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HUBSCHRAUBER
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keywords:(HUBSCHRAUBER)
Active-passive hybrid optimization of rotor blades with trailing edge flaps
Actuation of trailing edge flap in a wing model using piezostack device
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Aeroelastic response & stability of helicopters with elastomeric lag dampers
Aerolastic analysis of swept, anhedral, and tapered tip rotor blades
Aerolastic optimization of an advanced geometry helicopter rotor
Air and ground resonance of helicopters with elastically tailored composite rotor blades
Air resonance of hingeless helicopters in trimmed forward flight
An aeroelastic analysis methodology for bearingless main rotor helicopters
An optimal actuator placement methodology for active control of helicopter airframe vibrations
A parametric design study for actively controlled trailing edge flaps
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
Application of higher harmonic control to rotors operating at high speed and thrust
Assessment of transient analysis techniques for rotor stability testing
Blade response calcultaions using three-dimensional aerodynamic modeling
Detection of helicopter rotor system simulated faults using neural networks
Dynamic stability of a rotor blade using finite element analysis
Formulation of a helicopter rotor system damage detection methodology
Formulation, validation, and application of a finite element model for elastomeric lag dampers
Helicopter response to atmospheric turbulence in forward flight
Hover testing of smart rotor with induced-strain actuation of blade twist
Hover test of a Mach-scale rotor model with active blade tips
Prediction of tail rotor thrust and yaw control effectiveness
Response and hub loads sensitivity analysis of a helicopter rotor
Rotors with trailing edge flaps: Analysis and comparison with experimental data
Status of application of smart structures technology to rotorcraft systems
Torsional actuation with extension-torsion composite coupling and a magnetostrictive actuator
Trailing edge flap activated by a piezo-induced bending-torsion coupled beam
Wind tunnel testing of a smart rotor model with trailing-edge flaps
Wind tunnel test of a smart rotor model with individual blade twist control