An Active-Passive Hybrid Method for Optimization of Rotor Blades with Trailing Edge Flaps
Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps
AIAA-2004-1950 Helicopter Blade Lag Damping Using Embedded Fluid Elastic Inertial Dampers
Aeroelastic Stability of Folding Tiltrotor Aircraft in Cruise Flight with Composite Wings
Actuator Bonding Optimization and System Control of a Rotor Blade Ultrasonic Deicing System