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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
Helicopter response to atmospheric turbulence in forward flight
Application of higher harmonic control to rotors operating at high speed and thrust
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
Prediction of helicopter component loads using neural networks
Air and ground resonance of helicopters with elastically tailored composite rotor blades
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