Comparison of Calculated Vibratory Rotor Hub Loads With Experimental Data
Detection of helicopter rotor system simulated faults using neural networks
Detection of Helicopter Rotor System Simulated Faults Using Neural Networks
Formulation of a Helicopter Rotor System Damage Detection Methodology
Formulation of a helicopter rotor system damage detection methodology
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
Air Vehicle Diagnostic System Technology Demonstration Program
Aeromechanical stability of a bearingless composite rotor in forward flight
Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades
Aeroelastic response and blade loads ofa composite rotor in forward flight
Aeromechanical stability of rotorcraft with advanced geometry blades
Response and hub loads sensitivity analysis of a helicopter rotor
Health monitoring of a helicopter rotor in forward flight using fuzzy logic
Aeroelastic analysis of advanced geometry tiltrotor aircraft