Actuation of trailing edge flap in a wing model using piezostack device
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Aeroelastic optimization of an advanced geometry helicopter rotor
Aeroelastic response and blade loads ofa composite rotor in forward flight
Aeroelastic stability of smart trailing-edge flap helicopter rotors
Aerolastic analysis of swept, anhedral, and tapered tip rotor blades
Aerolastic optimization of an advanced geometry helicopter rotor
Aeromechanical stability of a bearingless composite rotor in forward flight
Aeromechanical stability of rotorcraft with advanced geometry blades
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
A Parametric Design Study for Actively Controlled Edge Flaps
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
Closed-loop hover test results with a neurocontroller on piezo-actuated smart rotor blades
Detection of helicopter rotor system simulated faults using neural networks
Detection of helicopter rotor system simulated faults using neural networks
Dynamically tuned blade pitch links for vibration reduction
Dynamic stability of a rotor blade using finite element analysis
Effect of modeling techniques in the coupled rotor-body vibration analysis
Formulation of a comprehensive aeroelastic analysis for tiltrotor aircraft
Formulation of a helicopter rotor system damage detection methodology
Formulation of a rotor-system damage detection methodology
Helicopter response to atmospheric turbulence in forward flight
Helicopter rotor system health monitoring using numerical simulation and neural networks
Helicopter vibration reduction with trailing edge flaps
Hover testing of smart rotor with induced-strain actuation of blade twist
Hover test of a Mach-scale rotor model with active blade tips
Multi-objective optimization of a composite helicopter rotor
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
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
Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades