analysis of swept, anhedral, and tapered tip rotor blades