Actively articulated suspension for a four-wheeled vehicle
Reconfigurable Controls for Rotorcraft - A Feasibility Study
Reconfigurable Controls for Rotorcraft - A Feasibility Study
Status of Euler and Navier-Stokes CFD Methods for Helicopter Applications
Status of Euler and Navier-Stokes CFD Methods for Helicopter Applications
Correlation Studies for Hingeless Rotors in Forward Flight using 2GCHAS
Correlation Studies for Hingeless Rotors in Forward Flight using 2GCHAS
Evaluation of a Flapped Airfoil Configuration for an Advanced Rotor
Evaluation of a Flapped Airfoil Configuration for an Advanced Rotor
Acoustic Flight Tests of Rotorcraft Noise-Abatement Approaches Using Local Differential GPS Guidance
Acoustic Flight Tests of Rotorcraft Noise-Abatement Approaches Using Local Differential GPS Guidance
Stabilization of Periodic Flap-Lag Dynamics in Rotor Blades
Stabilization of Periodic Flap-Lag Dynamics in Rotor Blades
Application of Multigrid CFD Methods to Rotor Analysis
Navier-Stokes Computation of Unsteady Internal Airloads
Navier-Stokes Computation of Unsteady Internal Airloads
Application of Neural Networks to Model and Predict Rotorcraft Hub Loads
Application of Neural Networks to Model and Predict Rotorcraft Hub Loads
Analytical Investigations of Coupled Rotorcraft / Engine / Drive Train Dynamics
Analytical Investigations of Coupled Rotorcraft / Engine / Drive Train Dynamics
Aeroelastic Analysis of Transient Blade Dynamics During Shipboard Engage/Disengage Operations
Aeroelastic Analysis of Transient Blade Dynamics During Shipboard Engage/Disengage Operations
Measurements of Rotor Tip Vortices Using Three-Component Laser Doppler Velocimetry
Aerothermoelastic Behavior of Helicopters with Elastomeric Lag Dampers
Aerothermoelastic Behavior of Helicopters with Elastomeric Lag Dampers
Helicopter Rotor-System Damage Detection
Helicopter Rotor-System Damage Detection
Helicopter Individual-Blade-Control: Promising Technology for the Future Helicopter
Helicopter Individual-Blade-Control: Promising Technology for the Future Helicopter
Aeroelastic Stability of Rotor Blades Using a Parallel Adaptive Finite Element Solver